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CN108451642B - A quick-change mechanism for mechanical decoupling of a single-port surgical robot - Google Patents

A quick-change mechanism for mechanical decoupling of a single-port surgical robot
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Publication number
CN108451642B
CN108451642BCN201810177475.6ACN201810177475ACN108451642BCN 108451642 BCN108451642 BCN 108451642BCN 201810177475 ACN201810177475 ACN 201810177475ACN 108451642 BCN108451642 BCN 108451642B
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gear shaft
sun gear
joint drive
driving mechanism
joint driving
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CN108451642A (en
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胡三元
冯红光
程晓林
田兆辉
姜秀新
樊炳辉
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Qilu Hospital of Shandong University
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Qilu Hospital of Shandong University
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Abstract

Translated fromChinese

本发明公开了一种用于单孔手术机器人的机械解耦的快换机构,由第一关节驱动机构、第二关节驱动机构、第三关节驱动机构、第四关节驱动机构、第五关节驱动机构、第六关节驱动机构、第七关节驱动机构、第八关节驱动机构和底座壳体、底座外罩、连接件和锁紧机构等组成。手术器械快换机构采用机械解耦机构,完全解决了手术器械执行机构各关节摆转时产生的相互运动耦合问题;将机械解耦机构安装在底座上,可以简化手术器械执行机构的结构设计,有利于手术器械执行机构的量产。本发明的用于单孔手术机器人的机械解耦的快换机构具有方便拆装、易于调整、定位准确、刚度较大、布局合理、小型化、轻量化的优点。

The present invention discloses a mechanically decoupled quick-change mechanism for a single-port surgical robot, which is composed of a first joint drive mechanism, a second joint drive mechanism, a third joint drive mechanism, a fourth joint drive mechanism, a fifth joint drive mechanism, a sixth joint drive mechanism, a seventh joint drive mechanism, an eighth joint drive mechanism, a base shell, a base cover, a connector, and a locking mechanism. The surgical instrument quick-change mechanism adopts a mechanical decoupling mechanism, which completely solves the problem of mutual motion coupling generated when the joints of the surgical instrument actuator are swung; installing the mechanical decoupling mechanism on the base can simplify the structural design of the surgical instrument actuator, which is conducive to the mass production of the surgical instrument actuator. The mechanically decoupled quick-change mechanism for a single-port surgical robot of the present invention has the advantages of convenient disassembly and assembly, easy adjustment, accurate positioning, large rigidity, reasonable layout, miniaturization, and light weight.

Description

Quick-change mechanism for mechanical decoupling of single-hole surgical robot
Technical Field
The invention relates to medical equipment in the field of minimally invasive surgery, in particular to a quick-change mechanism of a minimally invasive surgical single-hole surgical robot suitable for minimally invasive surgery operation of thoracic and abdominal cavities.
Background
Minimally invasive surgery represented by laparoscopy is known as one of important contributions of medical science to human civilization in the 20 th century, and minimally invasive surgery refers to surgery performed by a doctor penetrating into the body through a tiny incision in the surface of the human body by means of an elongated surgical instrument. Compared with the traditional open surgery, the traditional open surgery has the advantages of small surgical incision, small bleeding amount, small postoperative scar, quick recovery time and the like, and achieves the same curative effect as the traditional open surgery. The manual minimally invasive surgical instruments are passive forms of operation, typically with only one degree of freedom of movement at the distal end. In the operation process, a doctor applies a drive to realize the action of the tail end instrument by fingers, and various complex operations including suturing and knotting are smoothly finished by the movement flexibility of the arm and the wrist of the doctor. However, with respect to the auxiliary minimally invasive surgical robot system, since the operation of the surgical instrument is performed by the robot, the robot system itself does not have flexibility of human operation. Therefore, higher requirements are put on the design of surgical instruments dedicated to minimally invasive surgical robots. In order to meet the requirements of minimally invasive surgery, the surgical instrument is designed to meet the requirements of small volume, flexible operation, various forms, convenient installation with a robot arm, sufficient rigidity and strength, suitability for medical environment requirements (such as multiple disinfection) and the like. In particular, the surgical instrument has more degrees of freedom to meet the flexibility requirement so as to be suitable for complex surgical operations such as suture knot tying and the like.
In the minimally invasive surgical robot operation process, the surgical tool is the only part in contact with the pathological tissues of the human body and is also the robot part for directly performing the surgical operation, so that the performance of the surgical tool is the key point of the comprehensive performance of the minimally invasive surgical robot system. In order to meet the requirements of modern minimally invasive surgery, the design of the surgical tool should meet the requirements of exquisite structure, flexible operation, various forms, easy replacement, suitability for medical environment and the like, and particularly the surgical tool should have more degrees of freedom to meet the flexibility requirement and be easy to replace to realize complex surgical operation. Therefore, the performance of the surgical instrument matched with the surgical tool is also an important component of the comprehensive performance of the minimally invasive surgical robot system, and the performance index of the surgical instrument not only influences the use of the surgical tool, but also directly determines the design index and layout mode of the body system. In summary, the performance of the surgical tool and quick-change device is a key factor in representing the overall performance level of the surgical robotic system.
Internationally, a plurality of prototypes in the field of minimally invasive surgical robot system research reach the level of commercial clinical application, including da Vinci, zeus, LAPROTEK systems and the like. The development of surgical robotic systems has been studied to find that surgical tool systems are mainly composed of tool parts and quick-change devices. The development trend of the tool part is that the structure of the tool part is simplified more and more, the function of the tool part is more and more powerful, the quick-change device is gradually developed to be compact and integrated, and the performance of the quick-change device is more and more efficient and stable. The existing two sets of commercial minimally invasive surgical robots are four-degree-of-freedom surgical tool systems adopting wire transmission, but the surgical tool systems still have the defects of scattered structural layout, larger external dimensions and the like, so the surgical tool systems still have great development potential.
In China, the research and development of the minimally invasive surgical single-hole surgical robot is still in a starting stage, and particularly, the research on a surgical tool system is greatly different from that of foreign technologies, so that the development of a wire-driven, multi-degree-of-freedom surgical tool and a matched quick-change device with more stable and efficient performance has important significance for filling domestic blank and promoting technical progress in related fields. The research and development of the multi-degree-of-freedom surgical tool system with different silk transmission forms and quick-change modes compared with the existing system has profound significance for improving academic and technical status of China in the scientific research field.
Disclosure of Invention
The invention aims to overcome the defects of the prior art, and provides a mechanical decoupling quick-change mechanism for a minimally invasive single-hole surgical robot, which is convenient to assemble and disassemble, easy to adjust, accurate in positioning, high in rigidity, reasonable in layout, small in size and light in weight, and can clamp a surgical tool to assist a doctor in performing minimally invasive single-hole surgical operation.
The invention provides a mechanical decoupling quick-change mechanism for a minimally invasive single-hole surgical robot, which is convenient to assemble and disassemble, easy to adjust, accurate in positioning, high in rigidity, reasonable in layout, and light in weight, and the specific scheme is as follows:
a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot comprises a fixed seat, wherein a first joint driving mechanism, a second joint driving mechanism, a third joint driving mechanism, a fourth joint driving mechanism, a fifth joint driving mechanism, a sixth joint driving mechanism, a seventh joint driving mechanism and an eighth joint driving mechanism are arranged on the fixed seat;
The first, second, third, fourth, fifth, sixth, seventh and eighth joint driving mechanisms are arranged on the same base, and the first, second, third, fourth, fifth, sixth, seventh and eighth joint driving mechanisms are respectively connected with the surgical execution instrument through an interface clutch disc;
the first, second, third, fourth, fifth, sixth, seventh and eighth joint driving mechanisms correspondingly drive the first, second, third, fourth, fifth, sixth, seventh and eighth joint executing mechanisms of the surgical instrument executing mechanism M to rotate respectively through steel wire ropes;
The first joint driving mechanism comprises a motor, the motor drives the gear shaft to be rotationally connected, and the gear shaft is connected with the corresponding interface clutch disc;
The second, third, fourth, fifth and sixth joint driving mechanisms have the same structure and respectively comprise a motor, the motor drives a sun gear shaft to rotate, a large sun gear and a small sun gear are arranged on the sun gear shaft, the large sun gear and the small sun gear are meshed with three planetary gears arranged on a planet carrier gear shaft, the three planetary gears are externally meshed with the small sun gear, the three planetary gears are internally meshed with the large sun gear, the three planetary gears are uniformly distributed around the axis of the sun gear shaft, and the planet carrier gear shaft is connected with an interface clutch disc corresponding to the planetary gear shaft;
The seventh joint driving mechanism and the eighth joint driving mechanism have the same structure and respectively comprise a motor, the motors drive a sun gear shaft to rotate, a large sun gear and a small sun gear are arranged on the sun gear shaft, the large sun gear and the small sun gear are meshed with three planetary gears arranged on a planet carrier, the three planetary gears are externally meshed with the small sun gear, the three planetary gears are internally meshed with the large sun gear, the three planetary gears are uniformly distributed around the axis of the sun gear shaft, and the planet carrier is connected with an interface clutch disc corresponding to the planetary carrier;
a transition gear shaft is arranged among the first, second, third, fourth, fifth and sixth joint driving mechanisms, a transition gear shaft is arranged among the sixth and seventh joint driving mechanisms and the eighth joint driving mechanism respectively, and no transition gear shaft is arranged among the seventh and eighth joint driving mechanisms;
The gear shaft of the first joint driving mechanism is externally meshed with the transition gear shaft between the first joint driving mechanism and the second joint driving mechanism, and the transition gear shaft between the first joint driving mechanism and the second joint driving mechanism is externally meshed with the large sun gear of the second joint driving mechanism;
The planet carrier gear shaft of the second joint driving mechanism is externally meshed with the transition gear shafts between the second joint driving mechanism and the third joint driving mechanism, and the transition gear shafts between the second joint driving mechanism and the third joint driving mechanism are externally meshed with the large sun gear of the third joint driving mechanism;
The planet carrier gear shaft of the third joint driving mechanism is externally meshed with the transition gear shafts between the third joint driving mechanism and the fourth joint driving mechanism, and the transition gear shafts between the third joint driving mechanism and the fourth joint driving mechanism are externally meshed with the large sun gear of the fourth joint driving mechanism;
The planet carrier gear shaft of the fourth joint driving mechanism is externally meshed with the transition gear shafts between the fourth joint driving mechanism and the fifth joint driving mechanism, and the transition gear shafts between the fourth joint driving mechanism and the fifth joint driving mechanism are externally meshed with the large sun gear of the fifth joint driving mechanism;
The planet carrier gear shaft of the fifth joint driving mechanism is externally meshed with the transition gear shafts between the fifth joint driving mechanism and the sixth joint driving mechanism, and the transition gear shafts between the fifth joint driving mechanism and the sixth joint driving mechanism are externally meshed with the large sun gear of the sixth joint driving mechanism;
The planet carrier gear shaft of the sixth joint driving mechanism is externally meshed with the transition gear shafts between the sixth joint driving mechanism and the seventh joint driving mechanism, and the transition gear shafts between the sixth joint driving mechanism and the seventh joint driving mechanism are externally meshed with the large sun gear of the seventh joint driving mechanism;
The planet carrier gear shaft of the sixth joint driving mechanism is externally meshed with the transition gear shafts between the sixth joint driving mechanism and the eighth joint driving mechanism, and the transition gear shafts between the sixth joint driving mechanism and the eighth joint driving mechanism are externally meshed with the large sun gear of the eighth joint driving mechanism.
Furthermore, the two ends of the gear shaft of the first joint driving mechanism are axially fixed through bearings, and the bearings are fixed on the base.
Further, one end of the planet carrier gear shaft of the second, third, fourth, fifth and sixth joint driving mechanisms extends out of the three pin shafts, the three pin shafts of the planet carrier gear shaft are respectively inserted into the center holes of the three planet gears, one end of the planet carrier gear shaft is axially fixed through the bearings, the other end of the planet carrier gear shaft is axially fixed through the three planet gears, two ends of the sun gear shaft and two ends of the large sun gear are respectively axially fixed through the bearings, one bearing is fixed on the sun gear shaft and the large sun gear, the other two bearings are fixed on the base, and one end of the planet carrier gear shaft is in interference fit with the interface clutch disc.
Further, one end of the planet carrier of the seventh joint driving mechanism and one end of the planet carrier of the eighth joint driving mechanism extend out of the three pin shafts, the three pin shafts of the planet carrier are respectively inserted into the central holes of the three planet gears, one end of the planet carrier is axially fixed through the bearings, the other end of the planet carrier is axially fixed through the three planet gears, two ends of the sun gear shaft and the large sun gear are respectively axially fixed through the bearings, one bearing is fixed on the sun gear shaft and the large sun gear, the other two bearings are fixed on the base, and one end of the planet carrier is in interference fit with the interface clutch disc.
Further, two ends of a transition gear shaft arranged among the first, second, third, fourth, fifth and sixth joint driving mechanisms and among the sixth joint driving mechanism, the seventh joint driving mechanism and the eighth joint driving mechanism are axially fixed through bearings, and the bearings are fixed on the base.
Further, the cross sections of the small sun wheel and the sun wheel shaft of the second, third, fourth, fifth, sixth, seventh and eighth joint driving mechanisms are in a D shape, the small sun wheel and the D-shaped cross sections of the sun wheel shaft form interference fit, and the small sun wheel and the sun wheel shaft are circumferentially fixed through the D-shaped cross sections.
Further, the first, second, third, fourth, fifth and sixth joint driving mechanisms are arranged in series on the base in sequence in a single row, and the seventh joint driving mechanism, the eighth joint driving mechanism and the sixth joint driving mechanism are arranged on the base in parallel.
Further, the base include base casing and base dustcoat, base casing on be equipped with twice location boss, base casing both sides face is equipped with two long bolt holes respectively, long bolt hole link to each other with the base dustcoat.
Furthermore, the two base covers are respectively arranged and fixed on two sides of the base shell, the upper surface of the base cover is provided with a guide chute, the top end of the guide chute is in a horn mouth shape so as to facilitate the installation of the surgical instrument executing mechanism, the tail end of the guide chute and the bottom of the middle part of the guide chute are in an arc shape, the opening directions of the tail end of the guide chute and the bottom of the middle part of the arc chute are perpendicular to the axial direction of the guide chute, and the tail end of the arc-shaped guide chute and the bottom of the middle part of the guide chute are in interference fit with a fixed pin roll of the surgical instrument executing mechanism so as to prevent the fixed pin roll of the surgical instrument executing mechanism from sliding out from the tail end of the guide chute and the bottom of the middle part of the guide chute on the base cover, thereby leading the surgical instrument executing mechanism to be separated from the quick-change mechanism;
Furthermore, the surgical instrument actuating mechanism can be arranged on the quick-change mechanism along the guide chute on the base housing, two long bolt holes are designed on the base housing, the two long bolt holes on the base housing are perpendicular to the long hole axis of the long bolt hole on the base housing, and the installation relative position of the base housing and the base housing can be conveniently adjusted when the base housing is installed and fixed on the base housing.
Further, the quick-change mechanism base for the minimally invasive surgical single-hole surgical robot further comprises a locking mechanism used for fixing the surgical instrument executing mechanism on the base, each locking mechanism comprises two groups, each group comprises a locking hook, one end of each locking hook is rotatably arranged on the same base outer cover, the other end of each locking hook is provided with a groove, a boss is arranged at a corresponding position on the surgical instrument executing mechanism shell, and the grooves on the locking hooks are matched with the bosses at the corresponding positions on the surgical instrument executing mechanism shell to fix the surgical instrument executing mechanism.
The beneficial effects are that:
compared with the prior art, the quick-change mechanism for mechanical decoupling of the minimally invasive surgical single-hole surgical robot has the following beneficial effects:
1. The quick-change mechanism for mechanical decoupling of the minimally invasive surgical single-hole surgical robot is convenient to assemble and disassemble, easy to adjust, accurate in positioning, high in rigidity, reasonable in layout, small in size and light in weight.
2. The surgical instrument quick-change mechanism adopts mechanical decoupling, and the problem of mutual motion coupling generated when each joint of the surgical instrument actuating mechanism swings is completely solved.
3. Through adjusting the relative mounted position between base dustcoat and the base casing, can adjust the relative mounted position between the interface clutch disc on the guide chute on the base dustcoat and the base casing to when making surgical instrument actuating mechanism M install quick change mechanism N, interface clutch disc on the surgical instrument actuating mechanism M can cooperate the transmission in place just with the interface clutch disc on the base casing, can not lead to interface clutch disc on the surgical instrument actuating mechanism M and the interface clutch disc on the base casing unable cooperation because of interfering.
4. The top of the guide chute on the cutter holder outer cover is made into a horn mouth, so that the surgical instrument executing mechanism M is more convenient and quicker to install into the quick-change mechanism N, the curve of the guide chute can ensure that the cutter driving disc naturally slides to be abutted without interference, and the tail end of the guide chute and the bottom of the middle part of the guide chute adopt interference fit, so that the relative installation position of the surgical instrument executing mechanism M and the quick-change mechanism N can be accurately positioned. The surgical instrument executing mechanism M is installed and taken in and removed from the front upper side of the quick change mechanism N, accords with the customary operation direction, and reduces the installation and removal difficulty.
5. The hook locking mechanism can accurately and reliably fix the surgical instrument executing mechanism M on the quick-change mechanism N, and can conveniently lock and unlock the surgical instrument executing mechanism M.
6. The interface clutch disc on the quick-change mechanism N adopts single-row arrangement, so that the force arm between the fixed points of the surgical instrument executing mechanism M on the base is longer, and the fixation of the surgical instrument executing mechanism M on the base is more favorable for ensuring.
7. The interface clutch disc on the quick-change mechanism N is arranged in a single row, and the motors and the interface clutch disc are coaxially arranged, so that the motors of the second joint driving mechanism, the third joint driving mechanism, the fourth joint driving mechanism, the fifth joint driving mechanism, the sixth joint driving mechanism, the seventh joint driving mechanism and the eighth joint driving mechanism can be arranged in a single row, the possibility of interference when a plurality of quick-change mechanisms act cooperatively is reduced, and the space arrangement is reasonable.
8. The mechanical decoupling mechanism is designed on the quick-change mechanism N and is not designed on the surgical instrument executing mechanism M, so that the structural design of the surgical instrument executing mechanism M can be simplified, and the mass production of the surgical instrument executing mechanism M is facilitated.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings that are required in the embodiments or the description of the prior art will be briefly introduced below, it being obvious that the drawings in the following description are not necessarily to scale, but merely exemplary of the present invention, the drawings described below are only some embodiments of the present invention and not limiting the present invention, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a right side schematic view of a dual-head instrument decoupling structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 2 is a schematic front view of a dual-head instrument decoupling structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot.
Fig. 3 is a schematic top view of a dual-head instrument decoupling structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 4 is a right side schematic view of a single-head instrument decoupling structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 5 is a schematic front view of a single-head instrument decoupling structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot.
Fig. 6 is a right side view schematic of an assembly of a quick-change mechanism and an instrument actuator for mechanical decoupling of a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 7 is an assembled front view schematic of a mechanically decoupled quick-change mechanism and instrument actuator for a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 8 is an assembled top view schematic of a mechanically decoupled quick-change mechanism and instrument actuator for a minimally invasive surgical single-hole surgical robot of the present invention.
Fig. 9 is a schematic view of a base housing structure of a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot.
Fig. 10 is a right-side schematic view of a second embodiment of a dual-head instrument decoupling structure for a mechanically decoupled quick-change mechanism of a minimally invasive surgical single-hole surgical robot.
Fig. 11 is a schematic front view of a second embodiment of a dual-head instrument decoupling structure for a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot.
Fig. 12 is a right-side schematic view of a second embodiment of a single-head instrument decoupling structure for a mechanically decoupled quick-change mechanism of a minimally invasive surgical single-hole surgical robot.
Fig. 13 is a schematic front view of a second embodiment of a single-head instrument decoupling structure for a quick-change mechanism for mechanical decoupling of a minimally invasive surgical single-hole surgical robot.
Fig. 14-16 are partial enlarged views of fig. 7.
Fig. 17 to 18 are partial enlarged views of fig. 8.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The explanation of the reference numerals is specifically omitted among the reference numerals described below: 1_4 to 8_10 are represented by: 1_4, 2_10, 3_10, 4_10, 5_10, 6_10, 7_10, 8_10, and 2_3 to 8_3 are represented by: 2_3, 3_3, 4_3, 5_3, 6_3, 7_3, 8_3, 2_4 to 8_4 are represented by 2_4, 3_4, 5_4, 6_4, 7_4, 8_4, 2_10 to 6_10 are represented by 2_10, 3_10, 4_10, 5_10, 6_10, 2_3 to 6_3 are represented by 2_3, 3_3, 4_3, 5_3, 6_3, 2_6_6 to 2 are represented by 2_6, 2_7, 2_8 are represented by 3_6, 3_7, 3_8, 4_6 to 4_8 are represented by 4_6, 4_7, 4_8 are represented by 5_6 to 5_8, 5_8 are represented by 6_6, 6_76, 7, 1_7, 2_8 are represented by 2_6, 2_7, 2_8 are represented by 2_4_8, 2_8 are represented by 2_6, 2_4_8, 2_8 are represented by 2_4_8, 2_5_8 are represented by 3_6, 2_5_8, 5_6, 5_8 are represented by 2_5_6, 2_4 are represented by 3_1, 2_4, 2_1 are represented by 2_4, 2_2_4, 2_4, 2_2 represented by 2 each 2 by 2 each 2.2 each 2 each and each and.
Example 1
The mechanical decoupling quick-change mechanism for the minimally invasive single-hole surgical robot according to the present embodiment is described with reference to fig. 1 to 3, 6 to 9, and 14 to 18, and includes a fixing seat 1_1, and a first joint driving mechanism 1, a second joint driving mechanism 2, a third joint driving mechanism 3, a fourth joint driving mechanism 4, a fifth joint driving mechanism 5, a sixth joint driving mechanism 6, a seventh joint driving mechanism 7, an eighth joint driving mechanism 8, and the like, which are mounted on the fixing seat 1_1.
The first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5, the sixth joint driving mechanism 6, the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 are arranged on the same base 1_1, and the first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5, the sixth joint driving mechanism 6, the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 are respectively connected with the surgical instrument executing mechanism M through an interface clutch disc 1_4-8_10;
The first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5, the sixth joint driving mechanism 6, the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 correspondingly drive the rotation of the first joint executing mechanism 9, the second joint executing mechanism 10, the third joint executing mechanism 11, the fourth joint executing mechanism 12, the fifth joint executing mechanism 13, the sixth joint executing mechanism 14, the seventh joint executing mechanism 15 and the eighth joint executing mechanism 16 of the surgical instrument executing mechanism M through steel wire ropes respectively;
The first joint driving mechanism 1 comprises a motor 1_7, wherein the motor 1_7 is connected with a gear shaft 1_9 through a coupler 1_8, and the gear shaft 1_9 is connected with a corresponding interface clutch disc 1_4;
The second joint driving mechanism 2 comprises a motor 2_1, the motor 2_1 is connected with a sun gear shaft 2_3 through a coupling 2_2, a large sun gear 2_5 and a small sun gear 2_4 are arranged on the sun gear shaft 2_3, the large sun gear 2_5 and the small sun gear 2_4 are meshed with three planetary gears 2_6-2_8 arranged on a planet carrier gear shaft 2_9, the three planetary gears 2_6-2_8 are meshed with the small sun gear 2_4, the three planetary gears 2_6-2_8 are meshed with the large sun gear 2_5, the three planetary gears 2_6-2_8 are uniformly distributed around the sun gear shaft 2_3, and a planet carrier gear shaft 2_9 is connected with an interface clutch disc 2_10 corresponding to the planetary gear shaft;
The third joint driving mechanism 3 comprises a motor 3_1, the motor 3_1 is connected with a sun gear shaft 3_3 through a coupler 3_2, a large sun gear 3_5 and a small sun gear 3_4 are arranged on the sun gear shaft 3_3, the large sun gear 3_5 and the small sun gear 3_4 are meshed with three planetary gears 3_6-3_8 arranged on a planet carrier gear shaft 3_9, the three planetary gears 3_6-3_8 are meshed with the small sun gear 3_4, the three planetary gears 3_6-3_8 are meshed with the large sun gear 3_5, the three planetary gears 3_6-3_8 are uniformly distributed around the sun gear shaft 3_3, and a planet carrier gear shaft 3_9 is connected with an interface clutch disc 3_10 corresponding to the planetary gear shaft;
The fourth joint driving mechanism 4 comprises a motor 4_1, the motor 4_1 is connected with a sun gear shaft 4_3 through a coupler 4_2, a large sun gear 4_5 and a small sun gear 4_4 are arranged on the sun gear shaft 4_3, the large sun gear 4_5 and the small sun gear 4_4 are meshed with three planetary gears 4_6-4_8 arranged on a planet carrier gear shaft 4_9, the three planetary gears 4_6-4_8 are meshed with the small sun gear 4_4, the three planetary gears 4_6-4_8 are meshed with the large sun gear 4_5, the three planetary gears 4_6-4_8 are uniformly distributed around the sun gear shaft 4_3, and a planet carrier gear shaft 4_9 is connected with an interface clutch disc 4_10 corresponding to the planetary gear shaft;
The fifth joint driving mechanism 5 comprises a motor 5_1, the motor 5_1 is connected with a sun gear shaft 5_3 through a coupling 5_2, a large sun gear 5_5 and a small sun gear 5_4 are arranged on the sun gear shaft 5_3, the large sun gear 5_5 and the small sun gear 5_4 are meshed with three planetary gears 5_6-5_8 arranged on a planet carrier gear shaft 5_9, the three planetary gears 5_6-5_8 are meshed with a small sun gear 5_4 externally, the three planetary gears 5_6-5_8 are meshed with the large sun gear 5_5 internally, the three planetary gears 5_6-5_8 are uniformly distributed around the axis of the sun gear shaft 5_3, and the planet carrier gear shaft 5_9 is connected with an interface clutch disc 5_10 corresponding to the planetary carrier gear shaft;
The sixth joint driving mechanism 6 comprises a motor 6_1, the motor 6_1 is connected with a sun gear shaft 6_3 through a coupler 6_2, a large sun gear 6_5 and a small sun gear 6_4 are arranged on the sun gear shaft 6_3, the large sun gear 6_5 and the small sun gear 6_4 are meshed with three planetary gears 6_6-6_8 arranged on a planet carrier gear shaft 6_9, the three planetary gears 6_6-6_8 are meshed with a small sun gear 6_4 externally, the three planetary gears 6_6-6_8 are meshed with a large sun gear 6_5 internally, the three planetary gears 6_6-6_8 are uniformly distributed around a sun gear shaft 6_3 axis, and the planet carrier gear shaft 6_9 is connected with an interface clutch disc 6_10 corresponding to the planetary gear shaft 6_9;
The seventh joint driving mechanism 7 comprises a motor 7_1, the motor is connected with a sun gear shaft 7_3 through a coupling 7_2, a large sun gear 7_5 and a small sun gear 7_4 are arranged on the sun gear shaft 7_3, the large sun gear 7_5 and the small sun gear 7_4 are meshed with three planetary gears 7_6-7_8 arranged on a planet carrier 7_8, the three planetary gears 7_6-7_8 are meshed with the small sun gear 7_4 externally, the three planetary gears 7_6-7_8 are meshed with the large sun gear 7_5 internally, the three planetary gears 7_6-7_8 are evenly distributed around the sun gear shaft 7_3, and the planet carrier 7_9 is connected with an interface clutch disc 7_10 corresponding to the planetary carrier 7_9;
The eighth joint driving mechanism 8 comprises a motor 8_1 which is connected with a sun gear shaft 8_3 through a coupler 8_2, a large sun gear 8_5 and a small sun gear 8_4 are arranged on the sun gear shaft 8_3, the large sun gear 8_5 and the small sun gear 8_4 are meshed with three planetary gears 8_6-8_8 arranged on a planet carrier 8_8, the three planetary gears 8_6-8_8 are meshed with the small sun gear 8_4 externally, the three planetary gears 8_6-8_8 are meshed with the large sun gear 8_5 internally, the three planetary gears 8_6-8_8 are uniformly distributed around the axis of the sun gear shaft 8_3, and the planet carrier 8_9 is connected with an interface clutch disc 8_10 corresponding to the planetary gear carrier 8_9;
A transition gear shaft 1_2_1-5_6_1 is arranged among the first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6;
A transition gear shaft 6_7_1 and a transition gear shaft 6_8_1 are respectively arranged between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 and between the sixth joint driving mechanism 8;
a transition gear shaft is not arranged between the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8;
The gear shaft 1_9 of the first joint driving mechanism 1 is externally meshed with the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2, and the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2 is externally meshed with the large sun gear 2_5 of the second joint driving mechanism 2;
The gear shaft 2_3 of the second joint driving mechanism 2 is externally meshed with the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3, and the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3 is externally meshed with the large sun gear 3_5 of the third joint driving mechanism 3;
The planet carrier gear shaft 3_9 of the third joint driving mechanism 3 is externally meshed with the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4, and the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4 is externally meshed with the large sun gear 4_5 of the fourth joint driving mechanism 4;
The planet carrier gear shaft 4_9 of the fourth joint driving mechanism 4 is externally meshed with the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5, and the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5 is externally meshed with the large sun gear 5_5 of the fifth joint driving mechanism 5;
the planet carrier gear shaft 5_9 of the fifth joint driving mechanism 5 is externally meshed with the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6, and the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 is externally meshed with the large sun gear 6_5 of the sixth joint driving mechanism 6;
The planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 is externally meshed with the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7, and the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 is externally meshed with the large sun gear 7_5 of the seventh joint driving mechanism 7;
The planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 is externally meshed with the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8, and the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8 is externally meshed with the large sun gear 8_5 of the eighth joint driving mechanism 8;
Further, two ends of the gear shaft 1_9 of the first joint driving mechanism 1 are axially fixed through a bearing 1_5 and a bearing 1_6, and the bearing 1_5 and the bearing 1_6 are fixed on the base 1_3.
Further, one end of the planet carrier gear shaft 2_9 of the second joint driving mechanism 2 extends out of three pins, the three pins of the planet carrier gear shaft 2_9 are respectively inserted into the central holes of the three planet gears 2_6-2_8, one end of the planet carrier gear shaft 2_9 is axially fixed through a bearing 2_11, the other end of the planet carrier gear shaft 2_9 is axially fixed through the three planet gears 2_6-2_8, two ends of the sun gear shaft 2_3 and the large sun gear 2_5 are respectively axially fixed through a bearing 2_12 and a bearing 2_13, the bearing 2_12 is fixed on the sun gear shaft 2_3 and the large sun gear 2_5, the bearing 2_11 and the bearing 2_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 2_9 and the interface clutch disc 2_10 form interference fit.
Further, one end of the planet carrier gear shaft 3_9 of the third joint driving mechanism 3 extends out of three pins, the three pins of the planet carrier gear shaft 3_9 are respectively inserted into the central holes of the three planet gears 3_6-3_8, one end of the planet carrier gear shaft 3_9 is axially fixed through a bearing 3_11, the other end of the planet carrier gear shaft 3_9 is axially fixed through the three planet gears 3_6-3_8, two ends of the sun gear shaft 3_3 and the large sun gear 3_5 are respectively axially fixed through a bearing 3_12 and a bearing 3_13, the bearing 3_12 is fixed on the sun gear shaft 3_3 and the large sun gear 3_5, the bearing 3_11 and the bearing 3_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 3_9 and the interface clutch disc 3_10 form interference fit.
Further, one end of the planet carrier gear shaft 4_9 of the fourth joint driving mechanism 4 extends out of three pins, the three pins of the planet carrier gear shaft 4_9 are respectively inserted into the central holes of the three planet gears 4_6-4_8, one end of the planet carrier gear shaft 4_9 is axially fixed through a bearing 4_11, the other end of the planet carrier gear shaft 4_9 is axially fixed through the three planet gears 4_6-4_8, two ends of the sun gear shaft 4_3 and the large sun gear 4_5 are respectively axially fixed through a bearing 4_12 and a bearing 4_13, the bearing 4_12 is fixed on the sun gear shaft 4_3 and the large sun gear 4_5, the bearing 4_11 and the bearing 4_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 4_9 and the interface clutch disc 4_10 form interference fit.
Further, one end of the planet carrier gear shaft 5_9 of the fifth joint driving mechanism 5 extends out of three pin shafts, the three pin shafts of the planet carrier gear shaft 5_9 are respectively inserted into the central holes of the three planet gears 5_6-5_8, one end of the planet carrier gear shaft 5_9 is axially fixed through a bearing 5_11, the other end of the planet carrier gear shaft 5_9 is axially fixed through the three planet gears 5_6-5_8, two ends of the sun gear shaft 5_3 and the large sun gear 5_5 are respectively axially fixed through a bearing 5_12 and a bearing 5_13, the bearing 5_12 is fixed on the sun gear shaft 5_3 and the large sun gear 5_5, the bearing 5_11 and the bearing 5_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 5_9 and the interface clutch disc 5_10 form interference fit.
Further, one end of the planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 extends out of three pins, the three pins of the planet carrier gear shaft 6_9 are respectively inserted into the central holes of the three planet gears 6_6 to 6_8, one end of the planet carrier gear shaft 6_9 is axially fixed through a bearing 6_11, the other end of the planet carrier gear shaft 6_9 is axially fixed through the three planet gears 6_6 to 6_8, two ends of the sun gear shaft 6_3 and the large sun gear 6_5 are respectively axially fixed through a bearing 6_12 and a bearing 6_13, the bearing 6_12 is fixed on the sun gear shaft 6_3 and the large sun gear 6_5, the bearing 6_11 and the bearing 6_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 6_9 and the interface clutch disc 6_10 form interference fit.
Further, one end of the planet carrier 7_9 of the seventh joint driving mechanism 7 extends out of three pins, the three pins of the planet carrier 7_9 are respectively inserted into the central holes of the three planet gears 7_6-7_8, one end of the planet carrier 7_9 is axially fixed through a bearing 7_11, the other end of the planet carrier 7_9 is axially fixed through the three planet gears 7_6-7_8, two ends of the sun gear shaft 7_3 and the large sun gear 7_5 are respectively axially fixed through a bearing 7_12 and a bearing 7_13, the bearing 7_12 is fixed on the sun gear shaft 7_3 and the large sun gear 7_5, the bearing 7_11 and the bearing 7_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 7_9 and the interface clutch disc 7_10 form interference fit.
Further, one end of the planet carrier 8_9 of the eighth joint driving mechanism 8 extends out of three pins, the three pins of the planet carrier 8_9 are respectively inserted into the central holes of the three planet gears 8_6-8_8, one end of the planet carrier 8_9 is axially fixed through a bearing 8_11, the other end of the planet carrier 8_9 is axially fixed through the three planet gears 8_6-8_8, two ends of the sun gear shaft 8_3 and the large sun gear 8_5 are respectively axially fixed through a bearing 8_12 and a bearing 8_13, the bearing 8_12 is fixed on the sun gear shaft 8_3 and the large sun gear 8_5, the bearing 8_11 and the bearing 8_13 are fixed on the base 1_3, and one end of the planet carrier gear shaft 8_9 and the interface clutch disc 8_10 form interference fit.
Further, the two ends of the transition gear shafts 1_2_1 to 6_8_1 installed between the first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 and between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 and between the eighth joint driving mechanism 8 are respectively and axially fixed through bearings 1_2_2 to 6_8_3, and the bearings 1_2_2 to 6_8_3 are fixed on the base 1_3.
Further, the sections of the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5, the sixth joint driving mechanism 6, the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 are in a shape of D, the sections of the small sun gears 2_4-8_4 and the sun gear shafts 2_3-8_3 are in interference fit, and the sections of the small sun gears 2_4-8_4 and the sun gear shafts 2_3-8_3 are circumferentially fixed through the sections of the D.
Further, the first joint driving mechanism 1, the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 are sequentially arranged in series in a single row on the base 1_3, and the seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 are arranged in parallel with the sixth joint driving mechanism 6 on the base 1_3.
Further, the base 1_3 includes a base housing 1_3_1 and a base housing 1_3_2, two positioning bosses are disposed on the base housing 1_3_1, two long bolt holes are respectively disposed on two sides of the base housing 1_3_1, and the long bolt holes are connected with the base housing 1_3_2.
Furthermore, the two base outer covers 1_3_2 are respectively arranged and fixed on two sides of the base shell 1_3_1, a guide chute is designed on the base outer cover 1_3_2, the top end of the guide chute is in a horn mouth shape so as to facilitate the installation of the surgical instrument executing mechanism M, the tail end of the guide chute and the bottom of the middle part of the guide chute on the base outer cover 1_3_2 are in an arc shape, the opening directions of the bottom of the arc-shaped chute at the tail end and the bottom of the middle part of the guide chute are perpendicular to the axial direction of the guide chute, and the tail end and the bottom of the middle part of the arc-shaped guide chute and the fixed pin shaft 1_3_4 of the surgical instrument executing mechanism M form interference fit to prevent the fixed pin shaft 1_3_4 of the surgical instrument executing mechanism M from sliding out from the tail end of the guide chute on the base outer cover 1_3_2 and the bottom of the middle part of the guide chute, so that the surgical instrument executing mechanism M and the quick-change mechanism N are separated;
Furthermore, the surgical instrument executing mechanism M can be installed on the quick-change mechanism N along a guide chute on the base housing 1_3_2, two long bolt holes are designed on the base housing 1_3_2, the two long bolt holes on the base housing 1_3_2 are perpendicular to the long bolt hole axes on the base housing 1_3_1, and the installation relative positions of the base housing 1_3_2 and the base housing 1_3_1 can be conveniently adjusted when the base housing 1_3_2 is installed and fixed on the base housing 1_3_1.
Further, the quick-change mechanism N base 1_3 for the minimally invasive surgery single-hole surgical robot further comprises a locking mechanism 1_3_3 for fixing the surgical instrument executing mechanism M on the base 1_3, wherein each locking mechanism 1_3_3 comprises two groups, each group comprises a locking hook, namely, the locking hook 1_3_3_1 and the locking hook 1_3_3_2, one end of each locking hook 1_3_1 and one end of each locking hook 1_3_2 are rotatably arranged on the same base housing 1_3_2, grooves are formed in the other ends of the locking hooks 1_3_3_1 and the locking hooks 1_3_3_2, bosses are formed in corresponding positions on the outer shell of the surgical instrument executing mechanism M, and the grooves on the locking hooks 1_3_1 and 1_3_2 are matched with the bosses on corresponding positions on the outer shell of the surgical instrument executing mechanism M for fixing the surgical instrument executing mechanism M.
The working principle of the invention is as follows:
The interface clutch disc 1_4 of the first joint driving mechanism 1 rotates clockwise around the axis of the gear shaft 1_9, namely, the motor 1_7 on the first joint driving mechanism 1 is started to rotate the output shaft of the motor clockwise, so that the coupler 1_8 and the gear shaft 1_9 on the first joint driving mechanism 1 are driven to rotate clockwise, and the interface clutch disc 1_4 on the first joint driving mechanism 1 is driven to rotate clockwise around the axis of the gear shaft 1_9. The first arm segment 9_2 of the surgical instrument actuator M is actively rotated clockwise relative to the end-effector junction box 1_10 to change the relative angle between the first arm segment 9_2 and the end-effector junction box 1_10.
The gear shaft 1_9 of the first joint driving mechanism 1 is externally meshed with the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2, and the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2 is externally meshed with the large sun gear 2_5 of the second joint driving mechanism 2; at this time, the gear shaft 1_9 of the first joint driving mechanism 1 drives the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2 to rotate anticlockwise, the transition gear shaft 1_2_1 between the first joint driving mechanism 1 and the second joint driving mechanism 2 drives the external gear of the large sun gear 2_5 on the second joint driving mechanism 2 to rotate clockwise, the three planetary gears 2_6-2_8 on the second joint driving mechanism 2 are meshed with the large sun gear 2_5, each planetary gear 2_6-2_8 rotates clockwise around the axis of the planetary gear while rotating clockwise around the axis of the sun gear shaft 2_3, the three planetary gears 2_6-2_8 drive the planet carrier gear shaft 2_9 to rotate clockwise around the axis of the sun gear shaft 2_3, and the planet carrier gear shaft 2_9 drives the interface clutch disc 2_10 to rotate clockwise around the axis of the sun gear shaft 2_3 at this time, and the small sun gears 2_4 and the sun gear shaft 2_3 on the second joint driving mechanism 2 do not rotate clockwise. When the first joint 9_1 swings clockwise and the second joint 10_1 swings clockwise at the same time, the second joint 10_1 and the first joint 9_1 are set to have the same steering direction and the same rotating speed, and the first arm segment 9_2 of the surgical instrument executing mechanism M actively swings clockwise relative to the tail end transmission box connecting sleeve 1_10 to change the relative included angle between the first arm segment 9_2 and the tail end transmission box connecting sleeve 1_10, the second arm segment 10_2 does not swing passively relative to the first arm segment 9_2 to change the relative included angle between the second arm segment 10_2 and the first arm segment 9_2, and the purpose of decoupling is achieved through a mechanical structure.
The gear shaft 2_3 of the second joint driving mechanism 2 is externally meshed with the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3, the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3 is externally meshed with the large sun gear 3_5 of the third joint driving mechanism 3, at the moment, the gear shaft 2_3 of the second joint driving mechanism 2 drives the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3 to rotate anticlockwise, the transition gear shaft 2_3_1 between the second joint driving mechanism 2 and the third joint driving mechanism 3 drives an external gear of the large sun gear 3_5 on the third joint driving mechanism 3 to rotate clockwise, the three planetary gears 3_6-3_8 on the third joint driving mechanism 3 are internally meshed with the large sun gear 3_5, each planetary gear 3_6-3_8 rotates clockwise around the axis of the sun gear shaft 3_5 while rotating clockwise around the self-axis, the three planetary gears 3_6-3_8 drive the planetary gear shaft to rotate clockwise around the axis of the sun gear shaft 3_3_3, the three planetary gear shafts 3_6-3_8 drive the planetary gear shaft to rotate clockwise around the sun gear shaft 3_3_5, and the planetary carrier 3_3_4 rotates clockwise around the sun gear shaft 3_4, and the sun gear shaft 3_4 rotates clockwise. The second joint 10_1 swings clockwise and the third joint 11_1 swings clockwise, the proper proportion is set, the third joint 11_1 and the first joint 9_1 are identical in steering, the rotating speeds are equal, and when the first arm section 9_2 of the surgical instrument executing mechanism M swings clockwise relative to the tail end transmission box connecting sleeve 1_10 actively, the relative included angle between the first arm section 9_2 and the tail end transmission box connecting sleeve 1_10 is changed, the third arm section 11_2 does not swing passively relative to the second arm section 10_2, the relative included angle between the third arm section 11_2 and the second arm section 10_2 is not changed, and the aim of decoupling is achieved through a mechanical structure.
The planet carrier gear shaft 3_9 of the third joint driving mechanism 3 is externally meshed with the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4, the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4 is externally meshed with the large sun gear 4_5 of the fourth joint driving mechanism 4, at the moment, the planet carrier gear shaft 3_9 of the third joint driving mechanism 3 drives the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4 to rotate anticlockwise, the transition gear shaft 3_4_1 between the third joint driving mechanism 3 and the fourth joint driving mechanism 4 drives the outer gear of the large sun gear 4_5 on the fourth joint driving mechanism 4 to rotate clockwise, the three planet gears 4_6-4_8 on the fourth joint driving mechanism 4_5 are internally meshed with the large sun gear 4_5, at the moment, the planet gears 4_6-4_8 rotate clockwise around the axis of the sun gear shaft 4_3 while rotating clockwise around the self-axis, the planet carrier gear shaft 3_4_4_1 drives the planet gears to rotate clockwise around the sun gear shaft 3_4_1, and the planet carrier 4_4_4_4_4_4_4_4 rotates clockwise around the sun gear shaft 3, and the planet carrier 4_4_4_4_4 rotates clockwise around the sun gear shaft 4_4_4_4_4 rotates clockwise, and the planet carrier 4_4_4_4 rotates the sun gear 4_4_4_4_4 and the sun gear 4 rotates clockwise. The third joint 11_1 swings clockwise and the fourth joint 12_1 swings clockwise at the same time, the right proportion is set, the fourth joint 12_1 and the first joint 9_1 are identical in steering, the rotating speed is equal, and when the first arm section 9_2 of the surgical instrument executing mechanism M swings clockwise relative to the tail end transmission box connecting sleeve 1_10 actively, the relative included angle between the first arm section 9_2 and the tail end transmission box connecting sleeve 1_10 is changed, the fourth arm section 12_2 does not swing passively relative to the third arm section 11_2, the relative included angle between the fourth arm section 12_2 and the third arm section 11_2 is not changed, and the aim of decoupling is achieved through a mechanical structure.
The planet carrier gear shaft 4_9 of the fourth joint driving mechanism 4 is externally meshed with the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5, the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5 is externally meshed with the large sun gear 5_5 of the fifth joint driving mechanism 5, at the moment, the planet carrier gear shaft 4_9 of the fourth joint driving mechanism 4 drives the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5 to rotate anticlockwise, the transition gear shaft 4_5_1 between the fourth joint driving mechanism 4 and the fifth joint driving mechanism 5 drives the outer gear of the large sun gear 5_5 on the fifth joint driving mechanism 5 to rotate clockwise, the three planet gears 5_6-5_8 on the fifth joint driving mechanism 5 are internally meshed with the large sun gear 5_5, at the moment, the planet gears 5_6-5_8 rotate clockwise around the axis of the sun gear shaft 5_3 simultaneously, the three planet gears 5_6-5_8 rotate clockwise around the axis of the sun gear shaft 5_3, the planet carrier 5_5_1 drives the planet carrier 5_5_3 to rotate clockwise around the sun gear shaft 5_3, and the planet carrier 5_5_9 does not rotate clockwise around the sun gear shaft 5_3 rotates clockwise, and the planet carrier 5_5_5_3 rotates clockwise around the sun gear shaft 5_3, and the sun gear shaft 5_5_3 rotates clockwise around the sun gear shaft 5_3, and the sun carrier 5_5_5 rotates clockwise, and the sun gear 5_3 rotates the sun gear shaft 5_5_5_5. The fourth joint 12_1 swings clockwise and the fifth joint 13_1 swings clockwise, the proper proportion is set, the fifth joint 13_1 and the first joint 9_1 are identical in steering, the rotating speeds are equal, and when the first arm section 9_2 of the surgical instrument executing mechanism M swings clockwise relative to the tail end transmission box connecting sleeve 1_10 actively, the relative included angle between the first arm section 9_2 and the tail end transmission box connecting sleeve 1_10 is changed, the fifth arm section 13_2 does not swing passively relative to the fourth arm section 12_2, the relative included angle between the fifth arm section 13_2 and the fourth arm section 12_2 is not changed, and the aim of decoupling is achieved through a mechanical structure.
The planet carrier gear shaft 5_9 of the fifth joint driving mechanism 5 is externally meshed with the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6, the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 is externally meshed with the large sun gear 6_5 of the sixth joint driving mechanism 6, at the moment, the planet carrier gear shaft 5_9 of the fifth joint driving mechanism 5 drives the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 to rotate anticlockwise, the transition gear shaft 5_6_1 between the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 drives the outer gear of the large sun gear 6_5 on the sixth joint driving mechanism 6 to rotate clockwise, the three planet gears 6_6-6_8 on the sixth joint driving mechanism 6 are all internally meshed with the large sun gear 6_5, each planet gear 6_6-6_8 rotates clockwise around the axis of the sun gear shaft 6_3 at the same time, the planet gears 6-6_8 rotate clockwise around the axis of the sun gear shaft, the planet carrier gear shaft 5_6_6_1 drives the planet gears to rotate clockwise around the axis of the sun gear shaft 6_3, the planet carrier shaft 5_6_6_8 drives the planet carrier shaft 5_6_8 to rotate clockwise around the sun gear shaft axis of the sun gear shaft 6_3, and the planet carrier gear shaft 5_35 drives the planet carrier shaft 5_6_5 rotates clockwise around the sun gear shaft 5_35 to rotate clockwise, and the sun gear shaft axis 5 rotates clockwise, and the planet carrier shaft axis of the sun gear shaft 5 rotates the sun gear shaft 5_5_5 is driven to rotate clockwise, and the sun gear shaft 5 is driven. The fifth joint 13_1 swings clockwise and the sixth joint 14_1 swings clockwise, the proper proportion is set, the sixth joint 14_1 and the first joint 9_1 are identical in steering direction and rotation speed, when the first arm section 9_2 of the surgical instrument executing mechanism M swings clockwise relative to the tail end transmission box connecting sleeve 1_10 actively, and the relative included angle between the first arm section 9_2 and the tail end transmission box connecting sleeve 1_10 is changed, the sixth arm section 14_2 does not swing passively relative to the fifth arm section 13_2, and the relative included angle between the sixth arm section 14_2 and the fifth arm section 13_2 does not change, so that the aim of decoupling is achieved through a mechanical structure.
The planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 is externally meshed with the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7, the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 is externally meshed with the large sun gear 7_5 of the seventh joint driving mechanism 7, at the moment, the planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 drives the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 to rotate anticlockwise, the transition gear shaft 6_7_1 between the sixth joint driving mechanism 6 and the seventh joint driving mechanism 7 drives the outer gear of the large sun gear 7_5 on the seventh joint driving mechanism 7 to rotate clockwise, the three planet gears 7_6-7_8 on the seventh joint driving mechanism 7 are internally meshed with the large sun gear 7_5, each planet gear 7_6-7_8 rotates clockwise around the axis of the planet gears while rotating clockwise around the axis of the sun gear shaft 7_3, the three planet gears 7_6-7_8 drive the planet gears to rotate clockwise around the axis of the sun gear shaft 7_3, the planet carrier 7_9 rotates clockwise around the axis of the sun gear shaft 4, and the planet carrier 7_9 rotates clockwise around the axis 4 of the sun gear shaft 3. The sixth joint 14_1 swings clockwise and the seventh joint 15_1 swings clockwise, the proper proportion is set, the seventh joint 15_1 and the first joint 9_1 are identical in steering direction and rotation speed, when the first arm section 9_2 of the surgical instrument executing mechanism M swings clockwise relative to the tail end transmission box connecting sleeve 1_10 actively, and the relative included angle between the first arm section 9_2 and the tail end transmission box connecting sleeve 1_10 is changed, the first arm section seven 15_2 does not swing passively relative to the first arm section six 14_2, and the relative included angle between the first arm section seven 15_2 and the first arm section six 14_2 does not change, so that the aim of decoupling is achieved through a mechanical structure.
The planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 is externally meshed with the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8, the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8 is externally meshed with the large sun gear 8_5 of the eighth joint driving mechanism 8, at the moment, the planet carrier gear shaft 6_9 of the sixth joint driving mechanism 6 drives the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8 to rotate anticlockwise, the transition gear shaft 6_8_1 between the sixth joint driving mechanism 6 and the eighth joint driving mechanism 8 drives the outer gear of the large sun gear 8_5 on the eighth joint driving mechanism 8 to rotate clockwise, the three planet gears 8_6-8_8 on the eighth joint driving mechanism 8 are internally meshed with the large sun gear 8_5, each planet gear 8_6-8 rotates clockwise around the axis line of the planet gears while rotating clockwise around the axis of the sun gear shaft 8_3, the three planet gears 6-8_8 rotate clockwise around the axis line of the planet carrier 8_3 to rotate clockwise around the sun gear shaft 8_4, and the planet carrier 538-8-rotates clockwise around the axis of the sun gear shaft 3276. The eighth joint 16_1 is clockwise swung while the sixth joint 14_1 is clockwise swung, and the proper proportion is set, so that the eighth joint 16_1 and the first joint 9_1 are the same in steering and equal in rotating speed, and when the first arm segment 9_2 of the surgical instrument executing mechanism M is clockwise actively swung relative to the tail end transmission box connecting sleeve 1_10 to change the relative included angle between the first arm segment 9_2 and the tail end transmission box connecting sleeve 1_10, the eighth arm segment 16_2 is not passively swung relative to the sixth arm segment 14_2, and the relative included angle between the eighth arm segment 16_2 and the sixth arm segment 14_2 is not changed, so that the aim of decoupling is fulfilled through a mechanical structure.
The interface clutch disc 1_4 of the first joint driving mechanism 1 realizes a counterclockwise rotation around the axis of the gear shaft 1_9. The counterclockwise rotation around the axis of the gear shaft 1_9 of the interface clutch disc 1_4 of the first joint driving mechanism 1 is the same as the clockwise rotation around the axis of the gear shaft 1_9 of the interface clutch disc 1_4 of the first joint driving mechanism 1 in a transmission line, and the directions are opposite.
The second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the axes of the interface clutch plates 2_10-6_10 around the gear shafts 2_3-6_3 of the sixth joint driving mechanism 6 realize clockwise rotation, which is similar to the clockwise rotation of the axes of the interface clutch plates 1_4 around the gear shafts 1_3 of the first joint driving mechanism 1 in a transmission mode, the joint driving mechanisms actively rotate, and simultaneously the motion is transmitted to all joint driving mechanisms on one side close to the tail end joint (joint seven 15_1 and joint eight 16_1) of the surgical instrument executing mechanism M step by step, and the proper proportion is set, so that all joint driving mechanisms on the back side of the active rotation joint driving mechanism (on one side close to the tail end joint (joint seven 15_1 and joint eight 16_1) of the surgical instrument executing mechanism M) are the same as the active rotation driving mechanism, the rotation speed is equal, the arm section of the surgical instrument M controlled by the active rotation joint driving mechanism is enabled to rotate relative to the front adjacent arm section (joint seven sections are far away from the tail end joint 15_1 and the tail end joint 1) of the surgical instrument executing mechanism M and the front end joint eight (joint eight-16_1) of the surgical instrument executing mechanism is enabled to change the included angle between the front end joint segment and the front end joint 1 (joint 1) of the surgical instrument executing mechanism) to rotate correspondingly, all the joint driving mechanisms at the back of the active rotary joint driving mechanism (the side close to the joint at the tail end of the surgical instrument executing mechanism M (the side of the joint seven 15_1 and the joint eight 16_1)) correspondingly control the arm section of the surgical instrument executing mechanism M relative to the arm section of the surgical instrument executing mechanism M controlled by the active rotary joint driving mechanism, so that the arm section of the surgical instrument executing mechanism M correspondingly controlled by all the joint driving mechanisms at the back of the active rotary joint driving mechanism (the side close to the joint at the tail end of the surgical instrument executing mechanism M (the side of the joint seven 15_1 and the joint eight 16_1)) and the arm section of the surgical instrument executing mechanism M controlled by the active rotary joint driving mechanism do not change relative angles, and the aim of decoupling is achieved through a mechanical structure.
The axes of the interface clutch discs 2_10-6_10 of the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 around the gear shafts 2_3-6_3 realize anticlockwise rotation, wherein the axes of the interface clutch discs 2_10-6_10 of the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the sixth joint driving mechanism 6 around the gear shafts 2_3-6_3 realize anticlockwise rotation which is the same as the driving route of the clockwise rotation of the axes of the interface clutch discs 2_10-6_10 around the gear shafts 2_3-6_3 of the second joint driving mechanism 2, the third joint driving mechanism 3, the fourth joint driving mechanism 4, the fifth joint driving mechanism 5 and the interface clutch discs 2_10-6_10 of the sixth joint driving mechanism 6 realize anticlockwise rotation, and the driving route is opposite in direction.
Starting a motor 7_1 on the seventh joint driving mechanism 7 to enable an output shaft of the motor 7_1 to rotate clockwise, driving a coupler 7_2, a sun gear shaft 7_3 and a small sun gear 7_4 on the seventh joint driving mechanism 7 to rotate clockwise, enabling three planetary gears 7_6-7_8 to be meshed with the small sun gear 7_4, enabling each planetary gear 7_6-7_8 to rotate anticlockwise around an axis of the planetary gear shaft 7_3 and simultaneously enabling the three planetary gears 7_6-7_8 to drive a planet carrier 7_9 to rotate clockwise around an axis of the sun gear shaft 7_3, and enabling the planet carrier 7_9 to drive the interface clutch plate 7_10 to rotate clockwise around the axis of the sun gear shaft 7_3. The external gear of the large sun gear 7_5 on the seventh joint driving mechanism 7 and the seventh joint driving mechanism 7 are externally meshed with the transition gear shaft 6_7_1 of the sixth joint driving mechanism 6, and at this time, the large sun gear 7_5 on the seventh joint driving mechanism 7 is not rotated. The arm segment seven 15_2 of the surgical instrument actuating mechanism M actively swings clockwise relative to the arm segment six 14_2 to change the relative included angle between the arm segment seven 15_2 and the arm segment six 14_2.
The interface clutch disc 7_10 of the seventh joint driving mechanism 7 rotates anticlockwise around the axis of the sun gear shaft 7_3, and the anticlockwise rotation of the interface clutch disc 7_10 of the seventh joint driving mechanism 7 around the axis of the sun gear shaft 7_3 is the same as the clockwise rotation of the interface clutch disc 7_10 of the seventh joint driving mechanism 7 around the axis of the sun gear shaft 7_3 by a transmission route, and the directions are opposite.
The interface clutch disc 8_10 of the eighth joint driving mechanism 8 rotates clockwise around the axis of the sun wheel shaft 8_3, namely, a motor 8_1 on the eighth joint driving mechanism 8 is started to enable an output shaft of the motor 8_1 to rotate clockwise, a coupler 8_2, a sun wheel shaft 8_3 and a small sun wheel 8_4 on the eighth joint driving mechanism 8 are driven to rotate clockwise, three planetary wheels 8_6-8_8 are meshed with the small sun wheel 8_4, each planetary wheel 8_6-8_8 rotates anticlockwise around the axis of the planetary wheel shaft 3435 and simultaneously rotates clockwise around the axis of the sun wheel shaft 8_3, and a planet carrier 8_9 drives the interface clutch disc 8_10 to rotate clockwise around the axis of the sun wheel shaft 8_3. The external gear of the large sun gear 8_5 on the eighth joint driving mechanism 8 and the eighth joint driving mechanism 8 are externally meshed with the transition gear shaft 6_8_1 of the sixth joint driving mechanism 6, and at this time, the large sun gear 8_4 on the eighth joint driving mechanism 8 is not rotated. The arm segment eight 16_2 of the surgical instrument actuating mechanism M actively swings clockwise relative to the arm segment six 14_2 to change the relative included angle between the arm segment eight 16_2 and the arm segment six 14_2.
The interface clutch disc 8_10 of the eighth joint drive mechanism 8 performs a counter-clockwise rotation about the axis of the sun gear shaft 8_3. The interface clutch disc 8_10 of the eighth joint drive mechanism 8 performs a counter-clockwise rotation about the axis of the sun gear shaft 8_3 in the same "transmission line" as the interface clutch disc 8_10 of the eighth joint drive mechanism 8 performs a clockwise rotation about the axis of the sun gear shaft 8_3, with opposite directions.
Adjustment of the relative mounting position between the base housing 1_3_2 and the base housing 1_3_1:
two long bolt holes are designed on the base housing 1_3_2, two long bolt holes are respectively designed on two side surfaces of the base housing 1_3_1, the two long bolt holes on the base housing 1_3_2 are perpendicular to long bolt hole axes on the base housing 1_3_1, and when the two base housings 1_3_2 are fixed on the base housing 1_3_1, the installation relative positions of the base housing 1_3_2 and the base housing 1_3_1 can be adjusted by adjusting the relative fixed positions of the long bolt holes of the base housing 1_3_2 and the base housing 1_3_1.
Mounting and dismounting between the surgical instrument actuator M and the joint driving mechanism N:
When the surgical instrument executing mechanism M is installed in the joint driving mechanism N, the surgical instrument executing mechanism M slides into the tail end and the middle groove bottom of the guide sliding groove on the base housing 1_3_2 along the top end of the guide sliding groove in the shape of a horn mouth on the base housing 1_3_2, the tail end and the middle groove bottom of the guide sliding groove on the base housing 1_3_2 form interference fit with the fixed pin shaft of the surgical instrument executing mechanism M, and simultaneously the two locking hooks 1_3_1 and 1_3_2 on the two base housings 1_3_2 are respectively rotated, so that the grooves on the locking hooks 1_3_1 and 1_3_3_2 are matched with the bosses on the corresponding positions on the outer housing of the surgical instrument executing mechanism M, and the fixed pin shaft 1_3_4 of the surgical instrument executing mechanism M is prevented from sliding out of the guide sliding groove on the base housing 1_3_2, so that the surgical instrument executing mechanism M is separated from the joint driving mechanism N. Meanwhile, two positioning bosses on the base shell 1_3_1 can position and fix the surgical instrument executing mechanism M;
When the surgical instrument executing mechanism M is separated from the joint driving mechanism N, the two locking hooks 1_3_3_1 and 1_3_3_2 on the two base outer covers 1_3_2 are rotated respectively, so that the grooves on the locking hooks 1_3_3_1 and 1_3_3_2 are separated from the bosses on the corresponding positions on the outer cover of the surgical instrument executing mechanism M, the surgical instrument executing mechanism M slides out of the base outer cover 1_3_2 from the top end of the guide chute on the base outer cover 1_3_2 and the bottom of the middle part of the guide chute in a horn shape, and the surgical instrument executing mechanism M is separated from the joint driving mechanism N.
Example 2
The present embodiment will be described with reference to fig. 10 to 13, in which the layout of the quick-change mechanism for mechanical decoupling of the minimally invasive surgical single-hole surgical robot can be changed to the structure of fig. 10 to 13 based on the technical solution of the first embodiment. Namely, the layout of the quick-change mechanism for mechanical decoupling of the minimally invasive surgical single-hole surgical robot in the technical scheme of the first embodiment is adjusted to the technical scheme of the second embodiment, and meanwhile, the layout of the transmission box of the surgical instrument executing mechanism M is also adjusted to the technical scheme of the second embodiment, so that the mechanical decoupling can be correctly driven.
The quick-change mechanism N for mechanical decoupling of the minimally invasive surgery single-hole surgical robot can be applied to driving and mechanical decoupling of double-head instruments, such as clamping instruments and shearing instruments, and the eighth joint driving mechanism 8 of the quick-change mechanism for mechanical decoupling of the minimally invasive surgery single-hole surgical robot is omitted, as shown in fig. 4 and 5, and the quick-change mechanism for mechanical decoupling of the minimally invasive surgery single-hole surgical robot can be applied to driving and mechanical decoupling of single-head instruments, such as cutting instruments and 30-degree cavity mirror instruments. The seventh joint driving mechanism 7 and the eighth joint driving mechanism 8 of the mechanical decoupling quick-change mechanism for the minimally invasive single-hole surgical robot are omitted, and the mechanical decoupling quick-change mechanism for the minimally invasive single-hole surgical robot can be applied to driving and mechanical decoupling of 360-degree endoscopic instruments.
The foregoing description of the preferred embodiments of the invention is not intended to be limiting, but rather to enable any modification, equivalent replacement, improvement or the like to be made within the spirit and principles of the invention.
While the foregoing description of the embodiments of the present invention has been presented in conjunction with the drawings, it should be understood that it is not intended to limit the scope of the invention, but rather, it is intended to cover all modifications or variations within the scope of the invention as defined by the claims of the present invention.

Claims (8)

Translated fromChinese
1.用于单孔手术机器人的机械解耦的快换机构,其特征在于,包括一个固定座,在所述的固定座上安装有第一、第二、第三、第四、第五、第六、第七和第八关节驱动机构;1. A quick-change mechanism for mechanical decoupling of a single-port surgical robot, characterized in that it comprises a fixed seat, on which are mounted first, second, third, fourth, fifth, sixth, seventh and eighth joint drive mechanisms;所述的第一、第二、第三、第四、第五、第六、第七和第八关节驱动机构安装在同一个底座上,所述的第一、第二、第三、第四、第五、第六、第七和第八关节驱动机构各自通过一个接口离合盘与所述的手术执行器械相连;The first, second, third, fourth, fifth, sixth, seventh and eighth joint drive mechanisms are installed on the same base, and the first, second, third, fourth, fifth, sixth, seventh and eighth joint drive mechanisms are each connected to the surgical execution instrument via an interface clutch disk;所述的第一、第二、第三、第四、第五、第六、第七和第八关节驱动机构通过钢丝绳分别对应驱动手术器械执行机构M的第一、第二、第三、第四、第五、第六、第七和第八关节执行机构的旋转;The first, second, third, fourth, fifth, sixth, seventh and eighth joint driving mechanisms respectively drive the rotation of the first, second, third, fourth, fifth, sixth, seventh and eighth joint actuators of the surgical instrument actuator M through steel wire ropes;所述的第一关节驱动机构包括一个电机,该电机驱动齿轮轴旋转相连,所述的齿轮轴和与其相对应的接口离合盘相连;The first joint driving mechanism includes a motor, which drives a gear shaft to rotate and connect, and the gear shaft is connected to a corresponding interface clutch disk;所述的第二、第三、第四、第五和第六关节驱动机构的结构相同,各自包括一个电机,该电机驱动太阳轮轴旋转,在所述的太阳轮轴上安装有大太阳轮和小太阳轮,大太阳轮和小太阳轮与安装在行星架齿轮轴上的三个行星轮啮合,三个行星轮与小太阳轮外啮合,三个行星轮与大太阳轮内啮合,三个行星轮围绕太阳轮轴轴线均布,所述的行星架齿轮轴和与其相对应的接口离合盘相连;The second, third, fourth, fifth and sixth joint drive mechanisms have the same structure, and each includes a motor, which drives the sun gear shaft to rotate, and a large sun gear and a small sun gear are installed on the sun gear shaft, and the large sun gear and the small sun gear are meshed with three planetary gears installed on the planetary carrier gear shaft, and the three planetary gears are externally meshed with the small sun gear, and the three planetary gears are internally meshed with the large sun gear, and the three planetary gears are evenly distributed around the axis of the sun gear shaft, and the planetary carrier gear shaft is connected to the interface clutch disk corresponding thereto;所述的第七和第八关节驱动机构的结构相同,各自包括一个电机,该电机驱动太阳轮轴旋转,在所述的太阳轮轴上安装有大太阳轮和小太阳轮,大太阳轮和小太阳轮与安装在行星架上的三个行星轮啮合,三个行星轮与小太阳轮外啮合,三个行星轮与大太阳轮内啮合,三个行星轮围绕太阳轮轴轴线均布,所述的行星架和与其相对应的接口离合盘相连;The seventh and eighth joint drive mechanisms have the same structure, each comprising a motor, which drives the sun gear shaft to rotate, on which a large sun gear and a small sun gear are mounted, the large sun gear and the small sun gear are meshed with three planetary gears mounted on a planetary carrier, the three planetary gears are externally meshed with the small sun gear, the three planetary gears are internally meshed with the large sun gear, the three planetary gears are evenly distributed around the axis of the sun gear shaft, and the planetary carrier is connected to an interface clutch disc corresponding thereto;所述的第一、第二、第三、第四、第五和第六关节驱动机构之间均安装有一个过渡齿轮轴;所述的第六与第七关节驱动机构和所述的第八关节驱动机构之间分别安装有一个过渡齿轮轴;所述的第七和所述的第八关节驱动机构之间没有安装过渡齿轮轴;A transition gear shaft is installed between the first, second, third, fourth, fifth and sixth joint drive mechanisms; a transition gear shaft is installed between the sixth and seventh joint drive mechanisms and the eighth joint drive mechanism respectively; no transition gear shaft is installed between the seventh and eighth joint drive mechanisms;所述的第一关节驱动机构的齿轮轴与所述的第一、第二关节驱动机构之间的过渡齿轮轴外啮合,所述的第一、第二关节驱动机构之间的过渡齿轮轴与所述的第二关节驱动机构的大太阳轮外啮合;The gear shaft of the first joint drive mechanism is externally meshed with the transition gear shaft between the first and second joint drive mechanisms, and the transition gear shaft between the first and second joint drive mechanisms is externally meshed with the large sun gear of the second joint drive mechanism;所述的第二关节驱动机构的行星架齿轮轴与所述的第二、第三关节驱动机构之间的过渡齿轮轴外啮合,所述的第二、第三关节驱动机构之间的过渡齿轮轴与所述的第三关节驱动机构的大太阳轮外啮合;所述的第三关节驱动机构的行星架齿轮轴与所述的第三、第四关节驱动机构之间的过渡齿轮轴外啮合,所述的第三、第四关节驱动机构之间的过渡齿轮轴与所述的第四关节驱动机构的大太阳轮外啮合;所述的第四关节驱动机构的行星架齿轮轴与所述的第四、第五关节驱动机构之间的过渡齿轮轴外啮合,所述的第四、第五关节驱动机构之间的过渡齿轮轴与所述的第五关节驱动机构的大太阳轮外啮合;所述的第五关节驱动机构的行星架齿轮轴与所述的第五、第六关节驱动机构之间的过渡齿轮轴外啮合,所述的第五、第六关节驱动机构之间的过渡齿轮轴与所述的第六关节驱动机构的大太阳轮外啮合;所述的第六关节驱动机构的行星架齿轮轴与所述的第六、第七关节驱动机构之间的过渡齿轮轴外啮合,所述的第六、第七关节驱动机构之间的所述的过渡齿轮轴与所述的第七关节驱动机构的大太阳轮外啮合;所述的第六关节驱动机构的行星架齿轮轴与所述的第六、第八关节驱动机构之间的所述的过渡齿轮轴外啮合,所述的第六、第八关节驱动机构之间的所述的过渡齿轮轴与所述的第八关节驱动机构的大太阳轮外啮合。The planetary carrier gear shaft of the second joint drive mechanism is externally meshed with the transition gear shaft between the second and third joint drive mechanisms, and the transition gear shaft between the second and third joint drive mechanisms is externally meshed with the large sun gear of the third joint drive mechanism; the planetary carrier gear shaft of the third joint drive mechanism is externally meshed with the transition gear shaft between the third and fourth joint drive mechanisms, and the transition gear shaft between the third and fourth joint drive mechanisms is externally meshed with the large sun gear of the fourth joint drive mechanism; the planetary carrier gear shaft of the fourth joint drive mechanism is externally meshed with the transition gear shaft between the fourth and fifth joint drive mechanisms, and the transition gear shaft between the fourth and fifth joint drive mechanisms is externally meshed with the large sun gear of the fifth joint drive mechanism; The planetary carrier gear shaft of the five-joint drive mechanism is externally meshed with the transition gear shaft between the fifth and sixth joint drive mechanisms, and the transition gear shaft between the fifth and sixth joint drive mechanisms is externally meshed with the large sun gear of the sixth joint drive mechanism; the planetary carrier gear shaft of the sixth joint drive mechanism is externally meshed with the transition gear shaft between the sixth and seventh joint drive mechanisms, and the transition gear shaft between the sixth and seventh joint drive mechanisms is externally meshed with the large sun gear of the seventh joint drive mechanism; the planetary carrier gear shaft of the sixth joint drive mechanism is externally meshed with the transition gear shaft between the sixth and eighth joint drive mechanisms, and the transition gear shaft between the sixth and eighth joint drive mechanisms is externally meshed with the large sun gear of the eighth joint drive mechanism.2.如权利要求1所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,所述的第一关节驱动机构的齿轮轴两端通过轴承轴向固定,轴承固定在底座上;所述的第二、第三、第四、第五和第六关节驱动机构的所述的行星架齿轮轴一端伸出三个销轴,行星架齿轮轴的三个销轴分别插入三个行星轮的中心孔中,行星架齿轮轴一端通过轴承轴向固定,行星架齿轮轴另一端通过三个行星轮轴向固定,太阳轮轴和大太阳轮两端分别通过轴承轴向固定,其中一个轴承固定在太阳轮轴和大太阳轮上,另外两个轴承固定在底座上,行星架齿轮轴的一端与接口离合盘形成过盈配合; 所述的第七和第八关节驱动机构的所述的行星架一端伸出三个销轴,行星架的三个销轴分别插入三个行星轮的中心孔中,行星架一端通过轴承轴向固定,行星架另一端通过三个行星轮轴向固定,太阳轮轴和大太阳轮两端分别通过轴承轴向固定,其中一个轴承固定在太阳轮轴和大太阳轮上,另外两个轴承固定在底座上,行星架的一端与接口离合盘形成过盈配合; 所述的第一、第二、第三、第四、第五和第六关节驱动机构之间及所述的第六关节驱动机构与所述的第七关节驱动机构和所述的第八关节驱动机构之间安装的过渡齿轮轴两端通过轴承轴向固定,轴承固定在底座上。2. The quick-change mechanism for mechanical decoupling of a single-port surgical robot as described in claim 1 is characterized in that both ends of the gear shaft of the first joint drive mechanism are axially fixed by bearings, and the bearings are fixed on the base; three pins extend from one end of the planetary carrier gear shaft of the second, third, fourth, fifth and sixth joint drive mechanisms, and the three pins of the planetary carrier gear shaft are respectively inserted into the center holes of the three planetary gears, one end of the planetary carrier gear shaft is axially fixed by the bearing, and the other end of the planetary carrier gear shaft is axially fixed by the three planetary gears, and both ends of the sun gear shaft and the large sun gear are axially fixed by bearings respectively, one of the bearings is fixed on the sun gear shaft and the large sun gear, and the other two bearings are fixed on the base, and one end of the planetary carrier gear shaft forms an interference fit with the interface clutch disk; Three pins extend from one end of the planetary carrier of the seventh and eighth joint drive mechanisms, and the three pins of the planetary carrier are respectively inserted into the center holes of the three planetary gears. One end of the planetary carrier is axially fixed by a bearing, and the other end of the planetary carrier is axially fixed by the three planetary gears. Both ends of the sun gear shaft and the large sun gear are axially fixed by bearings respectively, one of the bearings is fixed on the sun gear shaft and the large sun gear, and the other two bearings are fixed on the base, and one end of the planetary carrier forms an interference fit with the interface clutch disk; Both ends of the transition gear shaft installed between the first, second, third, fourth, fifth and sixth joint drive mechanisms and between the sixth joint drive mechanism and the seventh joint drive mechanism and the eighth joint drive mechanism are axially fixed by bearings, and the bearings are fixed on the base.3.如权利要求1所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,所述的第二、第三、第四、第五、第六、第七和第八关节驱动机构的所述的小太阳轮与太阳轮轴截面呈“D”字形,小太阳轮与太阳轮轴的“D”字形截面形成过盈配合,小太阳轮与太阳轮轴通过 “D”字形截面周向固定。3. The mechanically decoupled quick-change mechanism for a single-port surgical robot as described in claim 1 is characterized in that the small sun gear and the sun gear shaft cross-section of the second, third, fourth, fifth, sixth, seventh and eighth joint drive mechanisms are in a "D" shape, and the "D"-shaped cross-section of the small sun gear and the sun gear shaft forms an interference fit, and the small sun gear and the sun gear shaft are circumferentially fixed by the "D"-shaped cross-section.4.如权利要求1所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,所述的第一、第二、第三、第四、第五、第六在所述的底座上单列依次串联布置;第七关节驱动机构和第八关节驱动机构与第六关节驱动机构在所述的底座上并联布置。4. The mechanically decoupled quick-change mechanism for a single-port surgical robot as described in claim 1 is characterized in that the first, second, third, fourth, fifth, and sixth joints are arranged in series in a single row on the base; the seventh joint drive mechanism and the eighth joint drive mechanism are arranged in parallel with the sixth joint drive mechanism on the base.5.如权利要求1所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,进一步的,所述的底座包括底座壳体和底座外罩,所述的底座壳体上设有两道定位凸台,底座壳体两侧面分别设有两个长螺栓孔,所述的长螺栓孔与底座外罩相连。5. The quick-change mechanism for mechanical decoupling of a single-port surgical robot as described in claim 1 is characterized in that, further, the base includes a base shell and a base cover, the base shell is provided with two positioning bosses, and two long bolt holes are respectively provided on both sides of the base shell, and the long bolt holes are connected to the base cover.6.如权利要求5所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,所述的底座外罩有两个,分别安装并固定于底座壳体的两侧;底座外罩上面设计导向滑槽,导向滑槽顶端呈“喇叭口”形状,以方便手术器械执行机构的安装,底座外罩上面导向滑槽末端及中部槽底呈“圆弧”形,导向滑槽末端及中部的“圆弧”形滑槽槽底开口方向与导向滑槽轴线方向垂直,并且该“圆弧”形的导向滑槽末端及中部槽底与手术器械执行机构的固定销轴形成“过盈”配合。6. The mechanically decoupled quick-change mechanism for a single-port surgical robot as described in claim 5 is characterized in that there are two base covers, which are respectively installed and fixed on both sides of the base shell; a guide groove is designed on the base cover, and the top of the guide groove is in a "trumpet" shape to facilitate the installation of the surgical instrument actuator, and the end and middle groove bottom of the guide groove on the base cover are in an "arc" shape, and the opening direction of the end and middle "arc" groove bottom of the guide groove is perpendicular to the axial direction of the guide groove, and the end and middle groove bottom of the "arc" shaped guide groove form an "interference" fit with the fixed pin shaft of the surgical instrument actuator.7.如权利要求6所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,手术器械执行机构能沿底座外罩上面的导向滑槽安装到快换机构上;底座外罩上设计有两个长螺栓孔,底座外罩上面的两个长螺栓孔与底座壳体上面的长螺栓孔长孔轴线垂直,方便底座外罩安装并固定于底座壳体上时调整底座外罩与底座壳体的安装相对位置。7. The mechanically decoupled quick-change mechanism for a single-port surgical robot as described in claim 6 is characterized in that the surgical instrument actuator can be installed on the quick-change mechanism along the guide groove on the base cover; two long bolt holes are designed on the base cover, and the two long bolt holes on the base cover are perpendicular to the long hole axes of the long bolt holes on the base shell, so as to facilitate the adjustment of the relative installation position of the base cover and the base shell when the base cover is installed and fixed on the base shell.8.如权利要求6所述的用于单孔手术机器人的机械解耦的快换机构,其特征在于,所述底座,还包括一个用于将手术器械执行机构固定到所述底座上的锁紧机构;所述的锁紧机构包括两组,每组包括一个锁紧挂钩,两个锁紧挂钩的一端旋转安装在同一个底座外罩上,锁紧挂钩另一端设有凹槽,手术器械执行机构外壳上对应位置设有凸台,锁紧挂钩上面的凹槽与手术器械执行机构外壳上对应位置的凸台配合用于固定手术器械执行机构。8. The mechanically decoupled quick-change mechanism for a single-port surgical robot as described in claim 6 is characterized in that the base also includes a locking mechanism for fixing the surgical instrument actuator to the base; the locking mechanism includes two groups, each group includes a locking hook, one end of the two locking hooks is rotatably mounted on the same base cover, the other end of the locking hook is provided with a groove, and a boss is provided at a corresponding position on the outer shell of the surgical instrument actuator, and the groove on the locking hook cooperates with the boss at a corresponding position on the outer shell of the surgical instrument actuator to fix the surgical instrument actuator.
CN201810177475.6A2018-03-022018-03-02 A quick-change mechanism for mechanical decoupling of a single-port surgical robotActiveCN108451642B (en)

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