CN214607264U - Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle - Google Patents
Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle Download PDFInfo
- Publication number
- CN214607264U CN214607264U CN202120569055.XU CN202120569055U CN214607264U CN 214607264 U CN214607264 U CN 214607264U CN 202120569055 U CN202120569055 U CN 202120569055U CN 214607264 U CN214607264 U CN 214607264U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- ground service
- protective frame
- vehicle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model belongs to the unmanned aerial vehicle field, especially, unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle, it is relatively poor to the fixed effect of current unmanned aerial vehicle ground service vehicle after receiving unmanned aerial vehicle, imperfect to unmanned aerial vehicle's protection work, cause the problem of unmanned aerial vehicle damage easily, present scheme, it includes ground service loading board, protective frame, unmanned aerial vehicle, clamping structure, heat radiation structure, inflation control structure and cleans the structure, protective frame fixed mounting is on ground service loading board, clamping structure establishes on ground service loading board, just fixed connection between ground service loading board and the clamping structure, clamping structure includes two centre gripping gasbags and two inflation connecting pipes. The utility model discloses structural configuration is reasonable relatively, and the fixed effect of unmanned aerial vehicle ground service car behind receiving unmanned aerial vehicle is better, and is perfect to unmanned aerial vehicle's protection work, is difficult for causing unmanned aerial vehicle's damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service car.
Background
The principle of the unmanned plane is that the unmanned plane is operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and along with the generalization of the unmanned plane, the unmanned plane is also used for shooting scenery and VLOG of ordinary users, the video or photo field of vision shot by the unmanned plane is wider, and when the unmanned plane takes a large-scale shooting task, the unmanned plane needs to follow a ground service vehicle of the unmanned plane for background guarantee of the unmanned plane;
however, the fixing effect of the existing ground service vehicle of the unmanned aerial vehicle after receiving the unmanned aerial vehicle is poor, the protection work of the unmanned aerial vehicle is incomplete, and the damage to the unmanned aerial vehicle is easily caused.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle fixing device on the unmanned aerial vehicle ground service car that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an unmanned aerial vehicle fixing device on an unmanned aerial vehicle ground service vehicle comprises a ground service bearing plate, a protective frame, an unmanned aerial vehicle, a clamping structure, a heat dissipation structure, an inflation control structure and a cleaning structure, wherein the protective frame is fixedly arranged on the ground service bearing plate, the clamping structure is arranged on the ground service bearing plate, the ground service bearing plate is fixedly connected with the clamping structure, the clamping structure comprises two clamping air bags and two inflation connecting pipes, one ends of the inflation connecting pipes are fixedly connected onto the corresponding clamping air bags, the inflation control structure is arranged on the protective frame, the protective frame is fixedly connected with the inflation control structure, the inflation control structure is connected with the clamping air bags through the two inflation connecting pipes, a cleaning structure is further arranged in the protective frame, and the cleaning structure comprises two moving seats, two gears, two racks and a cleaning brush rod, the movable seat is provided with a threaded hole, the threaded hole is internally threaded with a screw rod, the screw rod is also rotatably connected to the protective frame, and the inflation control structure and the heat dissipation structure are connected with the cleaning structure through the screw rod.
Preferably, the shifting chute has all been seted up on the both sides inner wall of protective frame, remove seat slidable mounting in the shifting chute that corresponds, two one side that the removal seat is close to each other all rotates installs the dwang, two fixed connection is at the both ends of cleaning the brush-holder stud respectively, two the equal fixed connection of gear is on two dwangs, two the equal fixed connection of rack is in protective frame, rack and the gear engagement who corresponds.
Preferably, the inflation control structure comprises a control box, a piston push plate, a threaded rod, a first belt wheel, a motor, a second belt wheel and a third belt wheel, the third belt wheel is fixedly connected to one end of the lead screw, the control box is fixedly installed on one side of the protective frame, the piston push plate is connected in the control box in a sliding mode, the threaded rod is fixedly connected to one side of the piston push plate, the threaded rod is connected to the control box in a sliding mode, and the first belt wheel is connected to the threaded rod in a threaded mode.
Preferably, first band pulley rotates with one side of control box to be connected, and motor fixed mounting is on the ground service loading board, and second band pulley fixed connection is on the output shaft of motor, and first band pulley, second band pulley and third band pulley transmission are connected with same belt.
Preferably, heat radiation structure includes two dead levers, two blades, two second sprocket and first sprocket, and two louvres have been seted up in the one end of lead screw to first sprocket fixed connection, one side of protection frame, and the dead lever rotates to be installed in the louvre that corresponds, and second sprocket fixed connection is in the one end of the dead lever that corresponds, and blade fixed connection is at the other end of the dead lever that corresponds, and two second sprockets and first sprocket transmission are connected with same chain.
Compared with the prior art, the beneficial effects of the utility model reside in that:
the scheme has the advantages that the clamping and fixing of the unmanned aerial vehicle are realized by inflating the two clamping air bags, the unmanned aerial vehicle can be well attached to realize fixing, the fixing effect is improved, the surface of the clamping air bags is in soft contact with the unmanned aerial vehicle, the unmanned aerial vehicle is well protected, clamping damage to the unmanned aerial vehicle during clamping is avoided, in the process of clamping the unmanned aerial vehicle, part of rotating force can be distributed to the lead screw, the lead screw drives the cleaning brush rod to move, the cleaning brush rod can automatically clean the surface of the borne unmanned aerial vehicle, and the air in the protective frame can be accelerated to flow after the unmanned aerial vehicle falls down and is fixed, so that the heat dissipation effect of the unmanned aerial vehicle is improved; the utility model discloses structural configuration is reasonable relatively, and the fixed effect of unmanned aerial vehicle ground service car behind receiving unmanned aerial vehicle is better, and is perfect to unmanned aerial vehicle's protection work, is difficult for causing unmanned aerial vehicle's damage.
Drawings
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle fixing device on an unmanned aerial vehicle ground service vehicle according to the present invention;
fig. 2 is a schematic view of a main view structure of the fixing device of the unmanned aerial vehicle on the ground service vehicle of the unmanned aerial vehicle;
fig. 3 is the utility model provides a partial structure schematic diagram of a of unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service car.
In the figure: 1. a ground service carrying plate; 2. a protective frame; 3. an unmanned aerial vehicle; 4. clamping the air bag; 5. a control box; 6. a piston push plate; 7. a threaded rod; 8. a first pulley; 9. a motor; 10. a second pulley; 11. a screw rod; 12. a third belt pulley; 13. a movable seat; 14. cleaning the brush rod; 15. a gear; 16. a rack; 17. a first sprocket; 18. a blade; 19. a second sprocket.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Unless otherwise defined, technical or scientific terms used herein shall have the ordinary meaning as understood by one of ordinary skill in the art to which this invention belongs. The use of "first," "second," and similar terms in the description and in the claims does not indicate any order, quantity, or importance, but rather is used to distinguish one element from another. Also, the use of the terms "a" or "an" and the like do not denote a limitation of quantity, but rather denote the presence of at least one.
Referring to fig. 1-3, an unmanned aerial vehicle fixing device on an unmanned aerial vehicle ground service vehicle comprises a ground service bearing plate 1, a protective frame 2, an unmanned aerial vehicle 3, a clamping structure, a heat dissipation structure, an inflation control structure and a cleaning structure, wherein the protective frame 2 is fixedly arranged on the ground service bearing plate 1, the clamping structure is arranged on the ground service bearing plate 1, the ground service bearing plate 1 is fixedly connected with the clamping structure, the clamping structure comprises two clamping air bags 4 and two inflation connecting pipes, the clamping and fixing of the unmanned aerial vehicle 3 are realized by inflating the two clamping air bags 4, not only can the unmanned aerial vehicle be well attached to realize the fixing, the unmanned aerial vehicle 3 is well protected, one ends of the inflation connecting pipes are fixedly connected to the corresponding clamping air bags 4, the inflation control structure is arranged on the protective frame 2, the protective frame 2 is fixedly connected with the inflation control structure, and the inflation control structure is connected with the clamping air bags 4 through the two inflation connecting pipes, still set up in protective frame 2 and clean the structure, at centre gripping unmanned aerial vehicle 3's in-process, can also distribute a part of turning force to lead screw 11, make lead screw 11 drive clean brush-holder stud 14 and move, clean the structure and include two removal seats 13, two gears 15, two racks 16 and clean brush-holder stud 14, remove and set up threaded hole on the seat 13, screw hole internal thread installs lead screw 11, lead screw 11 also rotates simultaneously and connects on protective frame 2, inflation control structure and heat radiation structure all are connected with cleaning the structure through lead screw 11, can also accelerate the flow to the air in protective frame 2 after unmanned aerial vehicle 3 falls down to fix, thereby promote unmanned aerial vehicle 3's radiating effect.
In this embodiment, the shifting chute has all been seted up on the both sides inner wall of protective frame 2, remove 13 slidable mounting of seat in the shifting chute that corresponds, two one sides that remove 13 mutual close to all rotate and install the dwang, the one end difference fixed connection that two dwangs are close to each other is at the both ends of cleaning brush-holder stud 14, the equal fixed connection of two gears 15 is on two dwangs, the equal fixed connection of two racks 16 is in protective frame 2, rack 16 and the 15 meshing of the gear that correspond, remove 13 drive of seat and clean brush-holder stud 14 and the 15 removal of gear, take place to rotate after gear 15 and the 16 meshing of rack, steerable brush-holder stud 14 that cleans rotates at the removal in-process.
In this embodiment, the inflation control structure includes control box 5, piston push pedal 6, threaded rod 7, first band pulley 8, motor 9, second band pulley 10 and third band pulley 12, third band pulley 12 fixed connection is in the one end of lead screw 11, control box 5 fixed mounting is in one side of protecting frame 2, 6 sliding connection of piston push pedal are in control box 5, 7 fixed connection of threaded rod is in one side of piston push pedal 6, 7 sliding connection of threaded rod is on control box 5, 8 threaded connection of first band pulley are on threaded rod 7, 8 drive threaded rod 7 and the removal of piston push pedal 6 of first band pulley, the gas in piston push pedal 6 will control box 5 is through propelling movement to two centre gripping gasbags 4 from its connecting pipe in.
In this embodiment, first band pulley 8 rotates with one side of control box 5 to be connected, and motor 9 fixed mounting is on ground service loading board 1, and second band pulley 10 fixed connection is on the output shaft of motor 9, and first band pulley 8, second band pulley 10 and the 12 transmission of third band pulley are connected with same belt, and motor 9 drives second band pulley 10 and rotates, and second band pulley 10 drives the belt motion, and the belt drives first band pulley 8 and the rotation of third band pulley 12 simultaneously.
In this embodiment, heat radiation structure includes two dead levers, two blades 18, two second sprocket 19 and first sprocket 17, first sprocket 17 fixed connection is in the one end of lead screw 11, two louvres have been seted up to one side of protection frame 2, the dead lever rotates and installs in the louvre that corresponds, 19 fixed connection of second sprocket is in the one end of the dead lever that corresponds, 18 fixed connection of blade is at the other end of the dead lever that corresponds, two second sprocket 19 and the transmission of first sprocket 17 are connected with same chain, lead screw 11 still controls first sprocket 17 and rotates, first sprocket 17 rotates with the help of two second sprocket 19 of chain control, 19 transmission blade 18 of second sprocket rotate, the rotation of two blades 18 can drive the air flow in the louvre.
In this embodiment, after the unmanned aerial vehicle 3 stops on the ground service bearing plate 1, the motor 9 drives the second belt wheel 10 to rotate, the second belt wheel 10 drives the belt to move, the belt drives the first belt wheel 8 and the third belt wheel 12 to rotate simultaneously, the first belt wheel 8 drives the threaded rod 7 and the piston push plate 6 to move, the piston push plate 6 pushes the gas in the control box 5 into the two clamping airbags 4 through the connecting pipe, the two clamping airbags 4 can clamp the unmanned aerial vehicle 3 after being expanded, the third belt wheel 12 can drive the lead screw 11 to rotate, the lead screw 11 controls the moving seat 13 to move, the moving seat 13 drives the cleaning brush rod 14 and the gear 15 to move, the gear 15 is meshed with the rack 16 to rotate, the cleaning brush rod 14 can be controlled to rotate in the moving process, the lead screw 11 also controls the first chain wheel 17 to rotate, the first chain wheel 17 controls the two second chain wheels 19 to rotate by means of a chain, the second chain wheel 19 drives the blades 18 to rotate, the rotation of the two blades 18 drives the air flow in the heat dissipation holes.
The utility model discloses the technological progress that prior art obtained relatively is: the utility model discloses structural configuration is reasonable relatively, and the fixed effect of unmanned aerial vehicle ground service car after receiving unmanned aerial vehicle 3 is better, and is perfect to unmanned aerial vehicle 3's protection work, is difficult for causing unmanned aerial vehicle 3's damage.
Claims (6)
1. An unmanned aerial vehicle fixing device on an unmanned aerial vehicle ground service vehicle comprises a ground service bearing plate (1), a protective frame (2), a clamping structure, a heat dissipation structure, an inflation control structure and a cleaning structure, and is characterized in that the protective frame (2) is fixedly installed on the ground service bearing plate (1), the clamping structure is arranged on the ground service bearing plate (1), the ground service bearing plate (1) is fixedly connected with the clamping structure, the clamping structure comprises two clamping airbags (4) and two inflation connecting pipes, one ends of the inflation connecting pipes are fixedly connected onto the corresponding clamping airbags (4), the inflation control structure is arranged on the protective frame (2), the protective frame (2) is fixedly connected with the inflation control structure, the inflation control structure is connected with the clamping airbags (4) through the two inflation connecting pipes, the cleaning structure is further arranged in the protective frame (2), the cleaning structure comprises two moving seats (13), two gears (15), two racks (16) and a cleaning brush rod (14), a threaded hole is formed in each moving seat (13), a screw rod (11) is installed in an internal thread of the threaded hole, the screw rod (11) is also rotatably connected to the protection frame (2) at the same time, and the inflation control structure and the heat dissipation structure are connected with the cleaning structure through the screw rod (11).
2. The unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle of claim 1, characterized by, still include unmanned aerial vehicle (3), unmanned aerial vehicle (3) are placed on the top of ground service loading board (1), and unmanned aerial vehicle (3) contact with two centre gripping gasbags (4).
3. The unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle of claim 1, characterized in that, the shifting chute has all been seted up on the both sides inner wall of protective frame (2), remove seat (13) slidable mounting in the corresponding shifting chute, two one side that removes seat (13) and be close to each other all rotates installs the dwang, two fixed connection is at the both ends of cleaning brush-holder stud (14), two respectively to the one end that the dwang is close to each other the equal fixed connection of gear (15) is on two dwangs, two the equal fixed connection of rack (16) is in protective frame (2), rack (16) and corresponding gear (15) meshing.
4. The fixing device of claim 1, wherein the moving seat (13) is provided with a rotating groove, and the rotating rod is rotatably mounted in the rotating groove.
5. The unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle of claim 1, characterized in that, protective frame (2) passes through screw fixed connection at the top of ground service loading board (1).
6. The unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle of claim 1, characterized in that, the both sides of protection frame (2) all seted up the auxiliary hole, lead screw (11) rotate to be installed in the auxiliary hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202120569055.XU CN214607264U (en) | 2021-03-19 | 2021-03-19 | Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202120569055.XU CN214607264U (en) | 2021-03-19 | 2021-03-19 | Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
CN214607264U true CN214607264U (en) | 2021-11-05 |
Family
ID=78395849
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202120569055.XU Active CN214607264U (en) | 2021-03-19 | 2021-03-19 | Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN214607264U (en) |
-
2021
- 2021-03-19 CN CN202120569055.XU patent/CN214607264U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5569755B2 (en) | Portable and removable device for powering the bicycle | |
CN109390815B (en) | Make things convenient for outdoor socket for electric bicycle that charges and protection nature is good | |
US3912039A (en) | Bicycle drive apparatus | |
CN112007810B (en) | Paint spraying apparatus is used in production of electric motorcycle car accessory | |
CN214607264U (en) | Unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service vehicle | |
CN206248988U (en) | One kind is used for pilotless automobile camera eyeglass dehydrating unit | |
CN117206568B (en) | Multi-degree-of-freedom automatic drilling crawling robot and crawling method | |
CN112045519A (en) | Bolt thread processing equipment | |
CN106553717A (en) | A kind of push-and-pull bicycle mechanism | |
CN207547715U (en) | A kind of device for milling aluminum-alloy wheel window burr | |
CN205989218U (en) | A kind of many sizes pipe outer surface polishing tool | |
CN113579948A (en) | Outer wall grinding device of cavity hexagonal spare | |
FR2837123A1 (en) | Cleaning unit to degrease the surfaces of aircraft engine nacelles, is positioned and operated by radio control to deliver a high speed jet stream of dry compressed air containing dry ice particles at the surface | |
CN111293561A (en) | Data line core stripping and tin immersion welding device | |
EP2014913A2 (en) | System for recovering, channelling and using natural air currents or those created by the movement of a transport unit with a view to their conversion to electrical power | |
CN110952402A (en) | Spike removing device for railway dismounting and repairing system | |
CN111645930A (en) | Packaging and film covering device for spinning rubber roll | |
CN213004560U (en) | Automatic polishing and wax spraying system equipment | |
CN205872003U (en) | Wheel snow removal device | |
CN105328637B (en) | A kind of screw rod docking facilities | |
CN218284430U (en) | Mechanism for automatically screwing gun drill chuck | |
CN113858996B (en) | Highly integrated vehicle-mounted charging system with rainproof and dehumidifying functions | |
CN114940227B (en) | Side pedal support bracket for automobile assembly | |
CN212942162U (en) | UV light-cured varnish spraying waste gas recovery treatment equipment | |
CN217528516U (en) | Auxiliary film laminating device for power battery side plate machining |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |