CN203793652U - Electronic governor positioning frame of agricultural unmanned aircraft - Google Patents
Electronic governor positioning frame of agricultural unmanned aircraft Download PDFInfo
- Publication number
- CN203793652U CN203793652U CN201420138959.7U CN201420138959U CN203793652U CN 203793652 U CN203793652 U CN 203793652U CN 201420138959 U CN201420138959 U CN 201420138959U CN 203793652 U CN203793652 U CN 203793652U
- Authority
- CN
- China
- Prior art keywords
- electronic governor
- positioning frame
- agricultural unmanned
- framework
- lugs
- 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
Landscapes
- Catching Or Destruction (AREA)
Abstract
The utility model discloses an electronic governor positioning frame of an agricultural unmanned aircraft. The electronic governor positioning frame comprises a frame body (1). The frame body (1) is in an elliptical annular sheet structure and is made of aircraft laminates. Lugs (2) protruding inwardly are symmetrically and integrally arranged on two sides of the lower portion of the inner annular wall of the frame body (1) and are symmetrically provided with openings (3), and the openings (3) of the lugs (2) are located on the same plane. The electronic governor positioning frame is simple in structure, easy to machine and manufacture, low in production cost and high in strength and has small bent angle and high vibration resistance; the frame matches with a base plate, and an electronic governor can be reliably mounted on the suspension of the aircraft and is convenient to demount.
Description
Technical field
The utility model belongs to agricultural vehicle technology field, specifically, and the particularly electronic governor posting on agricultural unmanned vehicle.
Background technology
Along with social development, the progress of science and technology, the work such as spray insecticide on a large scale in farmland, fertilising are progressively completed by unmanned vehicle.Electronic governor is the vitals on agricultural unmanned vehicle, and existing electronic governor is arranged in equipment compartment, and this kind of arrangement not only greatly takies equipment compartment space, affects the layout of other parts in equipment compartment; And very inconvenience of dismounting, heat dispersion is not good, and in-use performance does not ensure.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of posting of being convenient to install agricultural unmanned vehicle electronic governor.
The technical solution of the utility model is as follows: a kind of agricultural unmanned vehicle electronic governor posting, there is framework (1), described framework (1) is elliptical annular sheet body structure, and made by aviation laminate, bilateral symmetry in framework (1) internal ring wall bottom is provided with inwardly outstanding lug (2), this lug (2) is connected as a single entity with the internal ring wall of framework (1), and on each lug (2), offer an opening (3), opening (3) on two lugs (2) is symmetrical, and the opening (3) on two lugs (2) is in same level.
The utility model moulding is simple, be easy to processing and fabricating, productive costs is low.Adopt two postings described in the utility model to be arranged in the inside of aircraft fuselage cantilever, each posting is by the opening clamping base plate on the lug of inner side, base plate is coordinated with posting clamping, finally electronic governor is placed on base plate, thereby realize the installation to electronic governor.By coordinating of the utility model and base plate, electronic governor can be arranged in the cantilever of aircraft fuselage, take full advantage of on the one hand the space of cantilever, be conducive to electronic governor and carry out quickly and easily dismounting; On the other hand, for the equipment compartment of fuselage reserves more space, so that arrange other parts.Meanwhile, outline of the present utility model and cantilever cross section adapt, and can guarantee the steadiness to electronic governor support, loosening to prevent that electronic governor from occurring.The utility model adopts aviation laminate to make, and intensity is high, not yielding or damage; And angle of bend is little, aseismicity is good.
As preferably, the thickness of described framework (1) is 2-4mm.
Beneficial effect: the utility model not only simple in structure, be easy to processing and fabricating, productive costs is low, and intensity is high, angle of bend is little, aseismicity is good; The utility model coordinates with base plate, electronic governor can be arranged on to the cantilever of aircraft fuselage, and can guarantee that electronic governor installation is firm, and dismounting is convenient.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
The specific embodiment
Below in conjunction with drawings and Examples, the utility model is described in further detail:
As shown in Figure 1, the utlity model has framework 1, this framework 1 is elliptical annular sheet body structure, and is made by aviation laminate, and the thickness of framework 1 is 2-4mm.Bilateral symmetry in described framework 1 internal ring wall bottom is provided with inwardly outstanding lug 2, this lug 2 is connected as a single entity with the internal ring wall of framework 1, and on each lug 2, offer the opening 3 of a rectangle, opening 3 on two lugs 2 is symmetrical, and the opening 3 on two lugs 2 is in same level.
Claims (2)
1. an agricultural unmanned vehicle electronic governor posting, there is framework (1), it is characterized in that: described framework (1) is elliptical annular sheet body structure, and made by aviation laminate, bilateral symmetry in framework (1) internal ring wall bottom is provided with inwardly outstanding lug (2), this lug (2) is connected as a single entity with the internal ring wall of framework (1), and on each lug (2), offer an opening (3), opening (3) on two lugs (2) is symmetrical, and the opening (3) on two lugs (2) is in same level.
2. agricultural unmanned vehicle electronic governor posting according to claim 1, is characterized in that: the thickness of described framework (1) is 2-4mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420138959.7U CN203793652U (en) | 2014-03-26 | 2014-03-26 | Electronic governor positioning frame of agricultural unmanned aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420138959.7U CN203793652U (en) | 2014-03-26 | 2014-03-26 | Electronic governor positioning frame of agricultural unmanned aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203793652U true CN203793652U (en) | 2014-08-27 |
Family
ID=51375892
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420138959.7U Expired - Fee Related CN203793652U (en) | 2014-03-26 | 2014-03-26 | Electronic governor positioning frame of agricultural unmanned aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203793652U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108495787A (en) * | 2016-11-24 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Electron speed regulator and unmanned vehicle |
-
2014
- 2014-03-26 CN CN201420138959.7U patent/CN203793652U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108495787A (en) * | 2016-11-24 | 2018-09-04 | 深圳市大疆创新科技有限公司 | Electron speed regulator and unmanned vehicle |
| CN108495787B (en) * | 2016-11-24 | 2021-10-22 | 深圳市大疆创新科技有限公司 | Electronic speed regulator and unmanned vehicles |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203793652U (en) | Electronic governor positioning frame of agricultural unmanned aircraft | |
| CN203793607U (en) | Arrangement structure of electronic speed regulator of agricultural unmanned aerial vehicle | |
| CN204404008U (en) | A kind of fixed structure of car light LED circuit board | |
| CN203793608U (en) | Supporting device for electronic speed regulators of agricultural unmanned aerial vehicle | |
| CN203793599U (en) | Mounting structure for electronic speed regulators of agricultural unmanned aerial vehicle | |
| CN203793598U (en) | Agricultural unmanned aircraft body assembly | |
| CN205122667U (en) | Battery module installing support and have its battery box and vehicle | |
| CN203921204U (en) | Multi-axis aircraft horn mounting structure | |
| CN203005682U (en) | Multi-rib electric vehicle controller box | |
| CN203926700U (en) | A kind of axle part mounting platform | |
| CN202896870U (en) | High-strength machine body framework of aircraft | |
| CN203793611U (en) | Fuselage support assembly for four-axis unmanned aerial vehicle | |
| CN204296439U (en) | Part fixed support on a kind of engine | |
| CN203061686U (en) | Concave template of automobile die | |
| CN203038901U (en) | Novel graphite boat sticking point | |
| CN203793647U (en) | Arrangement structure for electronic speed regulators of agricultural aircraft | |
| CN103863549B (en) | A kind of four axle unmanned vehicle supporting fuselage assemblies | |
| CN203793589U (en) | Locating structure of top cover of four-axis agricultural aircraft | |
| CN203489442U (en) | Fixing device for air conditioner panel | |
| CN203285536U (en) | Supercharge turbo-blower | |
| CN202413932U (en) | Sunroof skeleton connecting support and structure for connecting sunroof skeleton and car body sides | |
| CN209023120U (en) | A kind of aircraft | |
| CN205524924U (en) | Strengthening rib and unmanned helicopter of fuselage and base | |
| CN203542910U (en) | Integrated anti-sliding die box | |
| CN204633098U (en) | A kind of new Joining Structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| 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: 20140827 Termination date: 20170326 |