CN105667769A - Undercarriage for unmanned aerial vehicle - Google Patents
Undercarriage for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105667769A CN105667769A CN201610107651.XA CN201610107651A CN105667769A CN 105667769 A CN105667769 A CN 105667769A CN 201610107651 A CN201610107651 A CN 201610107651A CN 105667769 A CN105667769 A CN 105667769A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- support bar
- protruding block
- undercarriage
- aerial 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/06—Undercarriages fixed
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Handcart (AREA)
Abstract
The invention discloses an undercarriage for an unmanned aerial vehicle. The undercarriage comprises a supporting rod and a base. The supporting rod is arranged on the base. The upper end of the supporting rod is provided with a connecting block. A plurality of clamping grooves are formed in the connecting block. The clamping grooves are clamped onto the unmanned aerial vehicle in a matched mode. The supporting rod is also provided with an elastic key which is provided with a protruding block. The protruding block is connected with the unmanned aerial vehicle in a clamped mode to fix the supporting rod. The protruding block is separated from the unmanned aerial vehicle by pressing the elastic key, so that the supporting rod is loosened. In this way, by adopting the undercarriage for the unmanned aerial vehicle, the space and weight of the unmanned aerial vehicle can be reduced. The undercarriage is simple in structure, safe and reliable.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of unmanned plane undercarriage.
Background technology
In recent years, unmanned air vehicle technique had had the development advanced by leaps and bounds. Current unmanned plane mainly includes fixed-wing unmanned plane and rotor wing unmanned aerial vehicle. Compared with fixed-wing unmanned plane, rotor wing unmanned aerial vehicle has simple in construction, controls flexibly, VTOL, can hover or the advantage such as inverted flight, has a wide range of applications in Aerial photography, police service application etc. , at present, the structure of unmanned plane itself is generally stationary structure, and agent structure is fixed, and the lift that wing produces is not enough so that the load-carrying ability of unmanned plane is limited, and its shock-absorbing capacity is poor simultaneously, it is impossible to meet demand.
Summary of the invention
The technical problem that present invention mainly solves is to provide a kind of unmanned plane undercarriage, it is possible to saving unmanned plane space, reduction unmanned plane weight, and simple in construction is safe and reliable.
For solving above-mentioned technical problem, the technical scheme that the present invention adopts is: provide a kind of unmanned plane undercarriage, including: support bar and base, described support bar is arranged on base, described post upper is provided with contiguous block, described contiguous block is provided with multiple draw-in groove, described card slot fit is connected on unmanned plane, described support bar is additionally provided with flexible keypad, described flexible keypad is provided with protruding block, described protruding block connects and fixes support bar mutually with unmanned plane, described protruding block makes it depart from from unmanned plane by pressing flexible keypad, thus unclamping support bar.
In a preferred embodiment of the present invention, described unmanned plane being provided with shackle member, described shackle member contacts with protruding block with fixing support bar.
In a preferred embodiment of the present invention, the cross section of described protruding block is trapezoidal, and described flexible keypad is provided with pressing striped.
In a preferred embodiment of the present invention, described support bar, base and contiguous block are formed in one.
In a preferred embodiment of the present invention, described unmanned plane being provided with mounting cup, described contiguous block is connected inside mounting cup.
The invention has the beneficial effects as follows: unmanned plane undercarriage of the present invention, it is possible to saving unmanned plane space, reduction unmanned plane weight, simple in construction, safe and reliable.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in the embodiment of the present invention, below the accompanying drawing used required during embodiment is described is briefly described, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings, wherein:
Fig. 1 is the structural representation of unmanned plane undercarriage one of the present invention preferred embodiment;
Fig. 2 is the structural representation of shown unmanned plane;
Fig. 3 is the partial structurtes enlarged diagram of unmanned plane shown in Fig. 2;
In accompanying drawing, the labelling of each parts is as follows: 1, support bar, and 2, base, 3, contiguous block, 4, draw-in groove, 5, flexible keypad, 6, protruding block, 7, unmanned plane, 8, shackle member, 9, mounting cup, 10, pressing striped.
Detailed description of the invention
Technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described embodiment is only a part of embodiment of the present invention, rather than whole embodiments. Based on the embodiment in the present invention, all other embodiments that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
Refer to Fig. 1 to Fig. 3, a kind of unmanned plane undercarriage, including: support bar 1 and base 2, described support bar 1 is arranged on base 2, described support bar 1 upper end is provided with contiguous block 3, described contiguous block 3 is provided with multiple draw-in groove 4, the cooperation of described draw-in groove 4 is connected on unmanned plane 7, described support bar 1 is additionally provided with flexible keypad 5, described flexible keypad 5 is provided with protruding block 6, described protruding block 6 and unmanned plane 7 phase connect and fix support bar, and described protruding block 6 makes it depart from from unmanned plane by pressing flexible keypad 5, thus unclamping support bar 1.
It addition, be provided with shackle member 8 on described unmanned plane 7, described shackle member 8 contacts with protruding block 6 with fixing support bar 1.
It addition, the cross section of described protruding block 6 is trapezoidal, described flexible keypad 5 is provided with pressing striped 10.
It addition, described support bar 1, base 2 and contiguous block 3 are formed in one.
It addition, be provided with mounting cup 9 on described unmanned plane 7, described contiguous block 3 is connected inside mounting cup 9.
Unmanned plane undercarriage specific works principle of the present invention is as follows: by corresponding for the draw-in groove 4 of the contiguous block 3 on support bar 1 mounting cup 9 inserting unmanned plane 7, protruding block 6 on elastic fastener 5 is just connected in the shackle member 8 of unmanned plane 7 simultaneously, it is prevented that support bar 1 drops. When undercarriage packed up by needs, pressing elastic fastener 5, the protruding block 6 on elastic fastener 5 made is 8 disengaging shackle member, then pulls support bar 1, makes the contiguous block 3 of support bar 1 depart from mounting cup 9, completes the dismounting of undercarriage.
It is different from prior art, unmanned plane undercarriage of the present invention, it is possible to saving unmanned plane space, reduction unmanned plane weight, simple in construction, safe and reliable.
The foregoing is only embodiments of the invention; not thereby the scope of the claims of the present invention is limited; every equivalent structure utilizing description of the present invention to make or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical field, all in like manner include in the scope of patent protection of the present invention.
Claims (5)
1. a unmanned plane undercarriage, it is characterized in that, including: support bar and base, described support bar is arranged on base, described post upper is provided with contiguous block, described contiguous block is provided with multiple draw-in groove, described card slot fit is connected on unmanned plane, described support bar is additionally provided with flexible keypad, described flexible keypad is provided with protruding block, described protruding block connects and fixes support bar mutually with unmanned plane, and described protruding block makes it depart from from unmanned plane by pressing flexible keypad, thus unclamping support bar.
2. unmanned plane undercarriage according to claim 1, it is characterised in that being provided with shackle member on described unmanned plane, described shackle member contacts with protruding block with fixing support bar.
3. unmanned plane undercarriage according to claim 1, it is characterised in that the cross section of described protruding block is trapezoidal, and described flexible keypad is provided with pressing striped.
4. unmanned plane undercarriage according to claim 1, it is characterised in that described support bar, base and contiguous block are formed in one.
5. unmanned plane undercarriage according to claim 1, it is characterised in that being provided with mounting cup on described unmanned plane, described contiguous block is connected inside mounting cup.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610107651.XA CN105667769A (en) | 2016-02-29 | 2016-02-29 | Undercarriage for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610107651.XA CN105667769A (en) | 2016-02-29 | 2016-02-29 | Undercarriage for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105667769A true CN105667769A (en) | 2016-06-15 |
Family
ID=56305992
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610107651.XA Pending CN105667769A (en) | 2016-02-29 | 2016-02-29 | Undercarriage for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105667769A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516089A (en) * | 2016-10-28 | 2017-03-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2020000644A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and aerial vehicle frame thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB505256A (en) * | 1937-11-04 | 1939-05-04 | Wallis Rigby | Improvements in toy aeroplanes |
| DE69419934T2 (en) * | 1993-11-05 | 2000-01-27 | Bell Helicopter Textron Inc | CHASSIS FOR HELICOPTERS |
| CN203996876U (en) * | 2014-07-04 | 2014-12-10 | 深圳市嘉兰图设计有限公司 | Four-axle aircraft carbon fiber mounting system |
| CN104443364A (en) * | 2014-12-22 | 2015-03-25 | 深圳市高巨创新科技开发有限公司 | Detachable undercarriage and quadcopter |
| 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 |
| CN205499341U (en) * | 2016-02-29 | 2016-08-24 | 无锡觅睿恪科技有限公司 | Undercarriage for unmanned aerial vehicle |
-
2016
- 2016-02-29 CN CN201610107651.XA patent/CN105667769A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB505256A (en) * | 1937-11-04 | 1939-05-04 | Wallis Rigby | Improvements in toy aeroplanes |
| DE69419934T2 (en) * | 1993-11-05 | 2000-01-27 | Bell Helicopter Textron Inc | CHASSIS FOR HELICOPTERS |
| CN203996876U (en) * | 2014-07-04 | 2014-12-10 | 深圳市嘉兰图设计有限公司 | Four-axle aircraft carbon fiber mounting system |
| CN104443364A (en) * | 2014-12-22 | 2015-03-25 | 深圳市高巨创新科技开发有限公司 | Detachable undercarriage and quadcopter |
| 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 |
| CN205499341U (en) * | 2016-02-29 | 2016-08-24 | 无锡觅睿恪科技有限公司 | Undercarriage for unmanned aerial vehicle |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516089A (en) * | 2016-10-28 | 2017-03-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2018077139A1 (en) * | 2016-10-28 | 2018-05-03 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN106516089B (en) * | 2016-10-28 | 2019-05-21 | 深圳市道通智能航空技术有限公司 | Unmanned plane |
| US10710707B2 (en) | 2016-10-28 | 2020-07-14 | Autel Robotics Co., Ltd | Unmanned aerial vehicle |
| WO2020000644A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and aerial vehicle frame thereof |
| CN110896630A (en) * | 2018-06-26 | 2020-03-20 | 深圳市大疆创新科技有限公司 | Unmanned vehicles and frame thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160615 |
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| RJ01 | Rejection of invention patent application after publication |