CN108928463B - Unmanned aerial vehicle containing box and undercarriage integrated device - Google Patents
Unmanned aerial vehicle containing box and undercarriage integrated device Download PDFInfo
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- CN108928463B CN108928463B CN201810689629.XA CN201810689629A CN108928463B CN 108928463 B CN108928463 B CN 108928463B CN 201810689629 A CN201810689629 A CN 201810689629A CN 108928463 B CN108928463 B CN 108928463B
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- cover plate
- undercarriage
- aerial vehicle
- unmanned aerial
- box body
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
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Abstract
The invention discloses an integrated device of an unmanned aerial vehicle storage box and an undercarriage, which is divided into the storage box and the undercarriage; the landing gear support comprises a box body, a cover plate A, a cover plate B, a cover plate C, a buckle, a bearing space, a handle, a cross brace, a stripe sculpture and a landing gear support leg; set up unmanned aerial vehicle's containing box and unmanned aerial vehicle's undercarriage as an organic whole, practiced thrift the space, also made things convenient for and carried, also prevented to only carry unmanned aerial vehicle and forgotten to carry the undercarriage and cause the unable circumstances of taking off.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle accessories, in particular to an integrated device of an unmanned aerial vehicle containing box and an undercarriage.
Background
Along with the rapid development of unmanned aerial vehicle technique, unmanned aerial vehicle is more and more common in daily life, but unmanned aerial vehicle's carrying is also very troublesome, has blade, battery, remote controller, fuselage etc. and the box of former dress is big again heavy now, and is inconvenient to put into in the box moreover.
Rotor VTOL unmanned aerial vehicle, it is big to take off weight, and the performance requirement to the bearing of undercarriage and keeping the aircraft stable during the landing is higher. Particularly, under the condition of severe taking-off and landing environments (such as ship taking-off and landing), the possibility of rollover of the unmanned aerial vehicle is greatly increased, and the landing gear of the unmanned aerial vehicle with a simple structure is urgently needed to ensure the taking-off and landing stability (mainly referring to the stability of the aircraft after lateral interference in the phase of contact between the landing gear and the ground or a deck and the like) and the safety of the unmanned aerial vehicle.
Required containing box and undercarriage are all bigger when using unmanned aerial vehicle to take off, carry very inconveniently.
Disclosure of Invention
The invention aims to solve the problems that in the prior art, a containing box and an undercarriage are independent devices, the undercarriage is arranged in the containing box, and the containing box and the undercarriage are combined into a whole, so that the integrated device of the containing box and the undercarriage of the unmanned aerial vehicle is provided.
In order to achieve the purpose, the invention adopts the following technical scheme:
an integrated device of an unmanned aerial vehicle storage box and an undercarriage is divided into a storage box and the undercarriage; the landing gear support comprises a box body, a cover plate A, a cover plate B, a cover plate C, a buckle, a bearing space, a handle, a cross brace, a stripe sculpture and a landing gear support leg; the unmanned aerial vehicle box comprises a box body, a handle, a cover plate A, a rotating hinge, a buckle and a bearing space, wherein the box body is cuboid, the handle is positioned in the center of the right side of the box body, the cover plate A with two different types of sizes is arranged on the upper side of the box body, the cover plate A is positioned in the middle of the upper side of the box body, the rotating hinge for connecting with the box body is arranged on the left side of the cover plate A, the box body at the corresponding position on the right side of the cover plate A is provided with the buckle for clamping, and the bearing space for bearing the unmanned aerial vehicle is arranged below the cover plate A;
the cover plate B and the cover plate C are identical in size, the cover plate B and the cover plate C are arranged on the front side and the rear side of the cover plate A, buckles for clamping are arranged on the box body at the positions, corresponding to the right sides of the cover plate B and the cover plate C, of the cover plate B, and landing gears matched with the cover plate B and the cover plate C are arranged in the space below the cover plate B and the cover plate C;
the undercarriage component under the cover plate B is rectangular and consists of two undercarriage supporting legs which are erected on the basis of the bottom surface of the box body and a cross brace which is connected with the top ends of the two undercarriage supporting legs, and the undercarriage component under the cover plate C is consistent with the undercarriage component under the cover plate B.
Preferably, the landing gear supporting legs are telescopic rods.
Preferably, install the bubble spirit level on the stull side, and have the line of being convenient for unmanned aerial vehicle to rise and fall above the stull and carve.
Compared with the prior art, the invention provides an integrated device of an unmanned aerial vehicle containing box and an undercarriage, which has the following beneficial effects: the storage box of the unmanned aerial vehicle facilitates the protection of the unmanned aerial vehicle in the carrying and transportation processes, and the undercarriage of the unmanned aerial vehicle facilitates the take-off and landing of the unmanned aerial vehicle; set up unmanned aerial vehicle's containing box and unmanned aerial vehicle's undercarriage as an organic whole, practiced thrift the space, also made things convenient for and carried, also prevented to only carry unmanned aerial vehicle and forgotten to carry the undercarriage and cause the unable circumstances of taking off.
The parts which are not involved in the device are the same as or can be realized by adopting the prior art, and the device has the advantages of simple structure and convenient operation.
Drawings
Fig. 1 is a schematic perspective view of a cover plate of an integrated device of an unmanned aerial vehicle containing box and an undercarriage provided by the invention when the cover plate is closed;
fig. 2 is a schematic perspective view of an unmanned aerial vehicle storage box and undercarriage integrated device provided by the invention when a cover plate is opened;
fig. 3 is a schematic structural diagram of an undercarriage of an integrated device of an unmanned aerial vehicle storage box and an undercarriage.
The reference numbers in the figures illustrate: 1 is the box, 2 is apron B, 3 is apron A, 4 is the buckle, 5 is the handle, 6 is apron C, 7 is undercarriage landing leg, 8 is the line and carves, 9 is the stull, 10 is the bearing space, 11 is the bubble spirit level.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
The embodiment is as follows: an integrated device of an unmanned aerial vehicle storage box and an undercarriage is divided into the storage box and the undercarriage; the landing gear support comprises a box body 1, a cover plate A3, a cover plate B2, a cover plate C6, a buckle 4, a bearing space 10, a handle 5, a cross brace 9, a stripe 8 and landing gear support legs 7; the unmanned aerial vehicle storage box is characterized in that the box body 1 is cuboid, the handle 5 is located in the center of the right side face of the box body 1, cover plates with two different types of sizes are mounted on the upper side face of the box body 1, the cover plate A3 is located in the middle of the upper side face of the box body 1, a rotary hinge used for being connected with the box body 1 is mounted on the left side of the cover plate A3, a buckle 4 used for clamping is mounted on the box body 1 at the corresponding position on the right side of the cover plate A3, and a holding space 10 used for holding an unmanned aerial vehicle is arranged below the cover plate A3;
the cover plate B2 and the cover plate C6 are the same in size, the cover plate B2 and the cover plate C6 are arranged and distributed on the front side and the rear side of the cover plate A3, buckles 4 for clamping are arranged on the box body 1 at the corresponding positions on the right sides of the cover plate B2 and the cover plate C6, and landing gears matched with the cover plate B2 and the cover plate C6 are arranged in the lower space of the cover plate B2 and the cover plate C6;
the undercarriage component under the cover plate B2 is rectangular, and consists of two undercarriage legs 7 erected on the basis of the bottom surface of the box body 1 and a cross brace 9 connected with the top ends of the two undercarriage legs 7, the undercarriage legs 7 are telescopic rods, a bubble level gauge 11 is installed on the side surface of the cross brace 9, patterns convenient for the unmanned aerial vehicle to rise and fall are carved on the cross brace 9, and the undercarriage component under the cover plate C6 is consistent with the undercarriage component under the cover plate B2.
In conclusion, when using the containing box, cover all apron, utilize buckle 4 with all apron chucking, play the effect of sealed protection, and buckle 4 is simple to use and firm, when using the undercarriage, only need open apron A3 and take out unmanned aerial vehicle after, open apron B2 and apron C6 again, utilize landing gear landing leg 7's telescopic link, after pulling up two undercarriage the same take the altitude, rethread bubble spirit level 11 adjusts to the level after, the used undercarriage of unmanned aerial vehicle has been made, the line 8 of carving above the stull 9 plays the effect of increaseing friction, can prevent unmanned aerial vehicle's landing to a certain extent.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered as the technical solutions and the inventive concepts of the present invention within the technical scope of the present invention.
Claims (1)
1. The utility model provides an unmanned aerial vehicle containing box and undercarriage integrated device which characterized in that: is divided into a containing box and an undercarriage; the landing gear box comprises a box body, a cover plate A, a cover plate B, a cover plate C, a buckle, a bearing space, a handle, a cross brace and landing gear support legs; the unmanned aerial vehicle box comprises a box body, a handle, a cover plate A, a rotating hinge, a buckle and a bearing space, wherein the box body is cuboid, the handle is positioned in the center of the right side of the box body, the cover plate A with two different types of sizes is arranged on the upper side of the box body, the cover plate A is positioned in the middle of the upper side of the box body, the rotating hinge for connecting with the box body is arranged on the left side of the cover plate A, the box body at the corresponding position on the right side of the cover plate A is provided with the buckle for clamping, and the bearing space for bearing the unmanned aerial vehicle is arranged below the cover plate A; the cover plate B and the cover plate C are identical in size, the cover plate B and the cover plate C are arranged on the front side and the rear side of the cover plate A, buckles for clamping are arranged on the box body at the positions, corresponding to the right sides of the cover plate B and the cover plate C, of the cover plate B, and landing gears matched with the cover plate B and the cover plate C are arranged in the space below the cover plate B and the cover plate C; the undercarriage component under the cover plate B is rectangular and consists of two undercarriage supporting legs which are erected on the basis of the bottom surface of the box body and a cross brace which is connected with the top ends of the two undercarriage supporting legs, and the undercarriage component under the cover plate C is consistent with the undercarriage component under the cover plate B; the landing gear supporting legs are telescopic rods; the lateral surface of the cross brace is provided with a bubble level gauge, and the upper surface of the cross brace is provided with a groove which is convenient for the unmanned aerial vehicle to rise and fall;
when using the containing box, cover all apron, utilize the buckle with all apron chuckings, play the effect of sealed protection, and the buckle is simple to use and firm, when using the undercarriage, only need open apron A and take out unmanned aerial vehicle after, open apron B and apron C again, utilize undercarriage landing leg's telescopic link, pull up two undercarriage the same take the altitude after, rethread bubble spirit level adjusts to the level after, the used undercarriage of unmanned aerial vehicle has just become, the line above the stull is carved, play the effect that increases friction, can prevent unmanned aerial vehicle's landing to a certain extent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810689629.XA CN108928463B (en) | 2018-06-28 | 2018-06-28 | Unmanned aerial vehicle containing box and undercarriage integrated device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810689629.XA CN108928463B (en) | 2018-06-28 | 2018-06-28 | Unmanned aerial vehicle containing box and undercarriage integrated device |
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| Publication Number | Publication Date |
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| CN108928463A CN108928463A (en) | 2018-12-04 |
| CN108928463B true CN108928463B (en) | 2022-09-20 |
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| CN201810689629.XA Active CN108928463B (en) | 2018-06-28 | 2018-06-28 | Unmanned aerial vehicle containing box and undercarriage integrated device |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103303471A (en) * | 2012-03-12 | 2013-09-18 | 霍尼韦尔国际公司 | Movable bushing interface and taxi drive system |
| CN106005468A (en) * | 2016-07-22 | 2016-10-12 | 珠海银通农业科技有限公司 | Integrated all-in-one unmanned aerial vehicle with trolley |
| CN106742013A (en) * | 2016-12-27 | 2017-05-31 | 纪泽源 | A kind of modularized multi-axis unmanned plane rises and falls base station |
| CN206939058U (en) * | 2017-05-12 | 2018-01-30 | 西华酷农无人机产业园运营有限公司 | A kind of undercarriage of unmanned plane |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0616985D0 (en) * | 2006-08-29 | 2006-10-04 | Borealis Tech Ltd | Transistor |
| EP3263451A1 (en) * | 2016-06-28 | 2018-01-03 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An aircraft with a fuselage and a non-retractable skid-type landing gear |
-
2018
- 2018-06-28 CN CN201810689629.XA patent/CN108928463B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103303471A (en) * | 2012-03-12 | 2013-09-18 | 霍尼韦尔国际公司 | Movable bushing interface and taxi drive system |
| CN106005468A (en) * | 2016-07-22 | 2016-10-12 | 珠海银通农业科技有限公司 | Integrated all-in-one unmanned aerial vehicle with trolley |
| CN106742013A (en) * | 2016-12-27 | 2017-05-31 | 纪泽源 | A kind of modularized multi-axis unmanned plane rises and falls base station |
| CN206939058U (en) * | 2017-05-12 | 2018-01-30 | 西华酷农无人机产业园运营有限公司 | A kind of undercarriage of unmanned plane |
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| Publication number | Publication date |
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| CN108928463A (en) | 2018-12-04 |
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Effective date of registration: 20220824 Address after: 362302 6th floor, innovation building, Fujian Branch, National University Science Park, Xiamei Town, Nan'an City, Quanzhou City, Fujian Province Applicant after: Gaojie technology holding (Fujian) Co.,Ltd. Address before: 256603 No. 517, Bohai 8th Road, West office, Bincheng District, Binzhou City, Shandong Province Applicant before: SHANDONG HAOKUN SAFETY TECHNOLOGY CONSULTATION Co.,Ltd. |
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Application publication date: 20181204 Assignee: Fujian Maotian Technology Co.,Ltd. Assignor: Gaojie technology holding (Fujian) Co.,Ltd. Contract record no.: X2023980033627 Denomination of invention: An integrated device for UAV storage box and landing gear Granted publication date: 20220920 License type: Common License Record date: 20230320 |
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