CN204399463U - A kind of unmanned plane wing connecting mechanism - Google Patents
A kind of unmanned plane wing connecting mechanism Download PDFInfo
- Publication number
- CN204399463U CN204399463U CN201420775078.6U CN201420775078U CN204399463U CN 204399463 U CN204399463 U CN 204399463U CN 201420775078 U CN201420775078 U CN 201420775078U CN 204399463 U CN204399463 U CN 204399463U
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- screw
- connection box
- wing
- screw rod
- stationary plate
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Abstract
The utility model relates to a kind of unmanned plane wing connecting mechanism, comprise fuselage connection box, wing tie-beam, the bilateral symmetry of described fuselage connection box is provided with two joints, described joint comprises connecting portion and fixed part, described fixed part is arranged on fuselage connection box by connecting portion, described fixed part comprises stationary plate and rotor plate, described rotor plate is hinged on stationary plate, rotor plate is evenly provided with many screw rods, stationary plate is provided with multiple screw accordingly, the front portion of described wing tie-beam is also provided with matched multiple screw with described screw rod, when wing tie-beam is connected with fuselage connection box, described screw rod is successively through the screw on the screw of wing tie-beam and stationary plate, and the end that screw rod stretches out stationary plate is provided with nut, described fuselage connection box is also provided with stirrup.The utility model is novel in design, quickly and easily wing tie-beam can be connected to fuselage and connect, have value of service widely.
Description
Technical field
The utility model relates to flight equipment technical field, is specifically related to a kind of unmanned plane wing connecting mechanism.
Background technology
Along with the development of society, unmanned plane has been used in the middle of civilian work widely, and the connection mode of unmanned plane wing mainly comprises two classes, and one is that wing attachment lug is docked by bolt with fuselage attachment lug; Another kind of is that left and right wing and central wing run through fuselage, and central wing is connected with fuselage frame.Auricle connection mode is generally ears sheet form, ears sheet connection mode complex structure, is not easy to maintenance and installs, and length consuming time.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of novel in design, and wing tie-beam rationally, can be connected to the unmanned plane wing connecting mechanism on fuselage connection box by structure quickly and easily.
For solving the problems of the technologies described above, the utility model provides following technical scheme: a kind of unmanned plane wing connecting mechanism, comprise fuselage connection box, wing tie-beam, the bilateral symmetry of described fuselage connection box is provided with two joints, described joint comprises connecting portion and fixed part, described fixed part is arranged on fuselage connection box by connecting portion, described fixed part comprises stationary plate and rotor plate, described rotor plate is hinged on stationary plate, rotor plate is evenly provided with many screw rods, stationary plate is provided with multiple screw accordingly, the front portion of described wing tie-beam is also provided with matched multiple screw with described screw rod, when wing tie-beam is connected with fuselage connection box, described screw rod is successively through the screw on the screw of wing tie-beam and stationary plate, and the end that screw rod stretches out stationary plate is provided with nut, described fuselage connection box is provided with stirrup.
The beneficial effect that the utility model compared with prior art has is: although the utility model is ears structure, but connect fuselage connection box and during wing tie-beam, be connected same convenience with monaural, only the screw on wing tie-beam need be aimed at the screw on stationary plate, and connect wing tie-beam with the screw rod on rotor plate, flexible operation is easy, and connect fast, the time of installation personnel can be saved in a large number; Fuselage connection box is provided with stirrup, the stability of fuselage connection box can be improved, there is higher anti-collision performance.The utility model is novel in design, and structure is rationally, easy to operate, has value of service widely.
Accompanying drawing explanation
Fig. 1 is the utility model integral structure schematic diagram;
Fig. 2 the utility model connection diagram;
Fig. 3 is the structural representation of the utility model fuselage connection box.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
In description of the present utility model, it will be appreciated that, term " longitudinal direction ", " transverse direction ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end ", " interior ", orientation or the position relationship of the instruction such as " outward " are based on orientation shown in the drawings or position relationship, it is only the utility model for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as restriction of the present utility model.
Known with reference to Fig. 1-Fig. 3, a kind of unmanned plane wing connecting mechanism, comprise fuselage connection box 1, wing tie-beam 2, the bilateral symmetry of described fuselage connection box 1 is provided with two joints, described joint comprises connecting portion 3 and fixed part, described fixed part is arranged on fuselage connection box 1 by connecting portion 3, described fixed part comprises stationary plate 4 and rotor plate 5, described rotor plate 5 is hinged on stationary plate 4, rotor plate 5 is evenly provided with many screw rods 6, stationary plate 4 is provided with accordingly multiple screw 7, the front portion of described wing tie-beam 2 is also provided with matched multiple screw 7 with described screw rod 6, when wing tie-beam 2 is connected with fuselage connection box 1, described screw rod 6 is successively through the screw 7 on the screw 7 of wing tie-beam 2 and stationary plate 4, and the end that screw rod 6 stretches out stationary plate 4 is provided with nut, described fuselage connection box 1 is provided with stirrup 8, the screw rod 6 that described rotor plate 5 is provided with is two, the screw rod 6 that described rotor plate 5 is provided with is three, and described three screw rod 6 one-tenth equilateral triangles distribution, the screw rod 6 that described rotor plate 5 is provided with is four, and described four screw rod 6 rectangularities distribution.Although the utility model is ears structure, but connect fuselage connection box 1 and during wing tie-beam 2, be connected same convenience with monaural, only the screw 7 on wing tie-beam 2 need be aimed at the screw 7 on stationary plate 4, and connect wing tie-beam 2 with the screw rod 6 on rotor plate 5, flexible operation is easy, and connect fast, the time of installation personnel can be saved in a large number; Fuselage connection box 1 is provided with stirrup 8, the stability of fuselage connection box 1 can be improved, there is higher anti-collision performance.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all do within spirit of the present utility model and principle any amendment, equivalent to replace and improvement etc., all should be included within protection domain of the present utility model.
Claims (4)
1. a unmanned plane wing connecting mechanism, comprise fuselage connection box, wing tie-beam, it is characterized in that: the bilateral symmetry of described fuselage connection box is provided with two joints, described joint comprises connecting portion and fixed part, described fixed part is arranged on fuselage connection box by connecting portion, described fixed part comprises stationary plate and rotor plate, described rotor plate is hinged on stationary plate, rotor plate is evenly provided with many screw rods, stationary plate is provided with multiple screw accordingly, the front portion of described wing tie-beam is also provided with matched multiple screw with described screw rod, when wing tie-beam is connected with fuselage connection box, described screw rod is successively through the screw on the screw of wing tie-beam and stationary plate, and the end that screw rod stretches out stationary plate is provided with nut, described fuselage connection box is provided with stirrup.
2. a kind of unmanned plane wing connecting mechanism according to claim 1, is characterized in that: the screw rod that described rotor plate is provided with is two.
3. a kind of unmanned plane wing connecting mechanism according to claim 1, is characterized in that: the screw rod that described rotor plate is provided with is three, and described three screw rods become equilateral triangle to distribute.
4. a kind of unmanned plane wing connecting mechanism according to claim 1, is characterized in that: the screw rod that described rotor plate is provided with is four, and described four screw rod rectangularities distribution.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420775078.6U CN204399463U (en) | 2014-12-10 | 2014-12-10 | A kind of unmanned plane wing connecting mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420775078.6U CN204399463U (en) | 2014-12-10 | 2014-12-10 | A kind of unmanned plane wing connecting mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204399463U true CN204399463U (en) | 2015-06-17 |
Family
ID=53423343
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420775078.6U Expired - Fee Related CN204399463U (en) | 2014-12-10 | 2014-12-10 | A kind of unmanned plane wing connecting mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204399463U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572759A (en) * | 2020-12-29 | 2021-03-30 | 北京北航天宇长鹰无人机科技有限公司 | Wing body combines to connect and unmanned aerial vehicle |
-
2014
- 2014-12-10 CN CN201420775078.6U patent/CN204399463U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112572759A (en) * | 2020-12-29 | 2021-03-30 | 北京北航天宇长鹰无人机科技有限公司 | Wing body combines to connect and unmanned aerial vehicle |
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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 |
Granted publication date: 20150617 Termination date: 20151210 |
|
| EXPY | Termination of patent right or utility model |