CN105173103A - Land skid structure for small unmanned aerial vehicles - Google Patents
Land skid structure for small unmanned aerial vehicles Download PDFInfo
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- CN105173103A CN105173103A CN201510569689.4A CN201510569689A CN105173103A CN 105173103 A CN105173103 A CN 105173103A CN 201510569689 A CN201510569689 A CN 201510569689A CN 105173103 A CN105173103 A CN 105173103A
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- unmanned aerial
- pallet
- alighting gear
- spacing
- skid structure
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Abstract
The invention discloses a land skid structure for small unmanned aerial vehicles. The land skid structure for the small unmanned aerial vehicles comprises wheels, a horizontal shaft, undercarriage tables and undercarriage limiters. The wheels are arranged at the two ends of the horizontal shaft, the horizontal shaft is provided with the undercarriage tables, and the undercarriage tables can prevent undercarriages of the unmanned aerial vehicles from moving in the horizontal direction. The undercarriage limiters are arranged at the upper parts of the undercarriage tables and used for fixing the undercarriages to a land skid for the unmanned aerial vehicles relatively.
Description
Technical field
The present invention relates to the land skid structure of a kind of land skid technical field, particularly a kind of SUAV (small unmanned aerial vehicle).
Background technology
Unmanned plane is generally used for aviation target, battlefield investigation, injures the military mission such as assessment, target guide, also can be used for the non-military task such as flight test, aerial mapping simultaneously, comparatively fixed wing aircraft, unmanned plane has the functions such as hovering, vertical takeoff and landing, can execute the task more flexibly.
Traditional SUAV (small unmanned aerial vehicle), short range or extraordinary circumstances transport, the mode adopting manpower directly to lift more, not only expend certain manpower, and easily aircraft is damaged accidentally in transport process, bring much unnecessary trouble, and transport efficiency is also low.
Therefore, wish that a kind of land skid of SUAV (small unmanned aerial vehicle) can overcome or at least alleviate the above-mentioned defect of prior art.
Summary of the invention
Technical matters to be solved by this invention is to overcome the defect existed in above-mentioned prior art, and provides a kind of portable and install the land skid of easy SUAV (small unmanned aerial vehicle), solves the problem that pushes in short range or special transport situation, improves work efficiency.
For solving the problems of the technologies described above, the land skid structure of SUAV (small unmanned aerial vehicle) of the present invention comprises: wheel, transverse axis, rise and fall pallet and alighting gear spacing, described wheel is arranged on the two ends of described transverse axis, rise and fall described in described transverse axis is arranged pallet, described in rise and fall pallet restriction unmanned plane alighting gear movement in the horizontal direction; Described alighting gear is spacing be arranged on described in rise and fall the top of pallet, described alighting gear is spacing for described alighting gear is relative fixing with the land skid of described unmanned plane.
Preferably, described wheel is fixed on the two ends of described transverse axis by binding bolt.
Preferably, the shape of pallet of rising and falling described in is groove shapes.
Preferably, the spacing and described pallet that rises and falls of described alighting gear is for being welded to connect.
Preferably, the shape that described alighting gear is spacing is the downward circular arc in the center of circle.
The invention provides a kind of land skid structure of SUAV (small unmanned aerial vehicle), the land skid structure of described SUAV (small unmanned aerial vehicle) is portable and install simple and easy, solves to push problem in short range or special transport situation, improves work efficiency.
Accompanying drawing illustrates:
Fig. 1 is the structural front view of the land skid of SUAV (small unmanned aerial vehicle).
Detailed description of the invention:
For making object of the invention process, technical scheme and advantage clearly, 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 further described in more detail.In the accompanying drawings, same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Described embodiment is the present invention's part embodiment, instead of whole embodiments.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the present invention, and can not limitation of the present invention be interpreted as.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.Below in conjunction with accompanying drawing, embodiments of the invention are described in detail.
In describing the invention; it will be appreciated that; term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " etc. instruction orientation or position relationship be based on orientation shown in the drawings or position relationship; be only the present invention for convenience of description and simplified characterization; instead of instruction or imply indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as limiting the scope of the invention
Land skid structure according to the SUAV (small unmanned aerial vehicle) of the present invention one broad embodiment comprises: wheel, transverse axis, rise and fall pallet and alighting gear spacing, described wheel is arranged on the two ends of described transverse axis, rise and fall described in described transverse axis is arranged pallet, described in rise and fall pallet restriction unmanned plane alighting gear movement in the horizontal direction; Described alighting gear is spacing be arranged on described in rise and fall the top of pallet, described alighting gear is spacing for described alighting gear is relative fixing with the land skid of described unmanned plane.
As shown in Figure 1, the land skid of SUAV (small unmanned aerial vehicle) comprises: 2 binding bolts, 1,2 wheels 2, alighting gear are spacing 3, transverse axis 4 and the pallet 5 that rises and falls.
As shown in Figure 1, described 2 wheels 2 are fixed on the two ends of described transverse axis 4 respectively by 2 binding bolts 1, and rise and fall described in described transverse axis 4 is arranged pallet 5, described in the pallet 5 that rises and falls limit the alighting gear movement in the horizontal direction of unmanned plane; Rise and fall described in described alighting gear spacing 3 is arranged on the top of pallet 5, described alighting gear spacing 3 is for relative fixing with the land skid of described unmanned plane by described alighting gear.
In a not shown embodiment, the connection mode of the spacing and described pallet that rises and falls of described alighting gear is for being welded to connect.But be understandable that, described alighting gear connection mode that is spacing and the described pallet that rises and falls is not limited to be welded to connect, and in another not shown embodiment, described alighting gear is spacing and the described pallet that rises and falls is one-body molded.
As shown in Figure 1, the shape of pallet 5 of rising and falling described in is groove shapes.But be understandable that, described in the rise and fall shape of pallet be not limited to diagramatic way, in a not shown embodiment, described in the rise and fall shape of pallet be center of circle arc-shaped upwards.
As shown in Figure 1, the shape of described alighting gear spacing 3 is the downward circular arc in the center of circle.But be understandable that, the spacing shape of described alighting gear is not limited to diagramatic way, in a not shown embodiment, the spacing shape of described alighting gear is groove shapes.
Above embodiments of the invention have been described in detail, but described content being only preferred embodiment of the present invention, can not being considered to for limiting practical range of the present invention.All equalizations done according to the present patent application scope change and improve, and all should still belong within patent covering scope of the present invention.
Claims (5)
1. the land skid structure of a SUAV (small unmanned aerial vehicle), it is characterized in that, comprise: wheel, transverse axis, rise and fall pallet and alighting gear spacing, described wheel is arranged on the two ends of described transverse axis, rise and fall described in described transverse axis is arranged pallet, described in rise and fall pallet restriction unmanned plane alighting gear movement in the horizontal direction; Described alighting gear is spacing be arranged on described in rise and fall the top of pallet, described alighting gear is spacing for described alighting gear is relative fixing with the land skid of described unmanned plane.
2., according to the land skid structure of the SUAV (small unmanned aerial vehicle) described in claim 1, it is characterized in that: described wheel is fixed on the two ends of described transverse axis by binding bolt.
3., according to the land skid structure of the SUAV (small unmanned aerial vehicle) described in claim 2, it is characterized in that: described in the rise and fall shape of pallet be groove shapes.
4. according to the land skid structure of the SUAV (small unmanned aerial vehicle) described in claim 2, it is characterized in that: the spacing and described pallet that rises and falls of described alighting gear is for being welded to connect.
5. according to the land skid structure of the SUAV (small unmanned aerial vehicle) described in claim 4, it is characterized in that: the spacing shape of described alighting gear is the downward circular arc in the center of circle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510569689.4A CN105173103A (en) | 2015-09-09 | 2015-09-09 | Land skid structure for small unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510569689.4A CN105173103A (en) | 2015-09-09 | 2015-09-09 | Land skid structure for small unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105173103A true CN105173103A (en) | 2015-12-23 |
Family
ID=54895686
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510569689.4A Pending CN105173103A (en) | 2015-09-09 | 2015-09-09 | Land skid structure for small unmanned aerial vehicles |
Country Status (1)
| Country | Link |
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| CN (1) | CN105173103A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
| CN110733633A (en) * | 2019-08-30 | 2020-01-31 | 南京利剑无人机科技有限公司 | Unmanned aerial vehicle undercarriage with transfer wheel |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07277064A (en) * | 1994-04-06 | 1995-10-24 | Factory- Zero:Kk | Disassembling type carrying vehicle for small boat or the like |
| JP3052237B2 (en) * | 1997-07-02 | 2000-06-12 | 有限会社エアロコンサルタント | Helicopter ground towing equipment |
| US20090108551A1 (en) * | 2007-10-26 | 2009-04-30 | Eurocopter Deutschland Gmbh | Transport wheel for a helicopter |
| JP2011031801A (en) * | 2009-08-04 | 2011-02-17 | Yanmar Co Ltd | Cart |
| KR20110125998A (en) * | 2010-05-14 | 2011-11-22 | 한국항공우주산업 주식회사 | Remote control towing device |
| CN205221134U (en) * | 2015-09-09 | 2016-05-11 | 天峋创新（北京）科技有限公司 | Unmanned aerial vehicle's land skid |
-
2015
- 2015-09-09 CN CN201510569689.4A patent/CN105173103A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07277064A (en) * | 1994-04-06 | 1995-10-24 | Factory- Zero:Kk | Disassembling type carrying vehicle for small boat or the like |
| JP3052237B2 (en) * | 1997-07-02 | 2000-06-12 | 有限会社エアロコンサルタント | Helicopter ground towing equipment |
| US20090108551A1 (en) * | 2007-10-26 | 2009-04-30 | Eurocopter Deutschland Gmbh | Transport wheel for a helicopter |
| JP2011031801A (en) * | 2009-08-04 | 2011-02-17 | Yanmar Co Ltd | Cart |
| KR20110125998A (en) * | 2010-05-14 | 2011-11-22 | 한국항공우주산업 주식회사 | Remote control towing device |
| CN205221134U (en) * | 2015-09-09 | 2016-05-11 | 天峋创新（北京）科技有限公司 | Unmanned aerial vehicle's land skid |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
| CN110733633A (en) * | 2019-08-30 | 2020-01-31 | 南京利剑无人机科技有限公司 | Unmanned aerial vehicle undercarriage with transfer wheel |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20151223 |
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| RJ01 | Rejection of invention patent application after publication |