CN106184721B - A kind of small drone buffering foot prop - Google Patents
A kind of small drone buffering foot prop Download PDFInfo
- Publication number
- CN106184721B CN106184721B CN201610652022.5A CN201610652022A CN106184721B CN 106184721 B CN106184721 B CN 106184721B CN 201610652022 A CN201610652022 A CN 201610652022A CN 106184721 B CN106184721 B CN 106184721B
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- sleeve
- mounting base
- small drone
- foot prop
- 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.)
- Expired - Fee Related
Links
Classifications
-
- 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
-
- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Dampers (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The present invention relates to a kind of small drone buffering foot props to be vertically fixedly installed arc-shaped connecting rod on strut including mounting base and two struts being set side by side；It further include the sleeve for being socketed two connection boom ends；Two connection boom ends are connected by spring；Restraining position ring block is arranged in connecting rod surface；Sleeve lining is provided with multiple elastic raised lines with stop collar cooperation；Mounting base lower surface is provided with and the matched cavity of sleeve configuration and cover board；When unmanned plane lands, strut and ground face contact, the vibration of generation are conducted by arc-shaped connecting rod, carry out bumper and absorbing shock by spring and elastic raised line, vibration influence when landing is greatly reduced prevents to turn on one's side；Overall structure is simple, at low cost.
Description
Technical field
The present invention relates to air vehicle technique fields, buffer foot prop more specifically to a kind of small drone.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, civilian nothing
It is man-machine take photo by plane, there is more important application in agricultural, plant protection, the fields such as the disaster relief；Unmanned plane used at present especially miniature self-service
Machine, the not set buffer structure of foot prop or buffer structure are unreasonable, and when landing is easy to happen rollover situation.
Summary of the invention
The technical problem to be solved in the present invention is that in view of the above drawbacks of the prior art, providing a kind of good buffer effect
Small drone buffer foot prop.
The technical solution adopted by the present invention to solve the technical problems is:
A kind of small drone buffering foot prop is constructed, including mounting base and two struts being set side by side；Wherein, the branch
Arc-shaped connecting rod is vertically fixedly installed on bar；It further include the sleeve for being socketed two connection boom ends；Two connections
Boom end is connected by spring；Restraining position ring block is arranged in the connecting rod surface；The sleeve lining is provided with and the stop collar
Multiple elastic raised lines of cooperation；The mounting base lower surface is provided with and the matched cavity of the sleeve configuration and cover board.
Small drone of the present invention buffers foot prop, wherein the strut lower surface is provided with multiple grooves, described
Shock absorption strip is provided in groove.
Small drone of the present invention buffers foot prop, wherein the shock absorption strip surface is provided with PVC coating.
The beneficial effects of the present invention are: when unmanned plane lands, strut and ground face contact, the vibration of generation are connected by arc
Extension bar conduction carries out bumper and absorbing shock by spring and elastic raised line, and vibration influence when landing is greatly reduced prevents to turn on one's side；It is logical
It crosses cavity and sleeve connection is installed, dismounting is more convenient, convenient for storage；Overall structure is simple, at low cost.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below in conjunction with attached drawing and reality
Applying example, the invention will be further described, and the accompanying drawings in the following description is only section Example of the invention, for this field
For those of ordinary skill, without creative efforts, it can also be obtained according to these attached drawings other accompanying drawings:
Fig. 1 is the small drone buffering foot rest structure schematic diagram of present pre-ferred embodiments.
Specific embodiment
In order to keep the purposes, technical schemes and advantages of the embodiment of the present invention clearer, implement below in conjunction with the present invention
Technical solution in example carries out clear, complete description, it is clear that and described embodiment is section Example of the invention, and
It is not all of embodiment.Based on the embodiment of the present invention, those of ordinary skill in the art are not before making the creative labor
Every other embodiment obtained is put, protection scope of the present invention is belonged to.
The small drone buffering foot prop of present pre-ferred embodiments is as shown in Figure 1, include that mounting base 1 and two set side by side
The strut 2 set vertically is fixedly installed arc-shaped connecting rod 3 on strut 2；It further include the sleeve 4 for being socketed two 3 ends of connecting rod；
Two 3 ends of connecting rod are connected by spring 30；Restraining position ring block 31 is arranged in 3 surface of connecting rod；4 inner wall of sleeve is provided with and limits
Multiple elastic raised lines 40 that ring 31 cooperates；1 lower surface of mounting base is provided with and the cavity 10 of 4 form fit of sleeve and cover board (figure
In do not show)；When unmanned plane lands, strut 2 and ground face contact, the vibration of generation is conducted by arc-shaped connecting rod 3, by spring 30
Bumper and absorbing shock is carried out with elastic raised line 40, vibration influence when landing is greatly reduced prevents to turn on one's side；Overall structure is simple, at
This is low.
As shown in Figure 1,2 lower surface of strut is provided with multiple grooves 20, be provided with shock absorption strip 21 in groove 20, when landing into
The preliminary damping of row, improves damping effect.
As shown in Figure 1,21 surface of shock absorption strip is provided with PVC coating, prevent from damaging shock absorption strip 21 with ground friction.
It should be understood that for those of ordinary skills, it can be modified or changed according to the above description,
And all these modifications and variations should all belong to the protection domain of appended claims of the present invention.
Claims (3)
1. a kind of small drone buffers foot prop, including mounting base and two struts being set side by side；It is characterized in that, the branch
Arc-shaped connecting rod is vertically fixedly installed on bar；It further include the sleeve for being socketed two connection boom ends；In mounting base
The connection boom end of two of portion is connected by spring；Restraining position ring block is arranged in the connecting rod surface；The sleeve lining is set
It is equipped with multiple elastic raised lines with stop collar cooperation；The mounting base lower surface is provided with matched with the sleeve configuration
Cavity and cover board.
2. small drone according to claim 1 buffers foot prop, which is characterized in that the strut lower surface is provided with more
A groove is provided with shock absorption strip in the groove.
3. small drone according to claim 2 buffers foot prop, which is characterized in that the shock absorption strip surface is provided with
PVC coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610652022.5A CN106184721B (en) | 2016-08-10 | 2016-08-10 | A kind of small drone buffering foot prop |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610652022.5A CN106184721B (en) | 2016-08-10 | 2016-08-10 | A kind of small drone buffering foot prop |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106184721A CN106184721A (en) | 2016-12-07 |
| CN106184721B true CN106184721B (en) | 2018-12-28 |
Family
ID=57514032
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610652022.5A Expired - Fee Related CN106184721B (en) | 2016-08-10 | 2016-08-10 | A kind of small drone buffering foot prop |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184721B (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018027685A1 (en) * | 2016-08-10 | 2018-02-15 | 张琬彬 | Cushioning leg support for small unmanned aerial vehicle |
| CN106604591A (en) * | 2017-02-08 | 2017-04-26 | 广东霍德韦信息技术有限公司 | Vehicular WIFI acquisition device |
| CN107187587B (en) * | 2017-05-06 | 2019-12-17 | 广厦传媒有限公司 | A intelligent unmanned aerial vehicle for film and television aerial photography |
| CN107599735A (en) * | 2017-08-22 | 2018-01-19 | 安徽风向标清洁设备有限公司 | Damping device |
| CN107985561A (en) * | 2017-12-31 | 2018-05-04 | 滁州职业技术学院 | A kind of easy-to-dismount unmanned plane foot stool |
| CN110254697A (en) * | 2019-08-01 | 2019-09-20 | 智飞智能装备科技东台有限公司 | A kind of unmanned plane drop buffer |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101106713B1 (en) * | 2009-07-29 | 2012-01-18 | 충남대학교산학협력단 | A shock-absorbing device for helicopter |
| CN102101527A (en) * | 2009-12-18 | 2011-06-22 | 梁华山 | Horizontal damping device for landing gear |
| CN203958611U (en) * | 2014-07-11 | 2014-11-26 | 湖北易瓦特科技有限公司 | Unmanned plane foot rest |
| CA2911998A1 (en) * | 2014-11-26 | 2016-05-26 | Gilles Daigle | Unmanned aerial vehicle |
| KR101571161B1 (en) * | 2015-01-13 | 2015-11-23 | 국방기술품질원 | Unmanned aerial vehicle, Charging station and Automatic charging system for Unmanned aerial vehicle comprising the same |
| CN105438451A (en) * | 2015-11-30 | 2016-03-30 | 无锡觅睿恪科技有限公司 | Elastic protective underframe of unmanned aerial vehicle |
| CN105756551B (en) * | 2016-04-08 | 2018-03-13 | 国家电网公司 | The crawling ladder fixing device of cylindrical type equipment |
-
2016
- 2016-08-10 CN CN201610652022.5A patent/CN106184721B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN106184721A (en) | 2016-12-07 |
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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 | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181109 Address after: 518000 A-D Unit, 6th Floor, R&D Building, Fuyong Street, Baoan District, Shenzhen City, Guangdong Province, Lixinhu Funing High-tech Industrial Park Applicant after: Shenzhen Shenghe Agricultural Technology Co.,Ltd. Address before: 518000 A36, Nanshan District, Shenzhen, Guangdong. Applicant before: Zhang Wanbin |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181228 |