CN107628237A - The undercarriage being connected with unmanned plane horn - Google Patents
The undercarriage being connected with unmanned plane horn Download PDFInfo
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- CN107628237A CN107628237A CN201710872230.0A CN201710872230A CN107628237A CN 107628237 A CN107628237 A CN 107628237A CN 201710872230 A CN201710872230 A CN 201710872230A CN 107628237 A CN107628237 A CN 107628237A
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- unmanned plane
- horn
- leg
- undercarriage
- block
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Abstract
The invention discloses a kind of undercarriage being connected with unmanned plane horn, it includes setting block, elastomeric element, limited block and leg, described setting block, elastomeric element and leg is the structure being connected, described elastomeric element is between setting block and leg, described setting block is detachably connected with horn, described limited block is located at the lower section of horn, and when leg stress, for limited block with setting block to contact, the lower end of described leg is provided with bumper and absorbing shock part.The undercarriage that the present invention is connected with unmanned plane horn is adopted in such a way, simple in construction, improves the stability of unmanned plane, strengthens damping effect；Undercarriage is repeatable to be utilized, and is easy to repair, and it is convenient to change, cost-effective, enhances the portability of the unmanned plane.
Description
Technical field
The present invention relates to unmanned plane, and in particular to a kind of undercarriage being connected with unmanned plane horn.
Background technology
UAV abbreviation unmanned plane, because unmanned plane requires low to the applicability of a variety of environment, flexibility, operation
And small volume, the development advanced by leaps and bounds in recent years.
The undercarriage of unmanned plane is substantially fixed at present, and undercarriage has on flat ground and well adapted to
Property, but in non-horizontal, nonplanar just more difficult landing in place；, can be various to it due to the extensive use of unmanned plane
Quiet takeoff and landing under environment, it is also corresponding to propose to be adapted to unmanned plane with a varied topography, but existing unmanned plane undercarriage is relatively more multiple
It is miscellaneous.
The content of the invention
To solve the deficiencies in the prior art, risen and fallen it is an object of the invention to provide a kind of with what unmanned plane horn was connected
Frame, it is simple in construction, the stability of unmanned plane can be improved.
In order to realize above-mentioned target, the present invention adopts the following technical scheme that：It is a kind of to be risen and fallen with what unmanned plane horn was connected
Frame, it includes setting block, elastomeric element, limited block and leg, described setting block, elastomeric element and leg to be connected
Structure, described elastomeric element is positioned at setting between block and leg, and described setting block is detachably connected with horn, described limit
Position block is located at the lower section of horn, and when leg stress, limited block is with setting block to contact.
Further, the described extended line of leg center line and the angle of horn are 60 degree.
Further, described elastomeric element is spring.
Further, described limited block is rubber parts.
Further, the lower end of described leg is provided with bumper and absorbing shock part.
Further, the material of described bumper and absorbing shock part is rubber.
The undercarriage that the present invention is connected with unmanned plane horn is adopted in such a way, and beneficial effect is：It is simple in construction, improve
The stability of unmanned plane, strengthen damping effect；Undercarriage is repeatable to be utilized, and is easy to repair, and it is convenient to change, cost-effective, increases
The strong portability of the unmanned plane.
Brief description of the drawings
Fig. 1 is the structural representation for the undercarriage that the present invention is connected with unmanned plane horn.
In figure：1. horn, 2. set block, 3. elastomeric elements, 4. limited blocks, 5. legs, 6. beams.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other under the premise of creative work is not made
Embodiment, belong to the scope of protection of the invention.
Reference picture 1, the undercarriage being connected with unmanned plane horn include setting block 2, elastomeric element 3, limited block 4 and leg 5,
It is the structure being connected to set block 2, elastomeric element 3 and leg 5, and elastomeric element 3 is between setting block 2 and leg 5, elasticity
Part 3 uses spring, sets block 2 to be detachably connected with horn 1, limited block 4 is located at the lower section of horn 1, when the stress time limit of leg 5
Position block 4 is with setting block 2 to contact, and limited block 4 is rubber parts, and the extended line of the center line of leg 5 and the angle of horn 1 are 60 degree, branch
The lower end of pin 5 has bumper and absorbing shock part 6, and the material of bumper and absorbing shock part 6 is rubber.
In the present embodiment, when unmanned plane lands, beam 6 contacts with ground first, and beam 6 prevents leg 5 and ground
Face friction produces abrasion, protects undercarriage；Secondly, elastomeric element 3 and limited block 4 weaken the impulse force that unmanned plane declines, with this
Limited block 4 also defines that spring force is excessive simultaneously, and limited block 4 prevents the excessive reaction force acts of spring in unmanned plane and protected
Unmanned plane is protected.Block 2 is set to be detachably connected with horn 1, such undercarriage is repeatable to be utilized, and is easy to repair, and it is convenient to change, section
About cost, enhance the portability of the unmanned plane.Unmanned plane landing gear structure recited above is simple, improves unmanned plane
Stability, strengthen damping effect.
Although the present invention is described in detail with reference to the foregoing embodiments, for those skilled in the art,
It can still modify to the technical scheme described in foregoing embodiments, or which part technical characteristic is carried out etc.
With replacing, within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., this should be included in
Within the protection domain of invention.
Claims (6)
- A kind of 1. undercarriage being connected with unmanned plane horn, it is characterised in that：It include set block, elastomeric element, limited block and Leg, described setting block, elastomeric element and leg are the structure being connected, and described elastomeric element is positioned at setting block and branch Between pin, described setting block is detachably connected with horn, and described limited block is located at the lower section of horn, when the leg stress time limit Position block is with setting block to contact.
- 2. the undercarriage according to claim 2 being connected with unmanned plane horn, it is characterised in that：Described leg center line Extended line and the angle of horn be 60 degree.
- 3. the undercarriage according to claim 2 being connected with unmanned plane horn, it is characterised in that：Described elastomeric element is Spring.
- 4. the undercarriage according to claim 2 being connected with unmanned plane horn, it is characterised in that：Described limited block is rubber Glue part.
- 5. according to any described undercarriage being connected with unmanned plane horn in Claims 1-4, it is characterised in that：Described The lower end of leg is provided with bumper and absorbing shock part.
- 6. the undercarriage according to claim 5 being connected with unmanned plane horn, it is characterised in that：Described bumper and absorbing shock part Material be rubber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710872230.0A CN107628237A (en) | 2017-09-25 | 2017-09-25 | The undercarriage being connected with unmanned plane horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710872230.0A CN107628237A (en) | 2017-09-25 | 2017-09-25 | The undercarriage being connected with unmanned plane horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107628237A true CN107628237A (en) | 2018-01-26 |
Family
ID=61102605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710872230.0A Pending CN107628237A (en) | 2017-09-25 | 2017-09-25 | The undercarriage being connected with unmanned plane horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107628237A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2483881A (en) * | 2010-09-22 | 2012-03-28 | Thomas Irps | A dual-function landing gear and rotor protector for a UAV |
| CN205311896U (en) * | 2015-11-25 | 2016-06-15 | 上海云犀智能***有限公司 | Unmanned aerial vehicle multi -level buffer undercarriage |
| CN205872452U (en) * | 2016-07-18 | 2017-01-11 | 中山市万顺精密工业有限公司 | A support for among unmanned aerial vehicle |
| CN205891217U (en) * | 2016-08-22 | 2017-01-18 | 四川建筑职业技术学院 | Built -in folding horn of multiaxis rotorcraft aircraft shock attenuation undercarriage |
| 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 |
| MD4439C1 (en) * | 2016-06-27 | 2017-05-31 | Андрей Коваленко | Octocopter |
| CN107097928A (en) * | 2017-05-19 | 2017-08-29 | 北京帝测科技股份有限公司 | A kind of Rapid Combination multi-rotor unmanned aerial vehicle structure |
-
2017
- 2017-09-25 CN CN201710872230.0A patent/CN107628237A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2483881A (en) * | 2010-09-22 | 2012-03-28 | Thomas Irps | A dual-function landing gear and rotor protector for a UAV |
| CN205311896U (en) * | 2015-11-25 | 2016-06-15 | 上海云犀智能***有限公司 | Unmanned aerial vehicle multi -level buffer undercarriage |
| MD4439C1 (en) * | 2016-06-27 | 2017-05-31 | Андрей Коваленко | Octocopter |
| CN205872452U (en) * | 2016-07-18 | 2017-01-11 | 中山市万顺精密工业有限公司 | A support for among unmanned aerial vehicle |
| CN205891217U (en) * | 2016-08-22 | 2017-01-18 | 四川建筑职业技术学院 | Built -in folding horn of multiaxis rotorcraft aircraft shock attenuation undercarriage |
| 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 |
| CN107097928A (en) * | 2017-05-19 | 2017-08-29 | 北京帝测科技股份有限公司 | A kind of Rapid Combination multi-rotor unmanned aerial vehicle structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180126 |