CN213649439U - Aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function - Google Patents
Aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function Download PDFInfo
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- CN213649439U CN213649439U CN202021199012.9U CN202021199012U CN213649439U CN 213649439 U CN213649439 U CN 213649439U CN 202021199012 U CN202021199012 U CN 202021199012U CN 213649439 U CN213649439 U CN 213649439U
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- unmanned aerial
- aerial vehicle
- wheel
- supporting base
- fixed
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Abstract
The utility model provides an aviation ground service vehicle unmanned aerial vehicle fixed bolster with anticollision early warning function, which comprises a supporting base and an airplane wheel fixing box; six dampers in total are fixedly and symmetrically arranged on two sides in the supporting base. The setting of the fixed box of wheel, be favorable to improving the security of using, it is fixed with the wheel clamp through solid fixed splint to press from both sides during fixed, the swash plate at the fixed box top of wheel can prevent the outside roll-off of wheel, when the transport vechicle frequently brakes or emergency brake, unmanned aerial vehicle forward inertial impulse can be used in on the fixed box of wheel, at this moment the fixed box of wheel just can slide forward in the support base inboard through the under bracing piece of bottom, the attenuator can provide reverse buffer power to it simultaneously, thereby reduce unmanned aerial vehicle's atress, and when the brake is too urgent, the under bracing piece can contact and press normally closed button switch, at this moment normally closed button switch can control the alarm of carriage internal connection and report to the police, the suggestion driver slowly brakes, avoid unmanned aerial vehicle to drop.
Description
Technical Field
The utility model belongs to the technical field of the air transportation device, more specifically say, in particular to aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function.
Background
Unmanned aerial vehicle is unmanned aerial vehicle for short, is the unmanned vehicles who utilizes radio remote control equipment and self-contained program control device to control, and unmanned aerial vehicle is the general name of unmanned aerial vehicle in fact, can divide into from the technical perspective: the unmanned helicopter, the unmanned fixed-wing aircraft, the unmanned multi-rotor aircraft, the unmanned airship and the unmanned parachute-wing aircraft are similar to the manned aircraft, and have the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like. Along with the high-speed development of present science and technology, unmanned aerial vehicle's use is also more and more extensive, and unmanned aerial vehicle needs ground service car to transport before taking off usually, then needs the fixed bolster to fix unmanned aerial vehicle in the transportation.
For example, application number is 201820198772.4's patent, discloses an unmanned aerial vehicle fixing device on unmanned aerial vehicle ground service car, including the installation base, the top of installation base is provided with the layer board, the spacing arc of bottom fixedly connected with of layer board, the inside of spacing arc is provided with the adjusting ball, the bottom and the installation base fixed connection of adjusting ball, the outside of adjusting ball and the inner wall contact of spacing arc, the left and right sides of installation base all is provided with spacing section of thick bamboo. The utility model discloses a, through the system that first articulated seat, down tube and the articulated seat of second constitute, can be when the layer board atress, slide in the spout through the slider, can promote the fixed block and remove in spacing section of thick bamboo, the frictional force between reduction fixed block that the gyro wheel can be very big and the spacing section of thick bamboo inner wall, through the system that fixing base, elastic rod, stable piece and ring constitute, can play absorbing effect, more can carry out the shock attenuation to unmanned aerial vehicle when ground service vehicle transports unmanned aerial vehicle.
Based on above-mentioned search discovery, above-mentioned patent combines most unmanned aerial vehicle fixed bolster among the prior art simultaneously, and it has following problem when using: present unmanned aerial vehicle fixed bolster is many only to have slight cushioning effect, and in the transportation, the transport vechicle may need frequent brake or even hard brake, and this unmanned aerial vehicle can appear a forward impulsive force because of inertia at this moment, but the structure to its buffering is not had to the power of this direction, and fixed position is in case not hard up then produces the collision easily moreover.
Therefore, in view of the above, research and improvement are performed on the existing structure and defects, and a fixing bracket for an unmanned aerial vehicle of an aviation ground service vehicle with an anti-collision early warning function is provided, so as to achieve the purpose of higher practical value.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides an aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function to solve present unmanned aerial vehicle fixed bolster and only have slight cushioning effect more, in the transportation, the transport vechicle may need frequent brake or even emergency brake, this moment unmanned aerial vehicle can appear a forward impulsive force because of inertia, but the power of this direction does not have the structure to its buffering, and fixed position in case not hard up then produces the problem of collision easily moreover.
The utility model discloses purpose and efficiency of aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function are reached by following concrete technical means:
an unmanned aerial vehicle fixing support with an anti-collision early warning function for an aviation ground service vehicle comprises a supporting base and a wheel fixing box; six dampers in total are fixedly and symmetrically arranged on two sides in the supporting base; the bottom of the airplane wheel fixing box is fixedly and symmetrically connected with two lower supporting blocks; the two lower supporting blocks are movably embedded and installed on the inner side of the supporting base; a normally closed button switch is fixedly arranged on one side inside the supporting base; a fixed clamping plate is movably arranged on the inner side of the airplane wheel fixing box; one side of the wheel fixing box is further provided with a screw rod in an embedded mode through threads, one end of the screw rod is rotatably connected with one side of the fixing clamping plate through a rotating shaft, and the other end of the screw rod is fixedly provided with a rotating handle.
Furthermore, a plurality of transversely-arranged rollers are fixedly arranged at the bottom of the lower supporting blocks, a plurality of roller grooves corresponding to the positions are also formed in the inner side of the bottom of the supporting base, a guide block is fixedly arranged on each of the front side and the rear side of each of the two lower supporting blocks, and a corresponding guide groove is also formed in each of the front side and the rear side of the inside of the supporting base.
Furthermore, the front side and the rear side of the fixed clamping plate are both fixedly provided with two vertically symmetrical convex blocks, the front side and the rear side of the inside of the wheel fixing box are also both provided with two corresponding guide grooves, the position of the screw rod embedded with the wheel fixing box is a threaded hole, and the screw rod can drive the fixed clamping plate to move left and right when rotating.
Furthermore, one side of the top of the wheel fixing box is provided with a plate-shaped structure inclining towards the inner side.
Further, the normally closed button switch is installed on one side of a vertical plate on the inner side of the supporting base, the side of the vertical plate and one side of a main cylinder of the damper are located on the same vertical surface, and one side of each of the two lower supporting blocks can be attached to one end of each of the two sets of dampers respectively under the normal condition.
Compared with the prior art, the utility model discloses following beneficial effect has:
the setting of the fixed box of wheel, be favorable to improving the security of using, it is fixed with the wheel clamp through solid fixed splint to press from both sides during fixed, the swash plate at the fixed box top of wheel can prevent the outside roll-off of wheel, when the transport vechicle frequently brakes or emergency brake, unmanned aerial vehicle forward inertial impulse can be used in on the fixed box of wheel, at this moment the fixed box of wheel just can slide forward in the support base inboard through the under bracing piece of bottom, the attenuator can provide reverse buffer power to it simultaneously, thereby reduce unmanned aerial vehicle's atress, and when the brake is too urgent, the under bracing piece can contact and press normally closed button switch, at this moment normally closed button switch can control the alarm of carriage internal connection and report to the police, the suggestion driver slowly brakes, avoid unmanned aerial vehicle to drop.
Drawings
Fig. 1 is a schematic side view of the present invention.
Fig. 2 is a schematic view of the structure of the present invention.
Fig. 3 is the schematic diagram of the partially-cut shaft side structure of the present invention.
Fig. 4 is the utility model discloses partially dissect and the axle side structure schematic diagram after the bottom suspension strut removes.
Fig. 5 is a schematic view of the structure of the wheel securing box on the bottom side.
In the drawings, the corresponding relationship between the component names and the reference numbers is as follows:
1. a support base; 2. an airplane wheel fixing box; 3. fixing the clamping plate; 4. a screw; 5. a lower support block; 6. a damper; 7. a normally closed push button switch.
Detailed Description
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
As shown in figures 1 to 5:
the utility model provides an aviation ground service vehicle unmanned aerial vehicle fixed bolster with anticollision early warning function, including supporting base 1 and wheel fixing box 2; six dampers 6 are fixedly and symmetrically arranged on two sides in the supporting base 1; the bottom of the airplane wheel fixing box 2 is fixedly and symmetrically connected with two lower supporting blocks 5; one side of the top of the airplane wheel fixing box 2 is also provided with a plate-shaped structure inclining towards the inner side, and the inclined plate at the top of the airplane wheel fixing box 2 can prevent the airplane wheel from sliding outwards after the airplane wheel is fixed; the two lower supporting blocks 5 are movably embedded and arranged on the inner side of the supporting base 1; a normally closed button switch 7 is fixedly arranged on one side inside the supporting base 1; a fixed clamping plate 3 is movably arranged on the inner side of the airplane wheel fixing box 2; two convex blocks which are symmetrical up and down are fixedly arranged on the front side and the rear side of the fixed clamping plate 3, two corresponding guide grooves are also formed in the front side and the rear side of the interior of the airplane wheel fixed box 2, the position where the screw rod 4 is embedded with the airplane wheel fixed box 2 is a threaded hole, the screw rod 4 can drive the fixed clamping plate 3 to move left and right when rotating, after the unmanned aerial vehicle is hoisted, the wheel is aligned with the airplane wheel fixed box 2 and descends, the airplane wheel is clamped into the inner side of the airplane wheel fixed box 2, the screw rod 4 is rotated clockwise, and the fixed clamping plate 3 is pushed to move forward to tightly; one side of the wheel fixing box 2 is further provided with a screw rod 4 in an embedded mode through threads, one end of the screw rod 4 is rotatably connected with one side of the fixing clamping plate 3 through a rotating shaft, and the other end of the screw rod 4 is fixedly provided with a rotating handle.
Wherein, the fixed gyro wheel that is provided with a plurality of transverse arrangement in bottom of lower supporting shoe 5, the bottom inboard of supporting base 1 also is provided with the gyro wheel groove that a plurality of positions correspond, the side still all is fixed to be provided with a guide block around two lower supporting shoes 5, both sides also all are provided with the guide way that corresponds around the inside of supporting base 1, when the transport vechicle frequently brakes or emergency brake, the forward inertial impulsive force of unmanned aerial vehicle can act on wheel set box 2, at this moment wheel set box 2 just can slide forward in supporting base 1 inboard through the lower supporting shoe 5 of bottom, attenuator 6 can provide reverse buffer power to it simultaneously, thereby reduce unmanned aerial vehicle's atress.
Wherein, normally closed button switch 7 installs in a vertical board one side of supporting base 1 inboard, and this one side of vertical board is located same vertical face with master cylinder one side of attenuator 6, one side of two lower supporting shoe 5 under the normal condition also can laminate with the one end of two sets of attenuators 6 respectively, when the brake is too urgent, lower supporting shoe 5 can contact and press normally closed button switch 7, at this moment normally closed button switch 7 can control the alarm of carriage internal connection and report to the police, the suggestion driver slowly brakes, avoid unmanned aerial vehicle collision that drops.
The specific use mode and function of the embodiment are as follows:
in the utility model, when the device is used for fixing the unmanned aerial vehicle, the device is fixed on the vehicle supporting plate through the fixing holes at the two sides of the supporting base 1 according to the position of the wheels of the unmanned aerial vehicle, the normally closed button switch 7 passes through the threading hole on the supporting base 1 through the lead and is connected with the alarm in the cab and powered on, then the wheels are aligned with the wheel fixing box 2 and are lowered after the unmanned aerial vehicle is hoisted, the wheels are clamped into the inner side of the wheel fixing box 2, at the moment, the screw rod 4 is rotated clockwise, the fixing splint 3 is pushed to move forwards to tightly push the wheels to fix, and the inclined plate at the top of the wheel fixing box 2 can also prevent the wheels from sliding outwards, when the transport vehicle is frequently braked or suddenly braked, the forward inertial impulsive force of the unmanned aerial vehicle can act on the wheel fixing box 2, at the moment, the wheel fixing box 2 can slide, simultaneously attenuator 6 can provide reverse buffer power to it, thereby reduce unmanned aerial vehicle's atress, and when the brake is too urgent, bottom suspension splice 5 can contact and press normally closed button switch 7, at this moment normally closed button switch 7 can control the alarm of carriage internal connection and report to the police, the suggestion driver slowly brakes, avoid unmanned aerial vehicle to drop the collision, normally closed button switch 7 model in this application is KFC-V-206KT, its concrete working method and line connection are the known mature technique in this field, do not do the detailed tired statement here.
Claims (5)
1. The utility model provides an aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function which characterized in that: comprises a supporting base (1) and an airplane wheel fixing box (2); six dampers (6) are fixedly and symmetrically arranged on two sides in the supporting base (1); the bottom of the airplane wheel fixing box (2) is fixedly and symmetrically connected with two lower supporting blocks (5); the two lower supporting blocks (5) are movably embedded and installed on the inner side of the supporting base (1); a normally closed button switch (7) is fixedly arranged on one side in the supporting base (1); a fixed clamping plate (3) is movably arranged on the inner side of the airplane wheel fixing box (2); one side of the wheel fixing box (2) is further provided with a screw rod (4) in an embedded mode through threads, one end of the screw rod (4) is rotatably connected with one side of the fixing clamping plate (3) through a rotating shaft, and the other end of the screw rod (4) is fixedly provided with a rotating handle.
2. The unmanned aerial vehicle fixing support with the anti-collision early warning function as claimed in claim 1, wherein: the bottom of the lower supporting block (5) is fixedly provided with a plurality of transversely arranged rollers, the inner side of the bottom of the supporting base (1) is also provided with a plurality of roller grooves corresponding to the positions, the front side and the rear side of the two lower supporting blocks (5) are also fixedly provided with a guide block, and the front side and the rear side of the inside of the supporting base (1) are also provided with a corresponding guide groove.
3. The unmanned aerial vehicle fixing support with the anti-collision early warning function as claimed in claim 1, wherein: the front side and the rear side of the fixed clamping plate (3) are both fixedly provided with two vertically symmetrical convex blocks, the front side and the rear side of the interior of the wheel fixing box (2) are also both provided with two corresponding guide grooves, the position of the screw rod (4) embedded with the wheel fixing box (2) is a threaded hole, and the screw rod (4) can drive the fixed clamping plate (3) to move leftwards and rightwards when rotating.
4. The unmanned aerial vehicle fixing support with the anti-collision early warning function as claimed in claim 1, wherein: one side of the top of the airplane wheel fixing box (2) is also provided with a plate-shaped structure inclining towards the inner side.
5. The unmanned aerial vehicle fixing support with the anti-collision early warning function as claimed in claim 1, wherein: the normally closed button switch (7) is installed on one side of a vertical plate on the inner side of the supporting base (1), the side of the vertical plate and one side of a main cylinder of the damper (6) are located on the same vertical surface, and one side of each of the two lower supporting blocks (5) can be attached to one end of each of the two groups of dampers (6) under a normal condition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021199012.9U CN213649439U (en) | 2020-06-25 | 2020-06-25 | Aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021199012.9U CN213649439U (en) | 2020-06-25 | 2020-06-25 | Aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213649439U true CN213649439U (en) | 2021-07-09 |
Family
ID=76683449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021199012.9U Expired - Fee Related CN213649439U (en) | 2020-06-25 | 2020-06-25 | Aviation ground service car unmanned aerial vehicle fixed bolster with anticollision early warning function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213649439U (en) |
-
2020
- 2020-06-25 CN CN202021199012.9U patent/CN213649439U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20211124 Address after: 200540 4th floor, building 5, No. 168, Lane 6495, Tingwei Road, Jinshan Industrial Zone, Jinshan District, Shanghai (Metalworking economic community) Patentee after: Yiying (Shanghai) aircraft Co.,Ltd. Address before: 314001 56 Jishui Road, Nanhu District, Jiaxing City, Zhejiang Province Patentee before: Yang Guowei |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210709 |