CN212501085U - Load quick replacement device for vertical take-off and landing fixed wing unmanned aerial vehicle - Google Patents
Load quick replacement device for vertical take-off and landing fixed wing unmanned aerial vehicle Download PDFInfo
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- CN212501085U CN212501085U CN202021207251.4U CN202021207251U CN212501085U CN 212501085 U CN212501085 U CN 212501085U CN 202021207251 U CN202021207251 U CN 202021207251U CN 212501085 U CN212501085 U CN 212501085U
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Abstract
The utility model discloses a vertical take-off and landing fixed wing unmanned aerial vehicle load quick replacement device, which comprises a body, the inboard of the body is provided with a bolt fixing seat, one side of the bolt fixing seat is respectively provided with a camera module and a pan-tilt module, the camera module consists of a task bin cover plate, a hook, a support plate, a cross-groove flat round head screw, a spring bolt, a vibration damping plate, a camera, a cover plate and a non-metal hexagonal locking nut, the pan-tilt module consists of a task bin cover plate II, a hook II, a support plate II, a cross-groove flat round head screw, a spring bolt II, a vibration damping plate II, a three-degree-of-freedom pan-tilt, a pan-tilt and a non-metal hexagonal locking nut II, the utility model discloses on one hand, installation can be realized without punching, and the appearance, resistance and structural strength of the unmanned aerial vehicle can not be influenced simultaneously, on the other hand, the modules with different functions can be conveniently replaced, and time and labor are saved.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is VTOL fixed wing unmanned aerial vehicle load quick replacement device.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
However, the existing vertical take-off and landing unmanned aerial vehicle mainly has the following disadvantages:
present unmanned aerial vehicle task load snap-on is in unmanned aerial vehicle's cabin, need trompil in cabin bottom, different holes need to be opened to different loads, traditional unmanned aerial vehicle task load is changed and is a very troublesome thing, the dismantlement load of making a round trip has the influence to the quality of equipment itself, still open various different holes in the fuselage below simultaneously, lead to the unmanned aerial vehicle outward appearance, resistance and structural strength receive the influence simultaneously, firstly, unmanned aerial vehicle changes the consuming time power of load like this, make load life shorten, secondly lead to unmanned aerial vehicle's outward appearance and structural strength step-down, there is the flight risk.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a VTOL fixed wing unmanned aerial vehicle load quick replacement device, with solve present unmanned aerial vehicle task load snap-on in unmanned aerial vehicle's the cabin among the above-mentioned background art, need trompil in the cabin bottom, different holes need to be opened to different loads, traditional unmanned aerial vehicle task load is changed and is a very troublesome thing, the dismantlement load of making a round trip has the influence to the quality of equipment itself, still open the hole of various differences in fuselage below simultaneously, lead to the unmanned aerial vehicle outward appearance, resistance and structural strength receive the influence simultaneously, firstly like this unmanned aerial vehicle changes the consuming time power of load, make load life shorten, secondly lead to unmanned aerial vehicle's outward appearance and structural strength step-down, there is the problem of flight risk.
In order to achieve the above object, the utility model provides a following technical scheme: vertical take-off and landing fixed wing unmanned aerial vehicle load quick replacement device, including the fuselage, the bolt fixing base is installed to the fuselage inboard, camera module and cloud platform module are installed respectively to bolt fixing base one side, camera module comprises task cang apron, couple, backup pad, the flat button head screw of cross recess, spring bolt, damping plate, camera, apron and nonmetal hex lock nut, the cloud platform module comprises task cang apron, couple, backup pad, the flat button head screw of cross recess, spring bolt, damping plate, three degree of freedom cloud platforms, apron and nonmetal hex lock nut No. two.
Preferably, a hook is fixedly connected to one end of the task bin cover plate, a supporting plate is arranged on the outer wall of the task bin cover plate and connected with the task bin cover plate through a cross groove flat round head screw, and a spring bolt is installed on one side of the supporting plate.
Preferably, a vibration damping plate is installed on the inner side of the task bin cover plate, and a camera is installed on one side of the vibration damping plate.
Preferably, an apron is installed to damping plate one side, an apron outer wall is equipped with nonmetal hexagonal lock nut No. one, and nonmetal hexagonal lock nut rotates with the flat button head screw of cross recess and is connected.
Preferably, No. two couples of task storehouse apron one end fixedly connected with, No. two task storehouse apron outer walls are equipped with the backup pad No. two, and No. two backup pads link to each other with No. two task storehouse apron through No. two cross recess flat round head screws, No. two spring bolts are installed to No. two backup pads one side.
Preferably, a second vibration damping plate is installed on the inner side of the second task cabin cover plate, and a three-degree-of-freedom holder is installed on one side of the second vibration damping plate.
Preferably, No. two apron are installed to No. two damping plates one side, No. two apron outer walls are equipped with No. two nonmetal hexagonal lock nuts, and No. two nonmetal hexagonal lock nuts and No. two cross recess flat round head screws rotate to be connected.
The utility model provides a VTOL fixed wing unmanned aerial vehicle load quick replacement device possesses following beneficial effect:
(1) the utility model has the advantages that the front part of the body is provided with the load cabin, meanwhile, the port part of the load cabin is provided with the bolt fixing seat, the first task cabin cover plate is arranged at the inner side of the load cabin, the camera is fixed on the surface of the first task cabin cover plate through the screw, the first cover plate is arranged at the outer side of the camera, the camera module is arranged at the inner side of the load cabin, the second task cabin cover plate is arranged at the inner side of the load cabin, the three-freedom-degree pan-tilt head is fixed on the surface of the second task cabin cover plate through the screw, the second cover plate is arranged at the outer side of the camera, the pan-tilt module is arranged at the inner side of the load cabin, the first hook and the first spring bolt on the first task cabin cover plate are the same as the second hook and the first spring bolt on the second task cabin cover plate in position and structure, the first hook is, need not punch on the one hand and can realize the installation, can not make unmanned aerial vehicle outward appearance, resistance and structural strength influenced simultaneously, on the other hand is convenient for change the module of different effects, labour saving and time saving.
Drawings
Fig. 1 is a schematic structural view of a camera module assembly according to the present invention;
FIG. 2 is a schematic structural view of a cradle head module assembly of the present invention;
fig. 3 is a schematic view of the assembly structure of the camera module according to the present invention;
fig. 4 is the utility model discloses a cloud platform module package assembly sketch map.
In the figure: 1. a body; 2. a bolt fixing seat; 3. a camera module; 301. a first task bin cover plate; 302. a first hook; 303. a first support plate; 304. a first cross-groove round head screw; 305. a first spring bolt; 306. a first damping plate; 307. a camera; 308. a first cover plate; 309. a first non-metal hexagonal locknut; 4. a cradle head module; 401. a second task bin cover plate; 402. a second hook; 403. a second support plate; 404. a second cross-groove round head screw; 405. a second spring bolt; 406. a second damping plate; 407. a three-degree-of-freedom holder; 408. a second cover plate; 409. no. two nonmetal hexagonal lock nuts.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
As shown in fig. 1-4, the utility model provides a technical solution: vertical take-off and landing fixed wing unmanned aerial vehicle load quick replacement device, including fuselage 1, bolt fixing base 2 is installed to 1 inboard of fuselage, camera module 3 and cloud platform module 4 are installed respectively to bolt fixing base 2 one side, camera module 3 comprises task storehouse apron 301, couple 302, a backup pad 303, the flat button head screw 304 of cross recess, spring bolt 305, damping plate 306, camera 307, apron 308 and nonmetal hexagonal lock nut 309, cloud platform module 4 comprises No. two task storehouse apron 401, No. two couples 402, No. two backup pads 403, the flat button head screw 404 of cross recess, No. two spring bolts 405, No. two damping plates 406, three degrees of freedom 407, No. two apron 408 and No. two nonmetal hexagonal lock nuts.
A load cabin is arranged at the front part of a machine body 1, meanwhile, a bolt fixing seat 2 is installed at a port of the load cabin, a first task cabin cover plate 301 is arranged at the inner side of the load cabin, a camera 307 is fixed on the surface of the first task cabin cover plate 301 through a screw, a first cover plate 308 is installed at the outer side of the camera 307, so that a camera module 3 is installed at the inner side of the load cabin, a second task cabin cover plate 401 is arranged at the inner side of the load cabin, a three-degree-of-freedom pan-tilt head 407 is fixed on the surface of the second task cabin cover plate 401 through a screw, a second cover plate 408 is installed at the outer side of the camera 307, so that a pan-tilt head module 4 is installed at the inner side of the load cabin, a first hook 302 and a first spring bolt 305 on the first task cabin cover plate 301 are identical in position and structure with a second hook 402 and a first spring bolt 405, and link to each other with 2 pegs graft of bolt fixing base through spring bolt, need not punch on the one hand and can realize the installation, can not make unmanned aerial vehicle outward appearance, resistance and structural strength receive the influence simultaneously, and on the other hand is convenient for change the module of different effects, labour saving and time saving.
A couple 302 of task storehouse apron 301 one end fixedly connected with, a task storehouse apron 301 outer wall is equipped with backup pad 303 No. one, and backup pad 303 links to each other with task storehouse apron 301 through a cross recess flat button head screw 304 No. one, a spring bolt 305 is installed to backup pad 303 one side.
A first vibration damping plate 306 is installed on the inner side of the first task cabin cover plate 301, and a camera 307 is installed on one side of the first vibration damping plate 306.
No. one apron 308 is installed to damping plate 306 one side, No. one apron 308 outer wall is equipped with nonmetal hexagonal lock nut 309 No. one, and nonmetal hexagonal lock nut 309 and the flat button head screw 304 of a cross recess rotate to be connected.
No. two couple 402 of task storehouse apron 401 one end fixedly connected with, No. two task storehouse apron 401 outer walls are equipped with No. two backup pads 403, and No. two backup pads 403 link to each other with No. two task storehouse apron 401 through No. two cross recess flat round head screws 404, No. two spring bolt 405 are installed to No. two backup pads 403 one side.
And a second vibration reduction plate 406 is arranged on the inner side of the second task cabin cover plate 401, and a three-degree-of-freedom holder 407 is arranged on one side of the second vibration reduction plate 406.
No. two apron 408 are installed to No. two damping plate 406 one side, No. two apron 408 outer walls are equipped with No. two nonmetal hexagonal lock nut 409, and No. two nonmetal hexagonal lock nut 409 and No. two cross recess flat round head screws 404 rotate to be connected.
It should be noted that, when the device for rapidly changing the load of the fixed-wing unmanned aerial vehicle for vertical take-off and landing is operated, a bolt fixing seat 2 is installed on the inner side of a machine body 1, a camera module 3 and a pan-tilt module 4 are respectively installed on one side of the bolt fixing seat 2, the camera module 3 is composed of a first task cabin cover plate 301, a first hook 302, a first supporting plate 303, a first cross-groove flat round head screw 304, a first spring bolt 305, a first vibration reduction plate 306, a camera 307, a first cover plate 308 and a first non-metal hexagonal locking nut 309, the pan-tilt module 4 is composed of a second task cabin cover plate 401, a second hook 402, a second supporting plate 403, a second cross-groove flat round head screw 404, a second spring bolt 405, a second vibration reduction plate 406, a pan-tilt 409, a second cover plate 408 and a second non-metal hexagonal locking nut 407, a load cabin is arranged on the front portion of the machine body 1, the first task bin cover plate 301 is arranged at the inner side of the load bin, the camera 307 is fixed on the surface of the first task bin cover plate 301 through a screw, the first task bin cover plate 308 is arranged at the outer side of the camera 307, the camera module 3 is arranged at the inner side of the load bin, the second task bin cover plate 401 is arranged at the inner side of the load bin, the three-freedom-degree tripod head 407 is fixed on the surface of the second task bin cover plate 401 through a screw, the second task bin cover plate 408 is arranged at the outer side of the camera 307, the tripod head module 4 is arranged at the inner side of the load bin, the first hook 302 and the first spring bolt 305 on the first task bin cover plate 301 are identical to the second hook 402 and the first spring bolt 405 on the second task bin cover plate 401 in position and structure, the first hook is hung at the bin opening of the load bin and is connected with the bolt fixing seat 2 through the spring bolt in an inserting, the unmanned aerial vehicle appearance, the resistance and the structural strength are not affected at the same time, so that modules with different functions can be replaced conveniently, and time and labor are saved.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Vertical take-off and landing fixed wing unmanned aerial vehicle load quick replacement device, including fuselage (1), its characterized in that: a bolt fixing seat (2) is arranged on the inner side of the machine body (1), a camera module (3) and a holder module (4) are respectively arranged on one side of the bolt fixing seat (2), the camera module (3) consists of a first task bin cover plate (301), a first hook (302), a first support plate (303), a first cross groove flat round head screw (304), a first spring bolt (305), a first vibration damping plate (306), a camera (307), a first cover plate (308) and a first nonmetal hexagonal locking nut (309), the cradle head module (4) is composed of a second task cabin cover plate (401), a second hook (402), a second support plate (403), a second cross groove flat round head screw (404), a second spring bolt (405), a second vibration damping plate (406), a three-degree-of-freedom cradle head (407), a second cover plate (408) and a second nonmetal hexagonal locking nut (409).
2. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: a couple (302) of task storehouse apron (301) one end fixedly connected with, a task storehouse apron (301) outer wall is equipped with backup pad (303) No. one, and backup pad (303) link to each other with task storehouse apron (301) through a cross recess flat button head screw (304) No. one, a spring bolt (305) is installed to backup pad (303) one side.
3. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: a damping plate (306) is installed on the inner side of the first task bin cover plate (301), and a camera (307) is installed on one side of the damping plate (306).
4. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: no. one apron (308) is installed to damping plate (306) one side, No. one apron (308) outer wall is equipped with nonmetal hexagonal lock nut (309), and nonmetal hexagonal lock nut (309) and a cross recess flat round head screw (304) rotate and be connected.
5. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: no. two tasks storehouse apron (401) one end fixedly connected with couple (402) No. two, No. two task storehouse apron (401) outer wall is equipped with backup pad (403) No. two, and No. two backup pad (403) link to each other with No. two task storehouse apron (401) through No. two cross recess flat round head screws (404), No. two spring bolt (405) are installed to No. two backup pad (403) one side.
6. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: and a second vibration reduction plate (406) is arranged on the inner side of the second task cabin cover plate (401), and a three-degree-of-freedom holder (407) is arranged on one side of the second vibration reduction plate (406).
7. The VTOL fixed-wing UAV load quick change device of claim 1, wherein: no. two apron (408) are installed to No. two damping plate (406) one side, No. two apron (408) outer walls are equipped with No. two nonmetal hexagonal lock nut (409), and No. two nonmetal hexagonal lock nut (409) and No. two cross recess flat round head screw (404) rotate to be connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021207251.4U CN212501085U (en) | 2020-06-28 | 2020-06-28 | Load quick replacement device for vertical take-off and landing fixed wing unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021207251.4U CN212501085U (en) | 2020-06-28 | 2020-06-28 | Load quick replacement device for vertical take-off and landing fixed wing unmanned aerial vehicle |
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| CN212501085U true CN212501085U (en) | 2021-02-09 |
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| CN202021207251.4U Active CN212501085U (en) | 2020-06-28 | 2020-06-28 | Load quick replacement device for vertical take-off and landing fixed wing unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023034095A1 (en) * | 2021-08-31 | 2023-03-09 | Textron Systems Corporation | Utilizing a customizable fuselage assembly for an unmanned aerial vehicle |
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2020
- 2020-06-28 CN CN202021207251.4U patent/CN212501085U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023034095A1 (en) * | 2021-08-31 | 2023-03-09 | Textron Systems Corporation | Utilizing a customizable fuselage assembly for an unmanned aerial vehicle |
| US11753137B2 (en) | 2021-08-31 | 2023-09-12 | Textron Systems Corporation | Utilizing a customizable fuselage assembly for an unmanned aerial vehicle |
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