CN205440853U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205440853U CN205440853U CN201521106108.5U CN201521106108U CN205440853U CN 205440853 U CN205440853 U CN 205440853U CN 201521106108 U CN201521106108 U CN 201521106108U CN 205440853 U CN205440853 U CN 205440853U
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- fixture
- undercarriage
- buckle
- fuselage
- unmanned plane
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- 239000012634 fragment Substances 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 12
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000035800 maturation Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Ladders (AREA)
- Toys (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle, including fuselage, undercarriage and connecting piece, the connecting piece includes two mountings at least, and one of them mounting is connected with the fuselage, and the another one mounting is connected with the undercarriage, one of them mounting be equipped with with the fixed chamber of another one mounting periphery shape matching and the draw -in groove that communicates with fixed chamber, the another one mounting be equipped with with draw -in groove complex buckle. The mounting that will be equipped with the buckle stretches into the fixed intracavity of another mounting to be connected through buckle and draw -in groove cooperation, realize that the fuselage is fixed with the installation of undercarriage, during the dismantlement, break away from the draw -in groove with the buckle to the fixed chamber of another mounting is taken out to the mounting that will be equipped with the buckle, can realize the dismantlement of fuselage and undercarriage. Through having set up the connecting piece between fuselage and undercarriage, make and realize between fuselage and the undercarriage dismantling the connection, realize the quick installation and the dismantlement of undercarriage, labour saving and time saving reduces unmanned aerial vehicle's occupation space, makes things convenient for carrying of unmanned aerial vehicle.
Description
Technical field
This utility model relates to a kind of vehicle technology field, particularly to a kind of unmanned plane.
Background technology
Unmanned plane has the advantages such as flight attitude is easily controlled, maturation now with technology, the range of application of unmanned plane constantly expands, particularly take photo by plane at some, the field such as detection, unmanned plane has higher popularity rate, the many rotor wing unmanned aerial vehicles generally seen are according to different application scenarios or the different terrain in different landing site, it is sometimes desirable to coordinate and select different undercarriages.But current many rotor wing unmanned aerial vehicles, because undercarriage generally uses screw fixation method that undercarriage is fixed on the bottom of unmanned aerial vehicle body, such fixed form causes the undercarriage can not disassembly and assembly easily, waste time and energy, disassembly process is complicated, and unmanned plane takes up room greatly, not readily portable.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, it is possible to realizes being rapidly assembled and disassembled of undercarriage, and facilitates carrying of unmanned plane.
For realizing the purpose of this utility model, adopt the technical scheme that:
A kind of unmanned plane, including fuselage, undercarriage and connector, connector at least includes two fixtures, one of them fixture is connected with fuselage, another one fixture is connected with undercarriage, one of them fixture is provided with the lock chamber with another one fixture peripheral shape coupling and the draw-in groove connected with lock chamber, and another one fixture is provided with and the buckle of card slot fit.
During installation, it is provided with in the lock chamber that the fixture of buckle stretches into another fixture, and is connected with draw-in groove by buckle, it is achieved the installation of fuselage and undercarriage is fixed；During dismounting, buckle is departed from draw-in groove, and the fixture being provided with buckle is extracted out the lock chamber of another fixture, the dismounting of fuselage and undercarriage can be realized.By being provided with connector between fuselage and undercarriage, make to realize between fuselage and undercarriage removably connecting, it is achieved being rapidly assembled and disassembled of undercarriage, time saving and energy saving, and after fuselage and undercarriage are dismantled, reduce taking up room of unmanned plane, facilitate carrying of unmanned plane.
Below technical scheme is further illustrated:
Further, the fixture being provided with lock chamber is connected with fuselage, and the fixture being provided with buckle is connected with undercarriage.
Further, the fixture being provided with buckle is connected with fuselage, and the fixture being provided with lock chamber is connected with undercarriage.
Further, buckle at least includes the jut with card slot fit, drives jut stretch into or depart from the press section of draw-in groove, and lock chamber is stretched out in press section.The press section of buckle is arranged on the outside of lock chamber, and the installation and removal making undercarriage are more convenient.
It is further, buckle is fixed on the outer wall of the second fixture, the fixture being provided with lock chamber is the first fixture, the fixture being provided with buckle is the second fixture, jut is provided with inclined-plane, and inclined-plane is gradually distance from the outer wall of the second fixture by the one end near the first fixture to the one end away from the first fixture.When second fixture inserts the lock chamber of the first fixture, inclined-plane is first adjacent to the inwall of lock chamber near one end of the second fixture outer wall, plays pretension effect, until the whole inclined-plane of jut buckles in draw-in groove, makes to fix more firm between fuselage and undercarriage.
Further, buckle is spring shell fragment.Utilizing the elastic force of spring shell fragment, make two fixtures be fixed together, the installation and removal also allowing for undercarriage are more laborsaving.
Further, the inwall of lock chamber is arranged with vertically arranged groove, and the fixture being provided with buckle is provided with the boss with groove fit.By groove and the cooperation of boss, the installation to the first fixture and the second fixture plays guiding and positioning action, makes to mount and dismount more quickly between fuselage and undercarriage.
Further, unmanned plane also includes the drive mechanism driving undercarriage to elongate or shorten.Making unmanned plane according to different flight state, adjust the pitching of undercarriage, the use making unmanned plane is more convenient.
Compared with prior art, this utility model has the advantages that
This utility model is by stretching into the fixture being provided with buckle in the lock chamber of another fixture, and is connected with draw-in groove by buckle, it is achieved the installation of fuselage and undercarriage is fixed；During dismounting, then buckle is departed from draw-in groove, and the fixture being provided with buckle is extracted out the lock chamber of another fixture, the dismounting of fuselage and undercarriage can be realized.By being provided with connector between fuselage and undercarriage, make to realize between fuselage and undercarriage removably connecting, it is achieved being rapidly assembled and disassembled of undercarriage, time saving and energy saving, and after fuselage and undercarriage are dismantled, reduce taking up room of unmanned plane, facilitate carrying of unmanned plane.
Accompanying drawing explanation
Fig. 1 is the structural representation of this utility model embodiment unmanned plane.
Description of reference numerals:
10. undercarriage, 20. connectors, 210. first fixtures, 211. lock chambers, 212. draw-in grooves, 220. second fixtures, 221. boss, 30. buckles, 310. juts, 311. inclined-planes, 320. press sections, 40. drive mechanisms.
Detailed description of the invention
Below in conjunction with the accompanying drawings embodiment of the present utility model is described in detail:
As shown in Figure 1, a kind of unmanned plane, including fuselage (accompanying drawing does not identifies), undercarriage 10 and connector 20, connector 20 at least includes the first fixture 210 and the second fixture 220, first fixture 210 is connected with fuselage, second fixture 220 is connected with undercarriage 10, and the first fixture 210 is provided with the lock chamber 211 with the second fixture 220 peripheral shape coupling and the draw-in groove 212 connected with lock chamber 211, and the second fixture 220 is provided with the buckle 30 coordinated with draw-in groove 212.
During installation, the second fixture 220 stretches in the lock chamber 211 of the first fixture 210, and is connected with draw-in groove 212 by buckle 30, it is achieved the installation of fuselage and undercarriage 10 is fixed；During dismounting, buckle 30 is departed from draw-in groove 212, and the second fixture 220 is extracted out the lock chamber 211 of the first fixture 210, the dismounting of fuselage and undercarriage 10 can be realized.By being provided with connector 20 between fuselage and undercarriage 10, make to realize between fuselage and undercarriage 10 removably connecting, it is achieved being rapidly assembled and disassembled of undercarriage 10, time saving and energy saving, and after fuselage and undercarriage 10 are dismantled, reduce taking up room of unmanned plane, facilitate carrying of unmanned plane.
In the present embodiment, the first fixture 210 is connected with fuselage, and the second fixture 220 is connected with undercarriage 10.First fixture 210 can also be connected by unmanned plane according to actual needs with undercarriage 10, is connected with fuselage by the second fixture 220.
As it is shown in figure 1, buckle 30 is fixed on the outer wall of the second fixture 220, buckle 30 at least includes the jut 310 coordinated with draw-in groove 212, drives jut 310 stretch into or depart from the press section 320 of draw-in groove 212, and lock chamber 211 is stretched out in press section 320.The press section 320 of buckle 30 is arranged on the outside of lock chamber 211, and the installation and removal making undercarriage 10 are more convenient.
Jut 310 is provided with inclined-plane 311, and inclined-plane 311 is gradually distance from the outer wall of the second fixture 220 by the one end near the first fixture 210 to the one end away from the first fixture 210.When second fixture 220 inserts the lock chamber 211 of the first fixture 210, inclined-plane 311 is first adjacent to the inwall of lock chamber 211 near one end of the second fixture 220 outer wall, play pretension effect, until the inclined-plane 311 of jut 310 buckles in draw-in groove 212, make to fix more firm between fuselage and undercarriage 10.
In the present embodiment, buckle 30 is spring shell fragment, elastic reaction due to spring shell fragment, when second fixture 220 inserts the lock chamber 211 of the first fixture 210, jut 310 can be compressed, until jut 310 moves to time the most relative with draw-in groove 212, under the effect of elastic force, make jut 310 buckle in draw-in groove 212, eliminate the gap during assembling.And the abutting part 330 that spring shell fragment is provided with between jut 310 and press section 320, during dismounting, down during pressure press section 320, make jut 310 back contract and depart from draw-in groove 212, afterwards the second fixture 220 is detached in the first fixture 210, convenient disassembly.
The inwall of lock chamber 211 is arranged with vertically arranged groove (accompanying drawing does not identifies), and the second fixture 220 outer wall is provided with the boss 221 with groove fit.By groove and the cooperation of boss 221, the installation to the first fixture 210 and the second fixture 220 plays guiding and positioning action, makes to mount and dismount more quickly between fuselage and undercarriage 10.
As it is shown in figure 1, unmanned plane also includes the drive mechanism 40 driving undercarriage 10 pitch attitude.Making unmanned plane according to different flight state, adjust undercarriage luffing angle, the use making unmanned plane is more convenient.
Each technical characteristic of embodiment described above can combine arbitrarily, for making description succinct, the all possible combination of each technical characteristic in above-described embodiment is not all described, but, as long as the combination of these technical characteristics does not exist contradiction, all it is considered to be the scope that this specification is recorded.
Embodiment described above only have expressed several embodiments of the present utility model, and it describes more concrete and detailed, but therefore can not be interpreted as the restriction to utility model patent scope.It should be pointed out that, for the person of ordinary skill of the art, without departing from the concept of the premise utility, it is also possible to make some deformation and improvement, these broadly fall into protection domain of the present utility model.Therefore, the protection domain of this utility model patent should be as the criterion with claims.
Claims (8)
1. a unmanned plane, it is characterized in that, including fuselage, undercarriage and connector, described connector at least includes two fixtures, one of them described fixture is connected with described fuselage, fixture described in another one is connected with described undercarriage, and one of them described fixture is provided with the lock chamber with fixture peripheral shape coupling described in another one and the draw-in groove connected with described lock chamber, and fixture described in another one is provided with and the buckle of described card slot fit.
Unmanned plane the most according to claim 1, it is characterised in that the described fixture being provided with described lock chamber is connected with described fuselage, the described fixture being provided with described buckle is connected with described undercarriage.
Unmanned plane the most according to claim 1, it is characterised in that the described fixture being provided with described buckle is connected with described fuselage, the described fixture being provided with described lock chamber is connected with described undercarriage.
Unmanned plane the most according to claim 1, it is characterised in that described buckle at least includes the jut with described card slot fit, drives described jut to stretch into or depart from the press section of described draw-in groove, and described lock chamber is stretched out in described press section.
Unmanned plane the most according to claim 4, it is characterized in that, described buckle is fixed on the outer wall of described fixture, the described fixture being provided with described lock chamber is the first fixture, the described fixture being provided with described buckle is the second fixture, described jut is provided with inclined-plane, and described inclined-plane is gradually distance from the outer wall of described second fixture by the one end near described first fixture to the one end away from described first fixture.
6. according to the unmanned plane described in any one of claim 1 to 5, it is characterised in that described buckle is spring shell fragment.
7., according to the unmanned plane described in any one of claim 1 to 5, it is characterised in that the inwall of described lock chamber is arranged with vertically arranged groove, the described fixture being provided with described buckle is provided with and the boss of described groove fit.
8. according to the unmanned plane described in any one of claim 1 to 5, it is characterised in that also include driving described undercarriage pitching to change.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521106108.5U CN205440853U (en) | 2015-12-24 | 2015-12-24 | Unmanned aerial vehicle |
| PCT/CN2016/108363 WO2017107753A1 (en) | 2015-12-24 | 2016-12-02 | Drone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521106108.5U CN205440853U (en) | 2015-12-24 | 2015-12-24 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205440853U true CN205440853U (en) | 2016-08-10 |
Family
ID=56579135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521106108.5U Active CN205440853U (en) | 2015-12-24 | 2015-12-24 | Unmanned aerial vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN205440853U (en) |
| WO (1) | WO2017107753A1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628125A (en) * | 2016-12-28 | 2017-05-10 | 中国航天电子技术研究院 | Quick-disassembling energy absorption undercarriage for multi-rotor unmanned aerial vehicle |
| WO2017107753A1 (en) * | 2015-12-24 | 2017-06-29 | 广州亿航智能技术有限公司 | Drone |
| WO2018133192A1 (en) * | 2017-01-18 | 2018-07-26 | 深圳市大疆创新科技有限公司 | Stand assembly and unmanned aerial vehicle |
| CN110228591A (en) * | 2019-06-05 | 2019-09-13 | 南京工业职业技术学院 | A kind of bracket telescopic transport unmanned plane |
| CN112960110A (en) * | 2021-04-09 | 2021-06-15 | 广州亿航智能技术有限公司 | Quick assembly disassembly connects and has undercarriage that this connects |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| MA41565B1 (en) | 2017-12-05 | 2019-11-29 | Univ Int Rabat | Detachable Landing Gear Drone |
| MA41573B1 (en) | 2017-12-06 | 2019-12-31 | Univ Int Rabat | Mechanical attachment for detachable landing gear |
| US11655023B2 (en) * | 2018-01-30 | 2023-05-23 | Ideaforge Technology Pvt. Ltd. | Fixed-wing vertical take-off and landing hybrid UAV |
| CN208325633U (en) * | 2018-06-26 | 2019-01-04 | 深圳市大疆创新科技有限公司 | Unmanned vehicle and its rack |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2795042B1 (en) * | 1999-06-15 | 2001-10-12 | Aerospatiale Airbus | AIRCRAFT HAVING A CONTROLLED DETACHMENT LANDING IN THE EVENT OF AN ACCIDENT |
| CN203461089U (en) * | 2013-09-22 | 2014-03-05 | 重庆金泰航空工业有限公司 | Pesticide box and combined type fuselage assembly of farm-oriented unmanned aerial vehicle |
| CN104210652B (en) * | 2014-08-26 | 2017-06-23 | 中国直升机设计研究所 | A kind of attachment structure of undercarriage |
| CN204223174U (en) * | 2014-10-27 | 2015-03-25 | 广州极飞电子科技有限公司 | Rotor craft foot rest fast assembling disassembling structure |
| CN104691746B (en) * | 2014-12-08 | 2016-08-17 | 中国航天空气动力技术研究院 | A kind of big span lightweight unmanned plane single-wheel telescopic landing gear structure |
| CN104443364B (en) * | 2014-12-22 | 2016-06-15 | 深圳市高巨创新科技开发有限公司 | Detachable undercarriage and four-axle aircraft |
| CN204548484U (en) * | 2015-01-09 | 2015-08-12 | 优利科技有限公司 | Alighting gear for aircraft and the aircraft containing it |
| CN204587303U (en) * | 2015-01-27 | 2015-08-26 | 优利科技有限公司 | Anchor fitting and containing its aircraft |
| CN204674821U (en) * | 2015-04-08 | 2015-09-30 | 优利科技有限公司 | Alighting gear, fuselage and aircraft |
| CN205440853U (en) * | 2015-12-24 | 2016-08-10 | 广州亿航智能技术有限公司 | Unmanned aerial vehicle |
-
2015
- 2015-12-24 CN CN201521106108.5U patent/CN205440853U/en active Active
-
2016
- 2016-12-02 WO PCT/CN2016/108363 patent/WO2017107753A1/en active Application Filing
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017107753A1 (en) * | 2015-12-24 | 2017-06-29 | 广州亿航智能技术有限公司 | Drone |
| CN106628125A (en) * | 2016-12-28 | 2017-05-10 | 中国航天电子技术研究院 | Quick-disassembling energy absorption undercarriage for multi-rotor unmanned aerial vehicle |
| WO2018133192A1 (en) * | 2017-01-18 | 2018-07-26 | 深圳市大疆创新科技有限公司 | Stand assembly and unmanned aerial vehicle |
| CN109641651A (en) * | 2017-01-18 | 2019-04-16 | 深圳市大疆创新科技有限公司 | Foot prop component and unmanned vehicle |
| CN109641651B (en) * | 2017-01-18 | 2022-06-10 | 深圳市大疆创新科技有限公司 | Foot rest component and unmanned aerial vehicle |
| CN110228591A (en) * | 2019-06-05 | 2019-09-13 | 南京工业职业技术学院 | A kind of bracket telescopic transport unmanned plane |
| CN112960110A (en) * | 2021-04-09 | 2021-06-15 | 广州亿航智能技术有限公司 | Quick assembly disassembly connects and has undercarriage that this connects |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2017107753A1 (en) | 2017-06-29 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |