CN209581935U - A kind of unmanned plane landing platform clamping device - Google Patents
A kind of unmanned plane landing platform clamping device Download PDFInfo
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- CN209581935U CN209581935U CN201821818472.8U CN201821818472U CN209581935U CN 209581935 U CN209581935 U CN 209581935U CN 201821818472 U CN201821818472 U CN 201821818472U CN 209581935 U CN209581935 U CN 209581935U
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- clamping jaw
- landing platform
- unmanned plane
- spacing
- grasping part
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Abstract
The utility model relates to air vehicle technique fields, specifically a kind of unmanned plane landing platform clamping device, it is characterized in that, including landing platform, spacing adjusting device, two vertically disposed clamping jaw devices, the grasping part of the clamping jaw device is located at the upper end of clamping jaw device, the spacing adjusting device is connected with the bottom of two clamping jaw devices respectively, two clamping jaw devices are driven to do the relative motion in horizontal direction, the landing platform is equipped with the gripper rail so that the perforation that the grasping part of clamping jaw device passes through；When clamping jaw device, which is in, loosens state, grasping part is in the lower section of landing platform upper surface, and when clamping jaw device is in promptly state, grasping part passes through the corresponding position that the gripper rail being arranged on landing platform grasps external unmanned plane；Compared to the prior art the utility model, improves the stability of unmanned plane landing, realize unmanned plane on vehicle-mounted removable airport and land and fix the functions such as transport.
Description
Technical field
The utility model relates to air vehicle technique field, specifically a kind of unmanned plane landing platform clamping device.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.Unmanned plane
By application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+
Industrial application is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country also in actively extension industrial application and develops unmanned plane
Technology.
Currently, the ground service system of unmanned plane lags behind the development of unmanned plane itself, sliding race landing (is mainly suitable for by runway
Unmanned plane)/airplane parking area (unmanned plane suitable for VTOL) and radio robot constitute, the degree of automation is extremely low,
It needs artificial on duty.In addition, what the automatic landing station of current unmanned plane, airport itself or static state were placed on the ground, such as
Fruit is placed on mobile vehicle, how to ensure that unmanned plane does not shift collision after landing, before this not no good solution party
Case and product.
Therefore, there are also to be developed for the prior art.
Utility model content
Place in view of above-mentioned deficiencies of the prior art, the purpose of this utility model is to provide a kind of unmanned plane landing platforms
Clamping device.Aim to solve the problem that prior art poor safety performance, the low problem of the degree of automation.
In order to achieve the above object, the utility model takes following technical scheme:
The utility model provides a kind of unmanned plane landing platform clamping device characterized by comprising
Landing platform；
Spacing adjusting device；
Two vertically disposed clamping jaw devices, the grasping part of the clamping jaw device is located at the upper end of clamping jaw device, between described
It is connected respectively with the bottom of two clamping jaw devices away from regulating device, two clamping jaw devices is driven to do the opposite fortune in horizontal direction
Dynamic, the landing platform is equipped with the gripper rail so that the perforation that the grasping part of clamping jaw device passes through；When clamping jaw device is in
When loosening state, grasping part is in the lower section of landing platform upper surface, when clamping jaw device is in promptly state, grasping part
The gripper rail being arranged on landing platform grasps the corresponding position of external unmanned plane.
Further, the spacing adjusting device includes that T-shaped plate, side wall are fixed on the vertical plate and landing platform of T-shaped plate
Between spacing adjust driving device, horizontally disposed in the active wedge of isosceles trapezoid, rail connects in active wedge two sides respectively
Two driven wedges at side, the bottom of two clamping jaw devices are separately fixed on the upper surface of two driven wedges, two from
Rail connects the corresponding position at the level board upper surface of T-shaped plate, the lower surface rail of the active wedge respectively for the lower surface of dynamic wedge
It connects at T-shaped plate vertical panel upper surface, the spacing adjusts the end of the telescopic rod of driving device and the bottom edge of active wedge and consolidates
Fixed connection pushes active wedge to move back and forth along the length direction of T-shaped plate vertical panel, thus drive two driven wedges along
The length direction of T-shaped plate level board does opposite reciprocating motion.
Further, the spacing adjusts driving device and adjusts driving electric cylinders using spacing.
It further, further include the pitch measuring being electrically connected with spacing adjusting device, the pitch measuring
It measures the spacing size of external unmanned plane undercarriage and distance signal is transferred to spacing adjusting device.
The utility model compared with prior art, improves the stability of unmanned plane landing, realizes unmanned plane vehicle-mounted
The functions such as mobile airport land and fixed transport.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of the utility model landing terrace part.
Specific embodiment
The preferred embodiment of the utility model is illustrated below, it should be understood that preferred embodiment described herein
It is only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment 1
The utility model provides a kind of unmanned plane landing platform clamping device characterized by comprising
Landing platform 1；
Spacing adjusting device；
Two vertically disposed clamping jaw devices, the grasping part of the clamping jaw device 4-3 are located at the upper end of clamping jaw device 4-3,
The spacing adjusting device is connected with the bottom of two clamping jaw device 4-3 respectively, and two clamping jaw device 4-3 is driven to do horizontal direction
On relative motion, the landing platform 1 be equipped with so that the perforation that the grasping part of clamping jaw device 4-3 passes through gripper rail 1-
2；When clamping jaw device 4-3, which is in, loosens state, grasping part is in the lower section of 1 upper surface of landing platform, as clamping jaw device 4-3
When in promptly state, grasping part passes through the correspondence that the gripper rail 1-2 being arranged on landing platform 1 grasps external unmanned plane
Position.
Further, the spacing adjusting device includes that T-shaped plate 4-2, side wall are fixed on the vertical plate of T-shaped plate 4-2 and rise
It drops the spacing between platform 1 and adjusts that driving device, the horizontally disposed active wedge 4-5 in isosceles trapezoid, rail connects in master respectively
Two driven wedge 4-4 at the dynamic two sides wedge 4-5, the bottom of two clamping jaw device 4-3 are separately fixed at two and driven carve
On the upper surface of block 4-4, the lower surface of two driven wedge 4-4 respectively rail connect it is corresponding at the level board upper surface of T-shaped plate 4-2
Position, the lower surface rail of the active wedge 4-5 connect at T-shaped plate 4-2 vertical panel upper surface, and the spacing adjusts driving device
The end of telescopic rod be fixedly connected with the bottom edge of active wedge 4-5, push active wedge 4-5 along T-shaped plate 4-2 vertical panel
Length direction moves back and forth, so that it is opposite to drive two driven wedge 4-4 to do along the length direction of T-shaped plate 4-2 level board
It moves back and forth.
Further, the spacing adjusts driving device and adjusts driving electric cylinders 4-1 using spacing.
It further, further include the pitch measuring being electrically connected with spacing adjusting device, the pitch measuring
It measures the spacing size of external unmanned plane undercarriage and distance signal is transferred to spacing adjusting device.
When utility model works, the pitch measuring measures the spacing size of external unmanned plane undercarriage and by between
Spacing is transferred to away from signal and adjusts driving electric cylinders 4-1, and the spacing adjusts driving electric cylinders 4-1 and pushes active wedge 4-5 along T shape
The vertical panel length direction of plate 4-2 moves, and two driven wedge 4-4 is driven to do along the level board length direction of T shape plate 4-2
Movement that is relatively close or being relatively distant from, until between the spacing between two driven wedge 4-4 and outside unmanned plane undercarriage
Away from identical, clamping jaw device 4-3 start-up operation at this time, the gripper rail 1-2 for the perforation that grasping part is arranged on landing platform 1
Completion grips external unmanned plane.
Claims (4)
1. a kind of unmanned plane landing platform clamping device characterized by comprising
Landing platform (1)；
Spacing adjusting device；
The grasping part of two vertically disposed clamping jaw devices, the clamping jaw device (4-3) is located at the upper end of clamping jaw device (4-3),
The spacing adjusting device is connected with the bottom of two clamping jaw devices (4-3) respectively, and two clamping jaw devices (4-3) is driven to do level
Relative motion on direction, the landing platform (1) are equipped with the folder so that the perforation that the grasping part of clamping jaw device (4-3) passes through
Hold track (1-2)；When clamping jaw device (4-3), which is in, loosens state, grasping part is under landing platform (1) upper surface
Side, when clamping jaw device (4-3) is in promptly state, grasping part passes through the gripper rail (1-2) being arranged on landing platform (1)
Grasp the corresponding position of external unmanned plane.
2. a kind of unmanned plane landing platform clamping device according to claim 1, which is characterized in that the spacing adjusts dress
It sets the spacing being fixed between the vertical plate of T-shaped plate (4-2) and landing platform (1) including T-shaped plate (4-2), side wall and adjusts driving
It is device, horizontally disposed in the active wedge (4-5) of isosceles trapezoid, rail meets two at the two sides active wedge (4-5) respectively
A driven wedge (4-4), the bottom of two clamping jaw devices (4-3) are separately fixed on the upper surface of two driven wedges (4-4),
Rail meets the corresponding position at the level board upper surface of T-shaped plate (4-2), the master respectively for the lower surface of two driven wedges (4-4)
The lower surface rail of dynamic wedge (4-5) connects at T-shaped plate (4-2) vertical panel upper surface, and the spacing adjusts the flexible of driving device
The end of bar is fixedly connected with the bottom edge of active wedge (4-5), pushes active wedge (4-5) along T-shaped plate (4-2) vertical panel
Length direction moves back and forth, so that two driven wedges (4-4) be driven to do phase along the length direction of T-shaped plate (4-2) level board
Pair reciprocating motion.
3. a kind of unmanned plane landing platform clamping device according to claim 2, which is characterized in that the spacing, which is adjusted, drives
Dynamic device adjusts driving electric cylinders (4-1) using spacing.
4. a kind of unmanned plane landing platform clamping device according to claim 1, which is characterized in that further include and spacing tune
The pitch measuring that regulating device is electrically connected, the pitch measuring measure the spacing size of external unmanned plane undercarriage simultaneously
Distance signal is transferred to spacing adjusting device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821818472.8U CN209581935U (en) | 2018-11-06 | 2018-11-06 | A kind of unmanned plane landing platform clamping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821818472.8U CN209581935U (en) | 2018-11-06 | 2018-11-06 | A kind of unmanned plane landing platform clamping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209581935U true CN209581935U (en) | 2019-11-05 |
Family
ID=68376280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821818472.8U Active CN209581935U (en) | 2018-11-06 | 2018-11-06 | A kind of unmanned plane landing platform clamping device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209581935U (en) |
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2018
- 2018-11-06 CN CN201821818472.8U patent/CN209581935U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: Room 1404, Guanghua Building, No. 777, Guangzhou Road, Binjiang Street, Haimen District, Nantong City, Jiangsu Province, 226100 Patentee after: Fuya Intelligent Technology Development (Jiangsu) Co.,Ltd. Address before: 200082 Shanghai Yangpu District Guotai Road 127 Lane 1, 3rd Floor (Centralized Registration Place) Patentee before: SHANGHAI FUYA INTELLIGENT TECHNOLOGY Co.,Ltd. |