技术领域technical field
本发明涉及航空信息化技术领域，具体是一种智能民用航空自动化管制系统。The invention relates to the field of aviation information technology, in particular to an intelligent civil aviation automatic control system.
背景技术Background technique
随着科技的发展，社会的进步，国家一直促进高科技的发展，在航空信息化技术领域中，一直存在一个比较困难的技术问题，一般的民航管制系统由于资金技术的限制，导致空中交通出现堵塞，产生极大的危险，一般的管制系统中的雷达显示屏均是固定在工作台上，移动和收纳不便，同时操作员观察视角不易调节，不仅影响操作员，而且严重时可能会导致信息观察漏洞，造成不可弥补的结果，此装置有效解决了此问题。With the development of science and technology and the progress of society, the country has been promoting the development of high technology. In the field of aviation information technology, there has always been a relatively difficult technical problem. Due to the limitation of capital and technology in the general civil aviation control system, air traffic has appeared. The blockage will cause great danger. The radar screen in the general control system is fixed on the workbench, which is inconvenient to move and store. At the same time, the operator's viewing angle is not easy to adjust, which not only affects the operator, but also may cause information in severe cases. Observe loopholes, resulting in irreparable results, this device effectively solves this problem.
发明内容Contents of the invention
本发明所要解决的技术问题是提供一种智能民用航空自动化管制系统，其能够解决上述现在技术中的问题。The technical problem to be solved by the present invention is to provide an intelligent civil aviation automatic control system, which can solve the above-mentioned problems in the prior art.
本发明是通过以下技术方案来实现的：本发明的一种智能民用航空自动化管制系统，包括机身以及设置在所述机身内开口向上的圆柱收纳腔，所述圆柱收纳腔内壁内相通设有环形滑槽，所述圆柱收纳腔左右内壁体内贯通设有相对称且位于所述环形滑槽顶部的导向槽，所述圆柱收纳腔底部设有第一空腔，所述环形滑槽内滑动配合连接有圆环块，所述圆环块内上下贯通设有圆柱腔，所述圆环块内螺纹配合连接有左右对称且上下延伸的升降螺纹杆，所述升降螺纹杆底部延伸末端伸进所述第一空腔内且在端面设有第一带轮，所述升降螺纹杆顶部延伸末端伸进所述导向槽内且在末端设有第一齿转轮，所述圆柱腔内转动配合连接有圆盘，所述圆盘内顶部端面内设有开口向上的收纳腔，所述收纳腔底部相通设有第一导滑槽，所述第一导滑槽右端设有开口向右的第二空腔，所述收纳腔底部内壁上设有支撑架，所述收纳腔上设有位于所述支撑架右端的脚座，所述支撑架上铰接连接有雷达银屏载板，所述雷达银屏载板顶部端面上设有雷达银屏，所述雷达银屏载板底部端面内设有开口向下的第二导滑槽，所述第二导滑槽内滑动配合连接有第一导滑块，所述第一导滑块与所述脚座之间铰接连接有第一连接杆，所述第一导滑槽内滑动配合连接有第二导滑块，所述第二导滑块内螺纹配合连接有左右延伸的调节螺纹杆，所述调节螺纹杆左端延伸末端与所述第一导滑槽左端内壁转动配合连接，所述调节螺纹杆右端延伸末端伸进所述第二空腔内且在末端设有第一锥齿轮，所述第二导滑块顶部铰接连接有第二连接杆，所述第二连接杆另一端与所述第一连接杆中部铰接连接，所述第二空腔内转动配合连接有上下延伸的第一转动轴，所述第一转动轴上设有用以与所述第一锥齿轮和所述圆柱腔内壁齿合连接的齿锥双用轮，所述圆柱收纳腔底部设有用以与所述圆盘动力连接的活动驱动装置，所述机身右端端面上设有电除尘装置。The present invention is achieved through the following technical solutions: An intelligent civil aviation automatic control system of the present invention includes a fuselage and a cylindrical storage cavity with an upward opening in the fuselage, and the inner wall of the cylindrical storage cavity is communicated with a There is an annular chute, and the left and right inner walls of the cylindrical storage cavity are provided with symmetrical guide grooves located on the top of the annular chute, and the bottom of the cylindrical storage cavity is provided with a first cavity, and the sliding in the annular chute There is a ring block connected in cooperation, and a cylindrical cavity is provided up and down inside the ring block, and a left-right symmetrical lifting threaded rod extending up and down is connected with the internal thread of the ring block, and the bottom extension end of the lifting threaded rod extends into the In the first cavity, a first pulley is provided on the end face, and the top extension end of the lifting threaded rod extends into the guide groove, and a first tooth runner is provided at the end, and the rotation fits in the cylindrical cavity. A disc is connected, and a storage chamber with an upward opening is arranged on the inner top surface of the disc. The bottom of the storage chamber communicates with a first guide chute, and the right end of the first guide chute is provided with a second guide chute that opens to the right. Two cavities, the bottom inner wall of the storage cavity is provided with a support frame, the storage cavity is provided with a foot seat located at the right end of the support frame, the support frame is hingedly connected with a radar screen carrier board, and the radar screen A radar silver screen is provided on the top end surface of the carrier board, and a second guide chute opening downward is provided in the bottom end surface of the radar silver screen carrier board, and a first guide slider is slidably connected to the second guide chute, so that A first connecting rod is hingedly connected between the first guide slider and the foot seat, a second guide slider is slidably connected in the first guide groove, and the second guide slider is connected with an internal thread. There is an adjusting threaded rod extending left and right, the left end of the adjusting threaded rod is rotated and connected with the inner wall of the left end of the first guide chute, and the right end of the adjusting threaded rod extends into the second cavity and is at the end A first bevel gear is provided, the top of the second guide slider is hingedly connected with a second connecting rod, the other end of the second connecting rod is hingedly connected with the middle part of the first connecting rod, and the second cavity rotates A first rotating shaft extending up and down is mated and connected, and the first rotating shaft is provided with a toothed bevel double-purpose wheel for meshing connection with the first bevel gear and the inner wall of the cylindrical cavity, and the bottom of the cylindrical storage cavity A movable driving device for power connection with the disk is provided, and an electric dust removal device is provided on the right end surface of the fuselage.
作为优选地技术方案，所述活动驱动装置包括设置在所述圆柱收纳腔内位于所述圆盘底部的活动块，所述活动块顶部端面内设有第一电动机，所述第一电动机顶部末端与所述圆盘底部端面动力连接，所述活动块底部四角设有上下延伸的导滑杆，所述导滑杆伸进所述圆柱收纳腔底部内壁体内且与之滑动配合连接。As a preferred technical solution, the movable driving device includes a movable block arranged in the cylindrical storage cavity at the bottom of the disc, a first motor is arranged in the top end surface of the movable block, and the top end of the first motor is It is connected to the bottom end surface of the disc by power, and the four corners of the bottom of the movable block are provided with guide rods extending up and down, and the guide rods extend into the inner wall of the bottom of the cylinder storage cavity and are connected with it by sliding fit.
作为优选地技术方案，所述第一空腔底部内壁内嵌设有第二电动机，所述第二电动机顶部末端动力连接有第二带轮，所述第一带轮与所述第二带轮之间动力连接有皮带。As a preferred technical solution, a second motor is embedded in the inner wall of the bottom of the first cavity, and a second pulley is connected to the top end of the second motor, and the first pulley and the second pulley There is a belt between the power connections.
作为优选地技术方案，所述导向槽内滑动配合连接有左右延伸的保护门板，所述保护门板底部端面内设有开口向下且用以与所述第一齿转轮齿合连接的动力槽。As a preferred technical solution, a protective door panel extending from left to right is slidingly fitted in the guide groove, and a power slot with an opening downward and used for meshing connection with the first gear wheel is provided in the bottom end surface of the protective door panel. .
作为优选地技术方案，所述电除尘装置包括设置在所述机身右端端面上的电除尘机体，所述电除尘机体内设有开口向右的滑移槽，所述滑移槽内滑动配合连接有滑移块，所述滑移块右端端面上设有电除尘器，所述滑移快上设有左右延伸的调节螺纹杆，所述调节螺纹杆左端末端动力连接有第三电动机，所述第三电动机外表面嵌设于所述滑移槽左端内壁内且与之固定连接。As a preferred technical solution, the electrostatic precipitator includes an electrostatic precipitator body arranged on the right end face of the fuselage, and a sliding groove opening to the right is provided in the electric dust removal body, and the sliding groove is fitted with a A sliding block is connected, and an electrostatic precipitator is provided on the right end surface of the sliding block, and an adjusting threaded rod extending left and right is provided on the sliding block, and a third motor is connected to the left end of the adjusting threaded rod, so The outer surface of the third motor is embedded in the inner wall at the left end of the sliding groove and is fixedly connected with it.
本发明的有益效果是：由于本发明的设备在初始状态时，所述圆环块位于所述环形滑槽最底部，此时，所述活动块底部端面与所述圆柱收纳腔底部内壁抵接，两个所述保护门板相对的端面抵接，所述保护门板将所述圆柱收纳腔完全封闭，所述雷达银屏载板完全位于所述收纳腔内且处于水平状态，所述第一导滑块位于所述第二导滑槽最右端，所述第二导滑块位于所述第一导滑槽最右端，从而便于装置维护和保养。The beneficial effects of the present invention are: when the device of the present invention is in the initial state, the ring block is located at the bottom of the annular chute, at this time, the bottom end surface of the movable block abuts against the inner wall of the bottom of the cylindrical storage chamber , the opposite end faces of the two protective door panels abut, the protective door panels completely seal the cylindrical storage cavity, the radar silver screen carrier board is completely located in the storage cavity and is in a horizontal state, the first guide slide The block is located at the rightmost end of the second guide chute, and the second guide slider is located at the rightmost end of the first guide chute, thereby facilitating device maintenance and maintenance.
当使用本发明的设备进行航空管制监测时，首先进行第一步启动装置，启动所述第二电动机带动所述第二带轮转动，所述第二带轮通过所述皮带和所述第一带轮带动所述升降螺纹杆转动，所述升降螺纹杆带动所述圆环块和所述圆盘整体上移，并同时带动所述第一齿转轮转动，所述第一齿转轮带动所述保护门板相背离移动，所述活动块受到所述圆盘的拉力向上移动，但由于所述导滑杆的作用使所述第一电动机可保持与所述圆盘的动力连接，当所述圆环块移动至所述环形滑槽最顶部时，两个所述保护门板最大距离远离，所述圆柱收纳腔完全被敞开，此时，所述雷达银屏完全暴露在外界便于操作员观察，此时，控制所述第二电动机停止运转，从而提高装置便利性。When using the equipment of the present invention for air traffic control monitoring, the first step is to start the device, start the second motor to drive the second pulley to rotate, and the second pulley passes through the belt and the first The pulley drives the lifting threaded rod to rotate, and the lifting threaded rod drives the ring block and the disc to move up as a whole, and at the same time drives the first tooth runner to rotate, and the first tooth runner drives The protective door panels move away from each other, and the movable block is moved upward by the pulling force of the disc, but due to the action of the guide rod, the first motor can maintain the power connection with the disc. When the ring block moves to the top of the annular chute, the maximum distance between the two protective door panels is far away, and the cylindrical storage cavity is completely opened. At this time, the radar silver screen is completely exposed to the outside world for the operator to observe. At this time, the second electric motor is controlled to stop running, thereby improving the convenience of the device.
当进行第二步观察位置调节时，启动所述第一电动机带动所述圆盘转动，同时，由于所述齿锥双用轮与所述圆柱腔的齿合，使所述齿锥双用轮转动且带动所述第一锥齿轮转动，使所述调节螺纹杆的转动并带动所述第二导滑块左移，所述第二导滑块通过所述第二连接杆和所述第一连接杆使所述雷达银屏载板逆时针转动，直至调节至适合操作员观察的位置，从而提高了装置工作效果。When performing the second step of observing position adjustment, start the first motor to drive the disc to rotate, and at the same time, due to the toothing of the dual-purpose wheel and the cylindrical cavity, the dual-purpose wheel Rotate and drive the first bevel gear to rotate, make the rotation of the adjusting threaded rod and drive the second guide slider to move left, the second guide slider passes through the second connecting rod and the first The connecting rod makes the radar silver screen carrier board rotate counterclockwise until it is adjusted to a position suitable for the operator to observe, thereby improving the working effect of the device.
当完成工作需要收纳时，控制所述第一电动机带动所述圆盘反向转动，同时，由于所述齿锥双用轮与所述圆柱腔的齿合，使所述齿锥双用轮反向转动且带动所述第一锥齿轮反向转动，使所述调节螺纹杆的反向转动并带动所述第二导滑块右移恢复初始位置，所述第二导滑块通过所述第二连接杆和所述第一连接杆使所述雷达银屏载板顺时针转动恢复初始位置，然后控制所述第一电动机停止运转，之后启动所述第二电动机带动所述第二带轮反向转动，所述第二带轮通过所述皮带和所述第一带轮带动所述升降螺纹杆反向转动，所述升降螺纹杆带动所述圆环块和所述圆盘整体下移，并同时带动所述第一齿转轮反向转动，所述第一齿转轮带动所述保护门板相向移动，所述活动块受到所述圆盘的压力向下移动，当所述圆环块移动至所述环形滑槽最底部时，两个所述保护门板抵接，所述圆柱收纳腔完全被封闭，控制所述第二电动机停止运转，从而提高了装置的实用性能。When the work needs to be stored, the first motor is controlled to drive the disc to rotate in the opposite direction. Rotate to the opposite direction and drive the first bevel gear to rotate in reverse, make the reverse rotation of the adjusting threaded rod and drive the second guide slider to move right to restore the original position, the second guide slider passes through the first The two connecting rods and the first connecting rod make the radar silver screen carrier board rotate clockwise to return to the initial position, then control the first motor to stop running, and then start the second motor to drive the second pulley to reverse Rotate, the second pulley drives the lifting threaded rod to rotate reversely through the belt and the first pulley, the lifting threaded rod drives the ring block and the disc to move down as a whole, and At the same time, it drives the first tooth runner to rotate in reverse, and the first tooth runner drives the protective door panels to move toward each other. The movable block moves downward under the pressure of the disc. When the ring block moves When reaching the bottom of the annular chute, the two protective door panels abut, the cylindrical storage cavity is completely closed, and the second motor is controlled to stop running, thereby improving the practical performance of the device.
本发明结构简单，操作方便，通过采用收纳机构与保护机构于一体，设备轻巧，操作简单，各个部件配合密切但又互不影响，同时又在收纳机构的内部设有活动式驱动机构，通过活动式驱动机构自动调节操作位置，使用寿命长，价格优异，实用性能较高。The invention is simple in structure and easy to operate. By integrating the storage mechanism and the protection mechanism, the equipment is light and handy, and the operation is simple. The parts cooperate closely but do not affect each other. The type driving mechanism automatically adjusts the operating position, has a long service life, excellent price and high practical performance.
附图说明Description of drawings
为了易于说明，本发明由下述的具体实施例及附图作以详细描述。For ease of illustration, the present invention is described in detail by the following specific embodiments and accompanying drawings.
图1为本发明的一种智能民用航空自动化管制系统初始状态时的整体结构示意图；Fig. 1 is the overall structure schematic diagram when a kind of intelligent civil aviation automatic control system initial state of the present invention;
图2为本发明的一种智能民用航空自动化管制系统工作时的整体结构示意图。Fig. 2 is a schematic diagram of the overall structure of an intelligent civil aviation automatic control system in operation according to the present invention.
具体实施方式Detailed ways
如图1和图2所示，本发明的一种智能民用航空自动化管制系统，包括机身100以及设置在所述机身100内开口向上的圆柱收纳腔118，所述圆柱收纳腔118内壁内相通设有环形滑槽101，所述圆柱收纳腔118左右内壁体内贯通设有相对称且位于所述环形滑槽101顶部的导向槽121，所述圆柱收纳腔118底部设有第一空腔109，所述环形滑槽101内滑动配合连接有圆环块104，所述圆环块104内上下贯通设有圆柱腔105，所述圆环块104内螺纹配合连接有左右对称且上下延伸的升降螺纹杆102，所述升降螺纹杆102底部延伸末端伸进所述第一空腔109内且在端面设有第一带轮108，所述升降螺纹杆102顶部延伸末端伸进所述导向槽121内且在末端设有第一齿转轮120，所述圆柱腔105内转动配合连接有圆盘134，所述圆盘134内顶部端面内设有开口向上的收纳腔123，所述收纳腔123底部相通设有第一导滑槽130，所述第一导滑槽130右端设有开口向右的第二空腔116，所述收纳腔123底部内壁上设有支撑架135，所述收纳腔123上设有位于所述支撑架135右端的脚座125，所述支撑架135上铰接连接有雷达银屏载板126，所述雷达银屏载板126顶部端面上设有雷达银屏124，所述雷达银屏载板126底部端面内设有开口向下的第二导滑槽127，所述第二导滑槽127内滑动配合连接有第一导滑块133，所述第一导滑块133与所述脚座125之间铰接连接有第一连接杆128，所述第一导滑槽130内滑动配合连接有第二导滑块132，所述第二导滑块132内螺纹配合连接有左右延伸的调节螺纹杆131，所述调节螺纹杆131左端延伸末端与所述第一导滑槽130左端内壁转动配合连接，所述调节螺纹杆131右端延伸末端伸进所述第二空腔116内且在末端设有第一锥齿轮114，所述第二导滑块132顶部铰接连接有第二连接杆129，所述第二连接杆129另一端与所述第一连接杆128中部铰接连接，所述第二空腔116内转动配合连接有上下延伸的第一转动轴115，所述第一转动轴115上设有用以与所述第一锥齿轮114和所述圆柱腔105内壁齿合连接的齿锥双用轮117，所述圆柱收纳腔118底部设有用以与所述圆盘134动力连接的活动驱动装置，所述机身100右端端面上设有电除尘装置。As shown in Figures 1 and 2, an intelligent civil aviation automatic control system of the present invention includes a fuselage 100 and a cylindrical storage cavity 118 with an upward opening in the fuselage 100, and the inner wall of the cylindrical storage cavity 118 An annular chute 101 is communicated with each other. A symmetrical guide groove 121 located on the top of the annular chute 101 runs through the left and right inner walls of the cylindrical storage chamber 118. A first cavity 109 is provided at the bottom of the cylindrical storage chamber 118. , the ring block 104 is slidably connected to the ring chute 101, and a cylindrical cavity 105 is formed up and down in the ring block 104, and a vertically symmetrical and vertically extending lift is connected to the internal thread of the ring block 104. Threaded rod 102, the bottom extension end of the lifting threaded rod 102 extends into the first cavity 109 and a first pulley 108 is provided on the end surface, the top extension end of the lifting threaded rod 102 extends into the guide groove 121 Inside and at the end is provided with a first tooth runner 120, a disk 134 is connected to the cylinder cavity 105 for rotation, the top end surface of the disk 134 is provided with a storage cavity 123 with an upward opening, and the storage cavity 123 The bottom is communicated with a first guide chute 130, the right end of the first guide chute 130 is provided with a second cavity 116 opening to the right, the inner wall of the bottom of the storage cavity 123 is provided with a support frame 135, the storage cavity 123 is provided with a foot seat 125 located at the right end of the support frame 135, and the support frame 135 is hingedly connected with a radar screen carrier board 126, and a radar screen 124 is arranged on the top end of the radar screen carrier board 126, and the radar screen carrier board 124 is provided with a radar screen 124. The bottom end surface of the silver screen carrier 126 is provided with a second sliding guide groove 127 with an opening downward, and a first sliding guide block 133 is slidably connected in the second guiding sliding groove 127, and the first sliding guide block 133 is connected with the first sliding guide block 133. A first connecting rod 128 is hingedly connected between the feet 125, a second guide slider 132 is slidably connected in the first guide chute 130, and the inner thread of the second guide slider 132 is connected with left and right extensions. Adjusting threaded rod 131, the left end extension of the adjustment threaded rod 131 is rotationally connected with the inner wall of the left end of the first guide chute 130, the right end extension of the adjustment threaded rod 131 extends into the second cavity 116 and The end is provided with a first bevel gear 114, the top of the second guide slider 132 is hingedly connected with a second connecting rod 129, and the other end of the second connecting rod 129 is hingedly connected with the middle part of the first connecting rod 128, so In the second cavity 116, there is a first rotating shaft 115 that extends up and down in a rotational fit connection, and the first rotating shaft 115 is provided with a toothing connection with the first bevel gear 114 and the inner wall of the cylindrical cavity 105. A toothed and conical double-purpose wheel 117, a movable driving device for power connection with the disc 134 is provided at the bottom of the cylindrical storage chamber 118, and an electrostatic precipitator is provided on the right end surface of the fuselage 100.
有益地，所述活动驱动装置包括设置在所述圆柱收纳腔118内位于所述圆盘134底部的活动块106，所述活动块106顶部端面内设有第一电动机113，所述第一电动机113顶部末端与所述圆盘134底部端面动力连接，所述活动块106底部四角设有上下延伸的导滑杆107，所述导滑杆107伸进所述圆柱收纳腔118底部内壁体内且与之滑动配合连接。Beneficially, the movable driving device includes a movable block 106 disposed at the bottom of the disc 134 in the cylinder receiving cavity 118, a first motor 113 is arranged in the top end surface of the movable block 106, and the first motor 113 top end is dynamically connected with the bottom end face of the disc 134, and the four corners of the bottom of the movable block 106 are provided with guide rods 107 extending up and down, and the guide rods 107 extend into the inner wall of the bottom of the cylindrical storage chamber 118 and are connected with The sliding fit connection.
有益地，所述第一空腔109底部内壁内嵌设有第二电动机111，所述第二电动机111顶部末端动力连接有第二带轮112，所述第一带轮108与所述第二带轮112之间动力连接有皮带110。Beneficially, a second motor 111 is embedded in the inner wall of the bottom of the first cavity 109, and the top end of the second motor 111 is power-connected with a second pulley 112, and the first pulley 108 and the second A belt 110 is dynamically connected between the pulleys 112 .
有益地，所述导向槽121内滑动配合连接有左右延伸的保护门板122，所述保护门板122底部端面内设有开口向下且用以与所述第一齿转轮120齿合连接的动力槽119。Beneficially, a protective door panel 122 extending left and right is slidingly connected to the guide groove 121, and the bottom end surface of the protective door panel 122 is provided with an opening downward and is used to mesh with the first gear wheel 120. Groove 119.
有益地，所述电除尘装置包括设置在所述机身100右端端面上的电除尘机体200，所述电除尘机体200内设有开口向右的滑移槽201，所述滑移槽201内滑动配合连接有滑移块203，所述滑移块203右端端面上设有电除尘器202，所述滑移快203上设有左右延伸的调节螺纹杆204，所述调节螺纹杆204左端末端动力连接有第三电动机205，所述第三电动机205外表面嵌设于所述滑移槽201左端内壁内且与之固定连接。Beneficially, the electrostatic precipitator includes an electrostatic precipitator body 200 arranged on the right end face of the fuselage 100, and the electric precipitator body 200 is provided with a sliding groove 201 opening to the right, and inside the sliding groove 201 The sliding block 203 is connected by sliding fit, and the right end surface of the sliding block 203 is provided with an electrostatic precipitator 202. The sliding block 203 is provided with an adjusting threaded rod 204 extending left and right, and the left end of the adjusting threaded rod 204 is The power is connected with a third motor 205, and the outer surface of the third motor 205 is embedded in the inner wall of the left end of the sliding groove 201 and is fixedly connected with it.
本发明的设备在初始状态时，所述圆环块104位于所述环形滑槽101最底部，此时，所述活动块106底部端面与所述圆柱收纳腔118底部内壁抵接，两个所述保护门板122相对的端面抵接，所述保护门板122将所述圆柱收纳腔118完全封闭，所述雷达银屏载板126完全位于所述收纳腔123内且处于水平状态，所述第一导滑块133位于所述第二导滑槽127最右端，所述第二导滑块132位于所述第一导滑槽130最右端。When the device of the present invention is in the initial state, the annular block 104 is located at the bottom of the annular chute 101. At this time, the bottom end surface of the movable block 106 abuts against the inner wall of the bottom of the cylindrical storage cavity 118, and the two The opposite end surfaces of the protective door panel 122 are in contact with each other, the protective door panel 122 completely seals the cylindrical storage cavity 118, the radar silver screen carrier plate 126 is completely located in the storage cavity 123 and is in a horizontal state, and the first guide The slider 133 is located at the rightmost end of the second sliding guide groove 127 , and the second sliding guide block 132 is located at the rightmost end of the first sliding sliding groove 130 .
当使用本发明的设备进行航空管制监测时，首先进行第一步启动装置，启动所述第二电动机111带动所述第二带轮112转动，所述第二带轮112通过所述皮带110和所述第一带轮108带动所述升降螺纹杆102转动，所述升降螺纹杆102带动所述圆环块104和所述圆盘134整体上移，并同时带动所述第一齿转轮120转动，所述第一齿转轮120带动所述保护门板122相背离移动，所述活动块106受到所述圆盘134的拉力向上移动，但由于所述导滑杆107的作用使所述第一电动机113可保持与所述圆盘134的动力连接，当所述圆环块104移动至所述环形滑槽101最顶部时，两个所述保护门板122最大距离远离，所述圆柱收纳腔118完全被敞开，此时，所述雷达银屏124完全暴露在外界便于操作员观察，此时，控制所述第二电动机111停止运转。When using the equipment of the present invention to monitor air traffic control, the first step is to start the device, start the second motor 111 to drive the second pulley 112 to rotate, and the second pulley 112 passes through the belt 110 and The first pulley 108 drives the lifting threaded rod 102 to rotate, and the lifting threaded rod 102 drives the ring block 104 and the disc 134 to move up as a whole, and at the same time drives the first gear wheel 120 Rotate, the first gear wheel 120 drives the protective door panel 122 to move away from each other, the movable block 106 is moved upward by the pulling force of the disc 134, but due to the action of the guide rod 107, the first An electric motor 113 can maintain a power connection with the disc 134. When the ring block 104 moves to the top of the annular chute 101, the maximum distance between the two protective door panels 122 is far away, and the cylindrical storage chamber 118 is fully opened, at this time, the radar silver screen 124 is completely exposed to the outside world for the operator to observe, at this time, the second motor 111 is controlled to stop running.
当进行第二步观察位置调节时，启动所述第一电动机113带动所述圆盘134转动，同时，由于所述齿锥双用轮117与所述圆柱腔105的齿合，使所述齿锥双用轮117转动且带动所述第一锥齿轮114转动，使所述调节螺纹杆131的转动并带动所述第二导滑块132左移，所述第二导滑块132通过所述第二连接杆129和所述第一连接杆128使所述雷达银屏载板126逆时针转动，直至调节至适合操作员观察的位置。When performing the second-step observation position adjustment, start the first motor 113 to drive the disc 134 to rotate, and at the same time, due to the toothing of the toothed bevel dual-purpose wheel 117 and the cylindrical cavity 105, the teeth The bevel double-purpose wheel 117 rotates and drives the first bevel gear 114 to rotate, so that the rotation of the adjusting threaded rod 131 drives the second guide slider 132 to move left, and the second guide slider 132 passes through the The second connecting rod 129 and the first connecting rod 128 make the radar screen carrier board 126 rotate counterclockwise until it is adjusted to a position suitable for the operator to observe.
当完成工作需要收纳时，控制所述第一电动机113带动所述圆盘134反向转动，同时，由于所述齿锥双用轮117与所述圆柱腔105的齿合，使所述齿锥双用轮117反向转动且带动所述第一锥齿轮114反向转动，使所述调节螺纹杆131的反向转动并带动所述第二导滑块132右移恢复初始位置，所述第二导滑块132通过所述第二连接杆129和所述第一连接杆128使所述雷达银屏载板126顺时针转动恢复初始位置，然后控制所述第一电动机113停止运转，之后启动所述第二电动机111带动所述第二带轮112反向转动，所述第二带轮112通过所述皮带110和所述第一带轮108带动所述升降螺纹杆102反向转动，所述升降螺纹杆102带动所述圆环块104和所述圆盘134整体下移，并同时带动所述第一齿转轮120反向转动，所述第一齿转轮120带动所述保护门板122相向移动，所述活动块106受到所述圆盘134的压力向下移动，当所述圆环块104移动至所述环形滑槽101最底部时，两个所述保护门板122抵接，所述圆柱收纳腔118完全被封闭，控制所述第二电动机111停止运转。When the work needs to be stored, the first motor 113 is controlled to drive the disc 134 to rotate in the opposite direction. The double-purpose wheel 117 reversely rotates and drives the first bevel gear 114 to reversely rotate, so that the reverse rotation of the adjusting threaded rod 131 and drives the second guide slider 132 to move rightward to restore the initial position, the first The second guide slider 132 makes the radar screen carrier board 126 rotate clockwise through the second connecting rod 129 and the first connecting rod 128 to restore the initial position, then controls the first motor 113 to stop running, and then starts the The second motor 111 drives the second pulley 112 to rotate reversely, and the second pulley 112 drives the lifting threaded rod 102 to rotate reversely through the belt 110 and the first pulley 108. The lifting threaded rod 102 drives the ring block 104 and the disc 134 to move down as a whole, and at the same time drives the first tooth runner 120 to rotate in reverse, and the first tooth runner 120 drives the protective door panel 122 Moving towards each other, the movable block 106 moves downward under the pressure of the disc 134. When the ring block 104 moves to the bottom of the annular chute 101, the two protective door panels 122 abut against each other, so The cylindrical storage cavity 118 is completely closed, and the second motor 111 is controlled to stop running.
本发明的有益效果是：由于本发明的设备在初始状态时，所述圆环块位于所述环形滑槽最底部，此时，所述活动块底部端面与所述圆柱收纳腔底部内壁抵接，两个所述保护门板相对的端面抵接，所述保护门板将所述圆柱收纳腔完全封闭，所述雷达银屏载板完全位于所述收纳腔内且处于水平状态，所述第一导滑块位于所述第二导滑槽最右端，所述第二导滑块位于所述第一导滑槽最右端，从而便于装置维护和保养。The beneficial effects of the present invention are: when the device of the present invention is in the initial state, the ring block is located at the bottom of the annular chute, at this time, the bottom end surface of the movable block abuts against the inner wall of the bottom of the cylindrical storage chamber , the opposite end faces of the two protective door panels abut, the protective door panels completely seal the cylindrical storage cavity, the radar silver screen carrier board is completely located in the storage cavity and is in a horizontal state, the first guide slide The block is located at the rightmost end of the second guide chute, and the second guide slider is located at the rightmost end of the first guide chute, thereby facilitating device maintenance and maintenance.
当使用本发明的设备进行航空管制监测时，首先进行第一步启动装置，启动所述第二电动机带动所述第二带轮转动，所述第二带轮通过所述皮带和所述第一带轮带动所述升降螺纹杆转动，所述升降螺纹杆带动所述圆环块和所述圆盘整体上移，并同时带动所述第一齿转轮转动，所述第一齿转轮带动所述保护门板相背离移动，所述活动块受到所述圆盘的拉力向上移动，但由于所述导滑杆的作用使所述第一电动机可保持与所述圆盘的动力连接，当所述圆环块移动至所述环形滑槽最顶部时，两个所述保护门板最大距离远离，所述圆柱收纳腔完全被敞开，此时，所述雷达银屏完全暴露在外界便于操作员观察，此时，控制所述第二电动机停止运转，从而提高装置便利性。When using the equipment of the present invention for air traffic control monitoring, the first step is to start the device, start the second motor to drive the second pulley to rotate, and the second pulley passes through the belt and the first The pulley drives the lifting threaded rod to rotate, and the lifting threaded rod drives the ring block and the disc to move up as a whole, and at the same time drives the first tooth runner to rotate, and the first tooth runner drives The protective door panels move away from each other, and the movable block is moved upward by the pulling force of the disc, but due to the action of the guide rod, the first motor can maintain the power connection with the disc. When the ring block moves to the top of the annular chute, the maximum distance between the two protective door panels is far away, and the cylindrical storage cavity is completely opened. At this time, the radar silver screen is completely exposed to the outside world for the operator to observe. At this time, the second electric motor is controlled to stop running, thereby improving the convenience of the device.
当进行第二步观察位置调节时，启动所述第一电动机带动所述圆盘转动，同时，由于所述齿锥双用轮与所述圆柱腔的齿合，使所述齿锥双用轮转动且带动所述第一锥齿轮转动，使所述调节螺纹杆的转动并带动所述第二导滑块左移，所述第二导滑块通过所述第二连接杆和所述第一连接杆使所述雷达银屏载板逆时针转动，直至调节至适合操作员观察的位置，从而提高了装置工作效果。When performing the second step of observing position adjustment, start the first motor to drive the disc to rotate, and at the same time, due to the toothing of the dual-purpose wheel and the cylindrical cavity, the dual-purpose wheel Rotate and drive the first bevel gear to rotate, make the rotation of the adjusting threaded rod and drive the second guide slider to move left, the second guide slider passes through the second connecting rod and the first The connecting rod makes the radar silver screen carrier board rotate counterclockwise until it is adjusted to a position suitable for the operator to observe, thereby improving the working effect of the device.
当完成工作需要收纳时，控制所述第一电动机带动所述圆盘反向转动，同时，由于所述齿锥双用轮与所述圆柱腔的齿合，使所述齿锥双用轮反向转动且带动所述第一锥齿轮反向转动，使所述调节螺纹杆的反向转动并带动所述第二导滑块右移恢复初始位置，所述第二导滑块通过所述第二连接杆和所述第一连接杆使所述雷达银屏载板顺时针转动恢复初始位置，然后控制所述第一电动机停止运转，之后启动所述第二电动机带动所述第二带轮反向转动，所述第二带轮通过所述皮带和所述第一带轮带动所述升降螺纹杆反向转动，所述升降螺纹杆带动所述圆环块和所述圆盘整体下移，并同时带动所述第一齿转轮反向转动，所述第一齿转轮带动所述保护门板相向移动，所述活动块受到所述圆盘的压力向下移动，当所述圆环块移动至所述环形滑槽最底部时，两个所述保护门板抵接，所述圆柱收纳腔完全被封闭，控制所述第二电动机停止运转，从而提高了装置的实用性能。When the work needs to be stored, the first motor is controlled to drive the disc to rotate in the opposite direction. Rotate to the opposite direction and drive the first bevel gear to rotate in reverse, make the reverse rotation of the adjusting threaded rod and drive the second guide slider to move right to restore the original position, the second guide slider passes through the first The two connecting rods and the first connecting rod make the radar silver screen carrier board rotate clockwise to return to the initial position, then control the first motor to stop running, and then start the second motor to drive the second pulley to reverse Rotate, the second pulley drives the lifting threaded rod to rotate reversely through the belt and the first pulley, the lifting threaded rod drives the ring block and the disc to move down as a whole, and At the same time, it drives the first tooth runner to rotate in reverse, and the first tooth runner drives the protective door panels to move toward each other. The movable block moves downward under the pressure of the disc. When the ring block moves When reaching the bottom of the annular chute, the two protective door panels abut, the cylindrical storage cavity is completely closed, and the second motor is controlled to stop running, thereby improving the practical performance of the device.
本发明结构简单，操作方便，通过采用收纳机构与保护机构于一体，设备轻巧，操作简单，各个部件配合密切但又互不影响，同时又在收纳机构的内部设有活动式驱动机构，通过活动式驱动机构自动调节操作位置，使用寿命长，价格优异，实用性能较高。The invention is simple in structure and easy to operate. By integrating the storage mechanism and the protection mechanism, the equipment is light and handy, and the operation is simple. The parts cooperate closely but do not affect each other. The type driving mechanism automatically adjusts the operating position, has a long service life, excellent price and high practical performance.
以上所述，仅为本发明的具体实施方式，但本发明的保护范围并不局限于此，任何不经过创造性劳动想到的变化或替换，都应涵盖在本发明的保护范围之内。因此，本发明的保护范围应该以权利要求书所限定的保护范围为准。The above is only a specific implementation of the present invention, but the scope of protection of the present invention is not limited thereto, and any changes or replacements that do not come to mind through creative work shall be covered within the scope of protection of the present invention. Therefore, the protection scope of the present invention should be determined by the protection scope defined in the claims.
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810416273.2ACN108520643B (en) | 2018-05-03 | 2018-05-03 | An intelligent civil aviation automatic control system |
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810416273.2ACN108520643B (en) | 2018-05-03 | 2018-05-03 | An intelligent civil aviation automatic control system |
| Publication Number | Publication Date |
|---|---|
| CN108520643A CN108520643A (en) | 2018-09-11 |
| CN108520643Btrue CN108520643B (en) | 2019-08-20 |
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810416273.2AActiveCN108520643B (en) | 2018-05-03 | 2018-05-03 | An intelligent civil aviation automatic control system |
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| CN (1) | CN108520643B (en) |
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201008430Y (en)* | 2006-12-29 | 2008-01-23 | 刘文其 | Automatic meshwork multimedia platform |
| CN102485105A (en)* | 2010-12-02 | 2012-06-06 | 樊立冬 | Desk with adjustable horizontal-screen computer |
| CN102697289A (en)* | 2012-06-07 | 2012-10-03 | 集美大学 | Computer concealed desk |
| CN102697288A (en)* | 2012-06-07 | 2012-10-03 | 集美大学 | Multifunctional desk |
| CN204427139U (en)* | 2015-03-04 | 2015-07-01 | 邵心玮 | A kind of computer for students table |
| CN106820580A (en)* | 2017-02-28 | 2017-06-13 | 广州市富可士数码科技有限公司 | Fully-automatic intelligent multimedia lectern |
| CN107613809A (en)* | 2015-06-16 | 2018-01-19 | 安玛思有限责任公司 | retractable display |
| CN107830374A (en)* | 2017-09-28 | 2018-03-23 | 洛阳师范学院 | A kind of computer desk |
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201008430Y (en)* | 2006-12-29 | 2008-01-23 | 刘文其 | Automatic meshwork multimedia platform |
| CN102485105A (en)* | 2010-12-02 | 2012-06-06 | 樊立冬 | Desk with adjustable horizontal-screen computer |
| CN102697289A (en)* | 2012-06-07 | 2012-10-03 | 集美大学 | Computer concealed desk |
| CN102697288A (en)* | 2012-06-07 | 2012-10-03 | 集美大学 | Multifunctional desk |
| CN204427139U (en)* | 2015-03-04 | 2015-07-01 | 邵心玮 | A kind of computer for students table |
| CN107613809A (en)* | 2015-06-16 | 2018-01-19 | 安玛思有限责任公司 | retractable display |
| CN106820580A (en)* | 2017-02-28 | 2017-06-13 | 广州市富可士数码科技有限公司 | Fully-automatic intelligent multimedia lectern |
| CN107830374A (en)* | 2017-09-28 | 2018-03-23 | 洛阳师范学院 | A kind of computer desk |
| Publication number | Publication date |
|---|---|
| CN108520643A (en) | 2018-09-11 |
| Publication | Publication Date | Title |
|---|---|---|
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| TR01 | Transfer of patent right | Effective date of registration:20231018 Address after:201-8, 2nd Floor, Building 4, No. 9 Ronghua South Road, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 100176 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee after:Beijing Huajia Safety Protection Technology Co.,Ltd. Address before:No. 19 Xiaxia Village, Zhengzhai Town, Jinhua City, Zhejiang Province, 322200 Patentee before:PUJIANG FEITONG ELECTRONIC TECHNOLOGY CO.,LTD. | |
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