CN201040583Y - Unmanned airplane empennage - Google Patents
Unmanned airplane empennage Download PDFInfo
- Publication number
- CN201040583Y CN201040583Y CNU2007200519199U CN200720051919U CN201040583Y CN 201040583 Y CN201040583 Y CN 201040583Y CN U2007200519199 U CNU2007200519199 U CN U2007200519199U CN 200720051919 U CN200720051919 U CN 200720051919U CN 201040583 Y CN201040583 Y CN 201040583Y
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- empennage
- button
- unmanned plane
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Abstract
The utility model relates to an unmanned aerial vehicle empennage, comprising a first empennage and a second empennage, which are respectively one body shaped with the two liners of the unmanned aerial vehicle. The first empennage and the second empennage are fixedly connected by a connecting mechanism, which form an inverted 'V' shaped empennage. The connecting mechanism comprises a positive button disposed on one end of the first empennage and a negative button disposed on one end of the second empennage, the positive button is accommodated in the negative button. Because the utility model uses that the inverted 'V' shaped empennage is broken down into a first empennage and a second empennage which are fixedly connected or one body shaped with the two liners of the unmanned aerial vehicle, when installed, only the first empennage and the second empennage are needed to be fixedly connected by the connecting mechanism. Compared with the prior art, when installed the empennage, the two ends of the inverted 'V' shaped empennage are needed to be respectively fixedly connected with the empennage individually, the utility model is more convenient and rapid; furthermore, because the empennage is broken down into two parts, the occupied size when transporting can be greatly reduced, which is convenient for transportation.
Description
Technical field
The utility model relates to the unmanned plane field, particularly a kind of unmanned plane empennage.
Background technology
At present, " v " T tail that falls that unmanned plane adopts all is " v " T tail (industry inside is commonly referred to as down " v tail ") of integral type.This integral type shortcoming of " v tail " is: the first, and packaging volume is bigger, and transportation is inconvenient; The second, assemble on the fuselage tail pipe in, need be separately fixed on two tail pipes, installation steps and location are comparatively complicated.
The utility model content
The purpose of this utility model is, provides a kind of and can make " v " T tail of unmanned plane quick and easy for installation.
The purpose of this utility model is achieved by the following technical solution:
A kind of unmanned plane empennage comprises and unmanned plane two tail pipes integrated first empennage of difference and second empennage that described first empennage is captiveed joint by bindiny mechanism with second empennage, forms " v " font empennage; Described bindiny mechanism comprises sun button that is positioned at first empennage, one end and the moon button that is positioned at second empennage, one end; Described sun button is contained in described the moon and smashs.
Described cloudy button is " ∏ " shape along the cross section of empennage Width; Described sun button is " one " shape along the cross section of empennage Width.
Described cloudy button is " m " shape along the cross section of empennage Width; Described sun button is " u " shape along the cross section of empennage Width.
Described cloudy button and sun button are all curved along the cross section of empennage length direction.
In described bindiny mechanism, can also increase bolt of rear end plate.
Two described tail pipes are captiveed joint with second empennage with first empennage respectively.
Because the utility model adopts and will fall " V " T tail, resolve into respectively and captive joint or integrated first empennage and second empennage with unmanned plane two tail pipes, when mounted, only first empennage need be captiveed joint by described bindiny mechanism with second empennage.Than of the prior art, when empennage is installed, need will to fall separately the two ends of " V " empennage to compare with the empennage captive joint respectively, convenient, quick; And because empennage is divided into two parts, the volume that takies when transportation will significantly reduce, and is convenient to transportation.
Description of drawings
Fig. 1 is the scheme drawing of the utility model embodiment one first empennage;
Fig. 2 is the section drawing of B-B direction on the utility model embodiment one first empennage;
Fig. 3 is the scheme drawing of the utility model embodiment one second empennage;
Fig. 4 is the section drawing of A-A direction on the utility model embodiment one second empennage;
When Fig. 5 is the utility model embodiment one first and second empennage captive joint, along the part sectional view of empennage length direction;
Fig. 6 is the decomposing state scheme drawing one of the utility model embodiment one described empennage;
Fig. 7 is the decomposing state scheme drawing two of the utility model embodiment one described empennage;
Fig. 8 is the decomposing state scheme drawing three of the utility model embodiment one described empennage;
The specific embodiment
Embodiment one
Shown in Fig. 1-8, a kind of unmanned plane empennage comprises and unmanned plane two tail pipe W respectively integrated first empennage 1 and second empennage 2, and described first empennage 1 is captiveed joint by bindiny mechanism with second empennage 2, forms " v " font empennage; Place, the summit of " v " font empennage adopts the cambered surface transition; Described bindiny mechanism comprises sun button 3 that is positioned at first empennage, 1 one ends and the moon button 4 that is positioned at second empennage, 2 one ends; Described cloudy button 4 cross sections along the empennage Width are " ∏ " shape; Described sun button 3 cross sections along the empennage Width are " one " shape.When described first empennage 1 was captiveed joint with second empennage 2, described positive button can be contained in described the moon and smash.More firm for the combination that makes both, in described bindiny mechanism, can also increase bolt of rear end plate.
Shown in Fig. 5-8, when assembling during unmanned plane, be installed on the unmanned plane wing with first empennage 1 and second empennage, 2 integrated described tail pipes respectively with two after; The sun button 3 that will be positioned at first empennage, 1 one ends fastens with the moon button 4 that is positioned at second empennage, 2 one ends, utilizes bolt of rear end plate that both are fastening then, just can finish installation.Otherwise, during dismounting, get final product according to the above-mentioned steps reverse operating; Quick and easy for installation.
Embodiment two
The difference of present embodiment and embodiment one is that described cloudy button is " m " shape along the cross section of empennage Width; Described sun button is " u " shape along the cross section of empennage Width.The both sides of the described sun button of " u " shape are contained in respectively in the space of the described cloudy button of " m " shape.Unmanned plane two described tail pipes are captiveed joint respectively with second empennage 2 with described first empennage 1.When mounted, installation process is identical with embodiment one.
The distortion that the utility model also has other bindiny mechanism as described can also have other variation, is positioned at the connecting portion on first empennage and second empennage, has the characteristic of cloudy button and sun button respectively.If those skilled in the art does not need performing creative labour to make corresponding variation by inspiration of the present utility model, all should fall into the protection domain of the utility model claim.
Claims (6)
1. a unmanned plane empennage is characterized in that, comprises and unmanned plane two tail pipes integrated first empennage of difference and second empennage that described first empennage is captiveed joint by bindiny mechanism with second empennage, forms " v " font empennage; Described bindiny mechanism comprises sun button that is positioned at first empennage, one end and the moon button that is positioned at second empennage, one end; Described sun button is contained in described the moon and smashs.
2. a kind of unmanned plane empennage according to claim 1 is characterized in that, described cloudy button is " ∏ " shape along the cross section of empennage Width; Described sun button is " one " shape along the cross section of empennage Width.
3. a kind of unmanned plane empennage according to claim 1 is characterized in that, described cloudy button is " m " shape along the cross section of empennage Width; Described sun button is " u " shape along the cross section of empennage Width.
4. according to claim 1 or 2 or 3 described a kind of unmanned plane empennages, it is characterized in that described cloudy button and sun button are all curved along the cross section of empennage length direction.
5. according to claim 1 or 2 or 3 described a kind of unmanned plane empennages, it is characterized in that, in described bindiny mechanism, be equipped with bolt of rear end plate.
6. according to claim 1 or 2 or 3 described a kind of unmanned plane empennages, it is characterized in that two described tail pipes are captiveed joint with second empennage with first empennage respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200519199U CN201040583Y (en) | 2007-05-25 | 2007-05-25 | Unmanned airplane empennage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200519199U CN201040583Y (en) | 2007-05-25 | 2007-05-25 | Unmanned airplane empennage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201040583Y true CN201040583Y (en) | 2008-03-26 |
Family
ID=39252292
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200519199U Expired - Fee Related CN201040583Y (en) | 2007-05-25 | 2007-05-25 | Unmanned airplane empennage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201040583Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104608917A (en) * | 2015-01-28 | 2015-05-13 | 梧州晟裕科技有限公司 | Tail wing structure of fixed wing unmanned aerial vehicle |
| CN106184696A (en) * | 2016-07-19 | 2016-12-07 | 深圳市创翼睿翔天空科技有限公司 | Tail pipe and there is its unmanned plane |
| CN107953984A (en) * | 2017-11-29 | 2018-04-24 | 北京航空航天大学 | A kind of easy-to-mount reverse V-shaped empennage connection structure |
| CN112429198A (en) * | 2020-11-27 | 2021-03-02 | 青岛航空技术研究院(中国科学院工程热物理研究所青岛研究中心) | Small unmanned aerial vehicle type V-shaped empennage sleeve plug-in multi-degree-of-freedom locking device |
-
2007
- 2007-05-25 CN CNU2007200519199U patent/CN201040583Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104608917A (en) * | 2015-01-28 | 2015-05-13 | 梧州晟裕科技有限公司 | Tail wing structure of fixed wing unmanned aerial vehicle |
| CN106184696A (en) * | 2016-07-19 | 2016-12-07 | 深圳市创翼睿翔天空科技有限公司 | Tail pipe and there is its unmanned plane |
| CN107953984A (en) * | 2017-11-29 | 2018-04-24 | 北京航空航天大学 | A kind of easy-to-mount reverse V-shaped empennage connection structure |
| CN107953984B (en) * | 2017-11-29 | 2020-10-30 | 北京航空航天大学 | Inverted V-shaped empennage connecting structure convenient to disassemble and assemble |
| CN112429198A (en) * | 2020-11-27 | 2021-03-02 | 青岛航空技术研究院(中国科学院工程热物理研究所青岛研究中心) | Small unmanned aerial vehicle type V-shaped empennage sleeve plug-in multi-degree-of-freedom locking device |
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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: ZHUHAI XINGYU AVIATION TECHNOLOGY CO., LTD. Free format text: FORMER NAME: ZHUHAI XINGYU MODEL INDUSTRY CO.,LTD. |
|
| CP03 | Change of name, title or address |
Address after: Three Hongqiao Road, Guangdong province Zhuhai City Baijiao Industrial Park No. 3, zip code: 519125 Patentee after: Zhuhai Xingyu Model Industrial Co., Ltd. Address before: Three Hongqiao Road, Guangdong province Zhuhai City Baijiao Industrial Park No. 3, zip code: 519125 Patentee before: Zhuhai Xingyu Model Industrial Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080326 Termination date: 20160525 |