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CN119196243A - A variable damping mechanism and a drone recovery device having the same - Google Patents

A variable damping mechanism and a drone recovery device having the same
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Publication number
CN119196243A
CN119196243ACN202411299542.3ACN202411299542ACN119196243ACN 119196243 ACN119196243 ACN 119196243ACN 202411299542 ACN202411299542 ACN 202411299542ACN 119196243 ACN119196243 ACN 119196243A
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CN
China
Prior art keywords
elastic part
folding
unmanned aerial
recovery
aerial vehicle
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Pending
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CN202411299542.3A
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Chinese (zh)
Inventor
李国平
张爽
杨北京
孙正金
侯佳乐
付晓龙
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Harbin Institute of Technology Shenzhen
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Harbin Institute of Technology Shenzhen
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Application filed by Harbin Institute of Technology ShenzhenfiledCriticalHarbin Institute of Technology Shenzhen
Priority to CN202411299542.3ApriorityCriticalpatent/CN119196243A/en
Publication of CN119196243ApublicationCriticalpatent/CN119196243A/en
Pendinglegal-statusCriticalCurrent

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Abstract

The invention provides a variable damping mechanism and an unmanned aerial vehicle recovery device with the same, and belongs to the field of unmanned aerial vehicle recovery. The problem that the traditional damping structure occupies a large space, has power requirements and can be greatly influenced by heating when the traditional unmanned aerial vehicle recovery device is used is solved. A variable damping mechanism comprises a flexible elastic part and a scroll elastic part, wherein the flexible elastic part is integrally in a rope shape, one end of the flexible elastic part is a free end, the scroll elastic part is integrally coiled and is provided with a fixed end and an extension end, and the extension end is connected with the other end of the flexible elastic part, wherein the free end is used for pulling the flexible elastic part to deform to a certain extent when being coupled with an unmanned aerial vehicle and then driving the extension end of the scroll elastic part to act. It is mainly used unmanned aerial vehicle retrieves.

Description

Variable damping mechanism and unmanned aerial vehicle recovery unit who has it
Technical Field
The invention belongs to the field of unmanned aerial vehicle recovery, and particularly relates to a variable damping mechanism and an unmanned aerial vehicle recovery device with the same.
Background
Along with the wide application of the high and new technology on weaponry, the development technology of the unmanned aerial vehicle also makes breakthrough progress, and the unmanned aerial vehicle technology has the characteristics of no casualties, less use limit, high concealment, high efficiency and cost ratio and the like. The military unmanned aerial vehicle has increasingly prominent status and function in modern war, and can be used for battlefield reconnaissance, air monitoring, electronic countermeasure, ground attack and the like, wherein the fixed-wing unmanned aerial vehicle has high flight speed and long endurance time, and is suitable for long-distance continuous work. However, the massive use of unmanned aerial vehicles also brings about a breakthrough problem, such as recovery of unmanned aerial vehicles. The ground and ship recovery modes of the small fixed wing unmanned aerial vehicle mainly comprise a parachute recovery mode, a net collision recovery mode, a wing line collision recovery mode, a net compound machine back overhead hook line collision recovery mode and the like. The recovery system of the net compound machine back overhead hook wire collision type ground and the ship-based small unmanned aerial vehicle has the advantages of low requirement on wing strength and capability of avoiding damage to sensitive equipment at the front end of the unmanned aerial vehicle.
At present, retrieve the support volume great in the compound recovery system of wire net, the transportation degree of difficulty is higher, the installation rate is slower, the installation degree of difficulty is higher, occupation space is great when not having recovery task, this recovery unit prevents through the elastic rope that unmanned aerial vehicle from receiving too big impact load and transshipping, elastic rope and wind spring combination provide variable damping simultaneously and absorb unmanned aerial vehicle kinetic energy, resolution formula recovery support can expand fast, compare in traditional recovery system, have that recovery environment requires is low, need not the electric power requirement, the transportation is swift, expand rapidly, occupation space is few when no recovery task, it is significant to need frequent conversion recovery place and the abominable condition of recovery place condition.
Disclosure of Invention
In view of the above, the invention aims to provide a variable damping mechanism and an unmanned aerial vehicle recovery device with the same, so as to solve the problems that the traditional damping structure occupies a large space, has power requirements and is greatly influenced by heat energy when the traditional unmanned aerial vehicle recovery device is used.
To achieve the above object, according to one aspect of the present invention, there is provided a variable damping mechanism comprising:
a flexible elastic part which is rope-shaped as a whole and one end of which is a free end;
The scroll elastic part is integrally coiled and provided with a fixed end and an extension end, and the extension end is connected with the other end of the flexible elastic part, wherein the free end is used for pulling the flexible elastic part to perform certain deformation when being coupled with the unmanned aerial vehicle and then driving the extension end of the scroll elastic part to act.
Further, the flexible elastic portion is an elastic rope.
Further, the scroll spring is a scroll spring damper.
According to another aspect of the present invention, there is provided an unmanned aerial vehicle recovery device comprising a variable damping mechanism as described above, further comprising:
the variable damping mechanism is fixed on the mobile vehicle;
The capturing net is arranged on the mobile vehicle, and the variable damping mechanism and the capturing net are sequentially arranged at intervals along the flight direction of the unmanned aerial vehicle.
Still further, the capture web is disposed perpendicular to the horizontal plane.
Still further, the recycling apparatus further includes:
the rotating end is used for rotating in the horizontal direction;
The fixed end of the amplitude changing device is connected with the rotating end of the rotary platform;
The telescopic lifting device is characterized in that the fixed end of the telescopic lifting device is connected with the amplitude changing end of the amplitude changing device, the telescopic end of the telescopic lifting device is connected with one end of the folding and unfolding driving mechanism, the middle part of the telescopic end of the telescopic lifting device is pivoted with the mechanical arm, the movable end of the mechanical arm is connected with the other end of the folding and unfolding driving mechanism and used for leveling the folding and unfolding driving mechanism, and the folding and unfolding driving mechanism is connected with the foldable recovery slideway and used for controlling folding and unfolding of the foldable recovery slideway.
Still further, the foldable recovery slideway comprises two split slideways, the folding driving mechanism is provided with two symmetrically arranged rotating ends, each split slideway is connected with the corresponding folding driving mechanism rotating end, and when the two rotating ends of the folding driving mechanism rotate, the two split slideways are driven to be in butt joint or separation.
Compared with the prior art, the invention has the beneficial effects that:
1. The variable damping mechanism can form a two-stage deceleration structure through the arrangement of the flexible elastic part and the scroll elastic part, the flexible elastic part can prevent the unmanned aerial vehicle from being overloaded due to overlarge impact load, meanwhile, the combination of the flexible elastic part and the scroll elastic part can provide variable damping to absorb the kinetic energy of the unmanned aerial vehicle, so that the variable damping mechanism is higher in safety, better in practicability, free from heating phenomenon, low in manufacturing cost and high in reliability, and a traditional electronic power structure is omitted;
2. The recovery device adopts a form of a mobile vehicle, and can be adjusted according to the flight condition of the unmanned aerial vehicle to complete corresponding coordination, so that the maneuverability of the recovery device is improved, and the recovery device has important significance for the conditions of frequent conversion of recovery places and severe conditions of the recovery places;
3. This recovery unit can save space through setting up the collapsible recovery slide that can roll over when not using, can form the slide to supply with unmanned aerial vehicle and retrieve the time slide when expanding, and cooperation variable damping mechanism can reduce unmanned aerial vehicle's kinetic energy better to form better recovery effect.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the invention. In the drawings:
Fig. 1 is a schematic diagram of the overall structure of an unmanned aerial vehicle recovery device according to the present invention;
FIG. 2 is a top plan view relative position layout of the telescopic lifting device, the foldable recovery slide and the folding and unfolding drive mechanism of the present invention;
FIG. 3 is a side view of FIG. 2 according to the present invention;
FIG. 4 is a relative positioning of the elastic cord, wrap spring damper and capture net of the present invention;
fig. 5 is a schematic view of a scroll spring damper according to the present invention.
The device comprises a mobile vehicle 1, a rotating platform 2, a luffing device 3, a telescopic lifting device 4, a mechanical arm 4-1, a foldable recovery slideway 5, a folding driving mechanism 6, a driving module 6-1, a connecting piece 6-2, an unmanned aerial vehicle back hook 7, an elastic rope 8, a spiral spring damper 9 and a capturing net 10.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. It should be noted that, in the case of no conflict, embodiments of the present invention and features of the embodiments may be combined with each other, and the described embodiments are only some embodiments of the present invention, not all embodiments.
It should be noted that, the descriptions of the directions of "left", "right", "upper", "lower", "top", "bottom", and the like of the present invention are defined based on the relation of orientations or positions shown in the drawings, and are only for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the structures must be constructed and operated in a specific orientation, and thus, the present invention should not be construed as being limited thereto. In the description of the present invention, the meaning of "plurality" is two or more unless specifically defined otherwise.
In the description of the present invention, unless explicitly stated and limited otherwise, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected, directly connected, indirectly connected through intervening mediums, or may be in communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
Referring to the drawings illustrating the present embodiment, according to one aspect of the present invention, there is provided a variable damping mechanism comprising:
The flexible elastic part is integrally rope-shaped, one end of the flexible elastic part is a free end, and the flexible elastic part is arranged to be capable of carrying out primary speed reduction on the unmanned aerial vehicle and bearing corresponding load in an initial stage so as to help the unmanned aerial vehicle to reduce speed.
The scroll elastic part is integrally coiled and provided with a fixed end and an extension end, and the extension end is connected with the other end of the flexible elastic part, wherein the free end is used for pulling the flexible elastic part to perform certain deformation when being coupled with the unmanned aerial vehicle and then driving the extension end of the scroll elastic part to act. The scroll spring is provided to reduce the volume of the occupied space in a limited space, and any spring having a space-saving and no electric power-performing member may be used in the present application.
In this embodiment, the flexible elastic portion is an elastic cord 8. The elastic rope 8 is a conventional component, is easily available and low in cost, can bear impact load in unmanned aerial vehicle recovery and ensures reasonable service life and reliability, and can be used in the application.
In this embodiment, the wrap spring is a wrap spring damper 9. The spiral spring damper 9 has a good space solving effect, is tightened after being stretched, generates moment due to angular deformation, and accordingly converts kinetic energy of the aircraft into elastic potential energy and reduces speed. The scroll spring damper 9 and the elastic rope 8 are matched, so that a variable damping structure can be formed, no overload phenomenon is caused in the whole recovery process of the unmanned aerial vehicle, and the recovery stability is ensured. In the spiral spring damper 9, as shown in fig. 5, one end of the spiral spring is fixed, and the other end is connected with one end of the elastic rope 8, in order to achieve a good recovery effect, the unmanned aerial vehicle back hook 7 needs to be installed on the unmanned aerial vehicle, and in order to achieve the elastic rope 8, a hook structure matched with the unmanned aerial vehicle back hook 7 or a structure such as a circular ring shape which is beneficial to the hooking of the unmanned aerial vehicle back hook 7 can be arranged at the other end, so that the recovery accuracy is improved.
According to another aspect of the present invention, there is provided an unmanned aerial vehicle recovery device comprising a variable damping mechanism as described above, further comprising:
The movable vehicle 1 is fixed on the movable vehicle 1, and the movable vehicle 1 is arranged to improve the recycling mobility, and in the operation process of the unmanned aerial vehicle, the movable damping mechanism is arranged on the movable vehicle 1 along with the use scene of the change of the operation place and the recycling place, so that the recycling mobility can be improved, the recycling difficulty of the unmanned aerial vehicle is reduced, meanwhile, the unmanned aerial vehicle can return in time when the cruising is insufficient, the falling event caused by insufficient electric quantity is avoided, and the operation safety is improved.
The capturing net 10 is arranged on the mobile vehicle 1, and the variable damping mechanism and the capturing net 10 are sequentially arranged at intervals along the flight direction of the unmanned aerial vehicle. The setting of catching net 10 can cooperate with the variable damping mechanism, forms the second protection that unmanned aerial vehicle retrieved and safety recovery unmanned aerial vehicle.
In this embodiment, the capturing net 10 has a net surface arranged perpendicular to the horizontal plane. The net surface of the capturing net 10 is oriented, so that the unmanned aerial vehicle can be better recovered, the contact area is enlarged, and the operation difficulty of an unmanned aerial vehicle operator is reduced. The specific fixing form of the capturing net 10 can be reasonably selected according to the actual mobile car 1, and can be fixed on the mobile car 1 through a bracket or can be mounted on a folding recovery slideway 5 mentioned later. The fixing form can be fixed with the corresponding bracket by adopting a mode of arranging binding ropes at four corners. Any capturing net 10 that can be recovered in combination with the folding recovery chute 5 can be used in the present application, as appropriate and chosen according to the actual needs.
In this embodiment, the recycling apparatus further includes:
The rotary platform 2 is arranged to reasonably adjust the position of the foldable recovery slideway 5 in the horizontal plane, the rotary platform 2 adopts the existing recovery platform, and the rotary platform with the rotary end rotating in the horizontal plane can be used in the application. For the rotary platform 2, the driving mode of the rotating end can be selected by combining a motor with a speed reducer to drive the rotating end to rotate, the power supply mode can be connected with a power supply module of the mobile vehicle 1 to supply power according to actual conditions, for example, a storage battery or a vehicle-mounted battery, and the like, and the connection mode can be selected according to the actual conditions in the prior art.
The fixed end of the amplitude changing device 3 is connected with the rotating end of the rotating platform 2, and the amplitude changing device 3 is arranged to change the working amplitude of the telescopic lifting device 4 through the amplitude changing device 3 after the rotating platform 2 adjusts the horizontal position, and an existing swing arm type amplitude changing mechanism is adopted, so that the fixed end of the swing arm type amplitude changing mechanism is connected with the rotating end of the rotating platform 2, the rotating platform 2 can adjust the position of the operating end of the swing arm of the amplitude changing device 3 in the horizontal direction, and the amplitude changing device can be transplanted to the application for use in a preferable mode by referring to the rotating structure and the amplitude changing structure of a crane.
The telescopic lifting device 4 is characterized in that a fixed end of the telescopic lifting device 4 is connected with an amplitude changing end of the amplitude changing device 3, the telescopic end is connected with one end of the folding and unfolding driving mechanism 6, the middle part of the telescopic end is pivoted with the mechanical arm 4-1, a movable end of the mechanical arm 4-1 is connected with the other end of the folding and unfolding driving mechanism 6 and is used for leveling the folding and unfolding driving mechanism 6, and the folding and unfolding driving mechanism 6 is connected with the foldable recovery slideway 5 and is used for controlling folding and unfolding of the foldable recovery slideway 5. The telescopic lifting device 4 is arranged to further adjust the position of the folding driving mechanism 6 on the premise of adjusting the positions of the rotary platform 2 and the amplitude changing device 3, so that the position of the foldable recovery slideway 5 is adjusted, and a precondition is provided for the recovery unmanned aerial vehicle to carry out flexible adaptability adjustment to the greatest extent. The telescopic lifting device 4 can adopt a hydraulic cylinder type telescopic structure, can also adopt a ball screw to drive the sliding block, and can be connected with the telescopic end and the sliding block, and the telescopic lifting device is selected according to actual needs. The general principle of use is that the fixed end is connected to the amplitude changing end of the amplitude changing device 3, and the energy supply mode adopts a vehicle-mounted energy supply mode as well. The mechanical arm 4-1 specifically adopts a hydraulic cylinder mode, and the movable end is connected with the folding and unfolding driving mechanism 6, so that the angle between the folding and unfolding driving mechanism 6 and the horizontal plane can be adjusted in the action process of the movable end of the mechanical arm 4-1 until the folding and unfolding driving mechanism 6 is in a horizontal state, and the adjustment is finished.
In this embodiment, the foldable recovery slide 5 includes two split slides, the folding driving mechanism 6 has two symmetrically arranged rotating ends, each split slide is connected to the corresponding rotating end of the folding driving mechanism 6, and when the two rotating ends of the folding driving mechanism 6 rotate, the two split slides are driven to be butted or separated. The split slide way is connected with the driving module 6-1 through the connecting piece 6-2, the connecting piece 6-2 can be driven to act through the driving module 6-1, so that the corresponding split slide way is driven to act, in the application, under the conventional form, the two split slide ways are in a separated form and are mutually parallel to be arranged at two sides of the folding and unfolding driving mechanism 6, when each driving module 6-1 drives the connecting piece 6-2 to rotate 90 degrees, the two split sliding ways are spliced to form a complete sliding way, and the variable damping mechanism and the capturing net 10 are connected to the same split sliding way or different split sliding ways respectively, and the variable damping mechanism and the capturing net are selected according to actual needs. The driving module 6-1 can specifically adopt a motor acceleration and deceleration device to drive the connecting piece 6-2. Compared with the traditional recovery system, the resolution type recovery support formed by the rotary platform 2, the amplitude changing device 3 and the telescopic lifting device 4 can be quickly unfolded, has the advantages of low recovery environment requirement, no need of electric power requirement, quick transportation, quick unfolding, small occupied space when no recovery task is needed, and the like, and has important significance for the conditions of frequent conversion of recovery sites and severe recovery site conditions.
When the unmanned aerial vehicle is used, after the form of the mobile vehicle 1 reaches a designated place, the rotating end of the rotating platform 2 is operated to rotate to adjust the horizontal position, then the space position is adjusted through the amplitude changing device 3, then the position in the vertical direction is adjusted through the telescopic lifting device 4, the folding and unfolding driving mechanism 6 is adjusted to be in a horizontal state through the mechanical arm 4-1, the folding and unfolding slideway 5 is kept horizontal at the moment, then the driving module 6-1 is operated to drive the split slideway to be combined into a whole through the connecting piece 6-2, the recycling condition is provided, after the unmanned aerial vehicle flies, the back-to-the-head hook 7 hooks the elastic rope 8, then the elastic rope 8 is pulled, the elastic rope 8 stretches to a certain extent, and then the extending end of the scroll spring damper 9 is driven to act, and the unmanned aerial vehicle is tightened into the capturing net 10 to complete recycling of the unmanned aerial vehicle. The elastic rope and coil spring combined type variable damping unmanned aerial vehicle recovery device adopts the plane non-contact scroll spring to replace a brake to play a braking role, so that the heat accumulation problem can not exist, the structure is simple, the maintenance cost is low, meanwhile, electric power intervention is not needed, and the problem of large volume of the linear spring is solved.
The controllers, sensors, control programs, etc. that may be involved in the above description are all of the prior art, and are not described in detail.
The embodiments of the invention disclosed above are intended only to help illustrate the invention. The examples are not intended to be exhaustive or to limit the invention to the precise forms disclosed. Many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and the practical application, to thereby enable others skilled in the art to best understand and utilize the invention.

Claims (7)

Translated fromChinese
1.一种可变阻尼机构,其特征在于,包括:1. A variable damping mechanism, comprising:柔性弹性部,整体呈绳索状,一端为自由端;The flexible elastic part is in the shape of a rope as a whole, and one end is a free end;涡卷弹性部,整体成盘卷状且设置有固定端和伸长端,伸长端与所述柔性弹性部的另一端相连,其中,所述自由端用于与无人机耦合时拉动柔性弹性部进行一定形变后带动涡卷弹性部的伸长端动作。The scroll elastic part is in a coiled shape as a whole and is provided with a fixed end and an extension end, wherein the extension end is connected to the other end of the flexible elastic part, wherein the free end is used to pull the flexible elastic part to undergo a certain deformation when coupled with the drone, thereby driving the extension end of the scroll elastic part to move.2.根据权利要求1所述的一种可变阻尼机构,其特征在于:所述柔性弹性部为弹性绳(8)。2. A variable damping mechanism according to claim 1, characterized in that the flexible elastic part is an elastic rope (8).3.根据权利要求1所述的一种可变阻尼机构,其特征在于:所述涡卷弹性部为涡卷弹簧阻尼器(9)。3. A variable damping mechanism according to claim 1, characterized in that the scroll elastic portion is a scroll spring damper (9).4.一种无人机回收装置,包括如权利要求1-3中任一项所述的一种可变阻尼机构,其特征在于,还包括:4. A drone recovery device, comprising a variable damping mechanism as claimed in any one of claims 1 to 3, characterized in that it also includes:移动车(1),所述可变阻尼机构固定在移动车(1)上;A moving vehicle (1), wherein the variable damping mechanism is fixed on the moving vehicle (1);捕获网(10),设置在移动车(1)上,所述可变阻尼机构和捕获网(10)沿无人机飞行方向顺次间隔布置。The capture net (10) is arranged on the mobile vehicle (1), and the variable damping mechanism and the capture net (10) are sequentially arranged at intervals along the flight direction of the drone.5.根据权利要求4所述的一种无人机回收装置,其特征在于:所述捕获网(10)网面垂直于水平面布置。5. A drone recovery device according to claim 4, characterized in that the surface of the capture net (10) is arranged perpendicular to the horizontal plane.6.根据权利要求4所述的一种无人机回收装置,其特征在于,所述回收装置还包括:6. The drone recovery device according to claim 4, characterized in that the recovery device further comprises:回转平台(2),固定端与移动车(1)相连,转动端用于水平方向转动;A rotating platform (2), the fixed end of which is connected to the moving vehicle (1), and the rotating end of which is used for horizontal rotation;变幅装置(3),固定端与所述回转平台(2)的转动端相连;A luffing device (3), the fixed end of which is connected to the rotating end of the rotary platform (2);伸缩升降装置(4),固定端与所述变幅装置(3)的变幅端相连,伸缩端与折展驱动机构(6)一端相连,所述伸缩端中部枢接机械臂(4-1),所述机械臂(4-1)的活动端与折展驱动机构(6)另一端相连用于调平折展驱动机构(6),所述折展驱动机构(6)与可折叠回收滑道(5)相连,用于控制可折叠回收滑道(5)的折展。A telescopic lifting device (4), wherein a fixed end is connected to the variable amplitude end of the variable amplitude device (3), a telescopic end is connected to one end of a folding and unfolding driving mechanism (6), a middle portion of the telescopic end is pivotally connected to a mechanical arm (4-1), a movable end of the mechanical arm (4-1) is connected to the other end of the folding and unfolding driving mechanism (6) for leveling the folding and unfolding driving mechanism (6), and the folding and unfolding driving mechanism (6) is connected to a foldable recovery slide (5) for controlling the folding and unfolding of the foldable recovery slide (5).7.根据权利要求6所述的一种无人机回收装置,其特征在于:所述可折叠回收滑道(5)包括两个分体滑道,所述折展驱动机构(6)具有两个对称布置的转动端,每个所述分体滑道与对应的折展驱动机构(6)转动端相连,当折展驱动机构(6)的两个转动端转动时,带动两个分体滑道对接或分离。7. A drone recovery device according to claim 6, characterized in that: the foldable recovery slide (5) includes two split slides, the folding drive mechanism (6) has two symmetrically arranged rotating ends, each of the split slides is connected to the corresponding rotating end of the folding drive mechanism (6), and when the two rotating ends of the folding drive mechanism (6) rotate, the two split slides are driven to dock or separate.
CN202411299542.3A2024-09-182024-09-18 A variable damping mechanism and a drone recovery device having the samePendingCN119196243A (en)

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