CN203666975U - Mounting fixing device for steering engine of unmanned aerial vehicle - Google Patents
Mounting fixing device for steering engine of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203666975U CN203666975U CN201320770117.9U CN201320770117U CN203666975U CN 203666975 U CN203666975 U CN 203666975U CN 201320770117 U CN201320770117 U CN 201320770117U CN 203666975 U CN203666975 U CN 203666975U
- Authority
- CN
- China
- Prior art keywords
- base plate
- steering engine
- cover plate
- fixing device
- holes
- 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
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a mounting fixing device for the steering engine of an unmanned aerial vehicle. The device comprises a base plate and a cover plate, wherein bolt holes are formed in the four corners of the base plate; by the fixing of the bolts on wings, four square holes and two round holes are formed in the middle part of the base plate; supporting parts connected with the four corners at the bottom of the cover plate are inserted into the four square holes; two screw holes are further formed in the two ends of the cover plate; two screw nuts penetrate through the screw holes and the two screw nuts penetrate through the two round holes formed in the base plate; screws are used for locking from the bottom of the base plate; the steering engine is positioned between the cover plate and the base plate and in the four supporting parts. According to the utility model, the device is simple in structure and convenient to assemble; the steering engine is mounted by horizontal arrangement instead of vertical arrangement, so that the interior vertical space is less occupied, therefore, the whole steering engine is enabled to be pasted on a fuselage more firmly.
Description
Technical field
The utility model relates to aircraft manufacturing field, is specifically related to a kind of steering engine for unmanned plane fixing device for installing.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the process controller of providing for oneself to handle.On machine, without driving compartment, but the equipment such as autopilot, process controller is installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital communication.Can under radio telecommand, as conventional airplane, take off or launch with booster rocket, also can take aerial input to by machine tool and fly.When recovery, the available mode automatic Landing the same with conventional airplane landing mission, also can reclaim with parachute or block by remote control.Can use repeatedly by repetitiousness.Be widely used in aerial reconnaissance, supervision, communication, antisubmarine, electro countermeasure etc.
Current unmanned plane, adopts the direct bonding steering wheel of mode of evolution Lu in the middle of wood chip mostly, makes that steering wheel is perpendicular puts installation, and whole like this rocking arm and check screw are all outside exposed, poor stability, and aircraft is subject to resistance large.
Utility model content
In order to overcome above-mentioned deficiency, the utility model provides a kind of close structure, the steering engine for unmanned plane fixing device for installing that stability is strong.
Scheme of the present utility model is as follows: a kind of steering engine for unmanned plane fixing device for installing, comprise base plate, cover plate, and four jiaos of described base plates are provided with bolt hole, are bolted on wing, and base plate middle part is provided with four square holes and two circular ports; Insert in four square holes with four jiaos of the cover plate bottoms strut member being connected, cover plate two ends are also provided with two screws, and two nuts, through screw until through two circular ports on base plate, use spiral shell fourth from the locking of base plate bottom, between steering wheel position and cover plate and base plate, within four strut members.
Further, described base plate one side also has rocking arm square opening, and the rocking arm that steering wheel side connects is through this square opening.
The utility model is simple in structure, easy to assembly, makes the installation of steering wheel change horizontal installation into by perpendicular putting, and has reduced inner vertical taking up room, and whole steering wheel is attached on fuselage, more firm.
Accompanying drawing explanation
Fig. 1 is the utility model perspective view.
Fig. 2 is upward view of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing, the utility model is described further.
A kind of steering engine for unmanned plane fixing device for installing, comprises base plate 1, cover plate 2, and four jiaos of described base plates are provided with bolt hole, are bolted on wing, and base plate 1 middle part is provided with four square holes and two circular ports 4; Insert in four square holes with four jiaos of 2 bottoms of the cover plate strut member being connected 3, cover plate 2 two ends are also provided with two screws, two nuts 5 are through screw until through two circular ports 4 on base plate 1, use spiral shell fourth from base plate 1 bottom locking, between 6 of steering wheels and cover plate 2 and base plate 1, within four strut members 3.
Described base plate 1 one sides also have rocking arm square opening 7, and the rocking arm 8 that steering wheel 6 sides connect is through this square opening.
Although above the specific embodiment of the present utility model has been given to describe in detail and explanation; but what should indicate is; we can carry out various equivalences to above-mentioned embodiment according to conception of the present utility model and change and revise; when its function producing does not exceed spiritual that specification sheets contains yet, all should be within protection domain of the present utility model.
Claims (2)
1. a steering engine for unmanned plane fixing device for installing, comprises base plate, cover plate, it is characterized in that four jiaos of described base plates are provided with bolt hole, is bolted on wing, and base plate middle part is provided with four square holes and two circular ports; Insert in four square holes with four jiaos of the cover plate bottoms strut member being connected, cover plate two ends are also provided with two screws, and two nuts, through screw until through two circular ports on base plate, use spiral shell fourth from the locking of base plate bottom, between steering wheel position and cover plate and base plate, within four strut members.
2. a kind of steering engine for unmanned plane fixing device for installing according to claim 1, is characterized in that described base plate one side also has rocking arm square opening, and the rocking arm that steering wheel side connects is through this square opening.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320770117.9U CN203666975U (en) | 2013-11-30 | 2013-11-30 | Mounting fixing device for steering engine of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320770117.9U CN203666975U (en) | 2013-11-30 | 2013-11-30 | Mounting fixing device for steering engine of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203666975U true CN203666975U (en) | 2014-06-25 |
Family
ID=50963295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320770117.9U Expired - Fee Related CN203666975U (en) | 2013-11-30 | 2013-11-30 | Mounting fixing device for steering engine of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203666975U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016065509A1 (en) * | 2014-10-27 | 2016-05-06 | 深圳市尚腾影科技有限公司 | Model aeroplane and steering engine assembly structure for same |
-
2013
- 2013-11-30 CN CN201320770117.9U patent/CN203666975U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016065509A1 (en) * | 2014-10-27 | 2016-05-06 | 深圳市尚腾影科技有限公司 | Model aeroplane and steering engine assembly structure for same |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11014666B2 (en) | Airframe | |
| CN205150264U (en) | Can dismantle unmanned aerial vehicle battery package assembly | |
| CN106945827B (en) | Floating body throwing type amphibious four-rotor unmanned aerial vehicle | |
| CN205239913U (en) | Top load unmanned aerial vehicle convenient to take off and land fast | |
| WO2020033978A3 (en) | Modular and dynamically reconfigurable flying systems encompassing flying vehicle modules | |
| CN205469856U (en) | Power supply module , Unmanned vehicles and remote control mobile device | |
| CN205293106U (en) | Novel unmanned aerial vehicle nacelle mounting structure | |
| CN105314110A (en) | Unmanned aerial vehicle with umbrella | |
| CN205221105U (en) | Solar energy VTOL fixed wing uavs | |
| CN203623966U (en) | Cargo delivery device for unmanned helicopter | |
| CN204368432U (en) | A kind of can the animal-breeding rotary wind type unmanned plane of simultaneously spray disinfectant agent and liquid medicine | |
| CN204223179U (en) | A kind of three rotor wing unmanned aerial vehicles high with flexible hook accurate positioning intensity | |
| CN204473152U (en) | A kind of integral type unmanned plane | |
| CN105151287A (en) | Quadrotor unmanned aerial vehicle easy to install | |
| CN203666975U (en) | Mounting fixing device for steering engine of unmanned aerial vehicle | |
| CN204916155U (en) | Multipurpose unmanned aerial vehicle | |
| CN203391991U (en) | Task load-oriented modularized unmanned helicopter | |
| CN203486130U (en) | Camera cabin at bottom of unmanned aerial vehicle | |
| CN204279925U (en) | The unmanned vehicle that alighting gear quick release is changed | |
| CN205221099U (en) | Many rotor crafts of flexible combination | |
| CN204979251U (en) | Novel spray rinsing unmanned aerial vehicle device | |
| CN203666970U (en) | Driving connecting structure for aileron of unmanned aerial vehicle | |
| CN103019243B (en) | Based on the self-navigation aircraft of cross flow fan | |
| CN203465855U (en) | Obstacle alarm system for unmanned plane | |
| CN108657435A (en) | A kind of stability it is good agricultural nobody spill medicine device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: ANHUI TIANLU AVIAT TECHNOLOGY CO., LTD. Free format text: FORMER NAME: HUAIBEI TIANLU AVIAT TECHNOLOGY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 235000, F industrial building, Longhu Industrial Park, Huaibei Economic Development Zone, Anhui Province, No. 3, building 1-2 Patentee after: Anhui's aviation Polytron Technologies Inc Address before: 235000, F industrial building, Longhu Industrial Park, Huaibei Economic Development Zone, Anhui Province, No. 3, building 1-2 Patentee before: Huaibei City Tian Lu Aerotech Inc. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Mounting fixing device for steering engine of unmanned aerial vehicle Effective date of registration: 20160329 Granted publication date: 20140625 Pledgee: Huaibei City Development Zone Hongfu Construction Development Co. Ltd. Pledgor: Anhui's aviation Polytron Technologies Inc Registration number: 2016340000013 |
|
| PLDC | Enforcement, change and cancellation of contracts on pledge of patent right or utility model | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20170512 Granted publication date: 20140625 Pledgee: Huaibei City Development Zone Hongfu Construction Development Co. Ltd. Pledgor: Anhui's aviation Polytron Technologies Inc Registration number: 2016340000013 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Mounting fixing device for steering engine of unmanned aerial vehicle Effective date of registration: 20170522 Granted publication date: 20140625 Pledgee: Huaibei City Development Zone Hongfu Construction Development Co. Ltd. Pledgor: Anhui's aviation Polytron Technologies Inc Registration number: 2017340000063 |
|
| 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: 20140625 Termination date: 20201130 |