CN208530832U - Built-in steering engine formula composite material unmanned plane wing - Google Patents
Built-in steering engine formula composite material unmanned plane wing Download PDFInfo
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- CN208530832U CN208530832U CN201821116566.0U CN201821116566U CN208530832U CN 208530832 U CN208530832 U CN 208530832U CN 201821116566 U CN201821116566 U CN 201821116566U CN 208530832 U CN208530832 U CN 208530832U
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- steering engine
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- aileron
- box
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Abstract
The utility model relates to a kind of built-in steering engine formula composite material unmanned plane wings, belong to unmanned plane field.Equipped with left floor and right floor, the upper side and downside of left floor and right floor are fitted with covering and lower covering, left floor, right floor, upper covering and lower covering have collectively constituted wing, steering engine cartridge apertures is machined on lower covering, steering engine box is installed in steering engine cartridge apertures, steering engine is fixed in steering engine box, the port of steering engine box is equipped with steering engine box cover, the outer surface of steering engine box cover is consistent with the outer surface curvature of lower covering, inboard is machined with long strip type aileron slot, aileron is installed in aileron slot, it is hinged together between aileron and wing through kevlar fabric narrowband, the steering box and the telescopic rod of steering engine installed in aileron are mutually hinged, wing inner transverse is fixed with wing girder pipe, fuselage connection girder is fitted in wing girder pipe, wing inner transverse is also equipped with steering engine penetration pipe, steering engine penetration pipe is connected with steering engine box, on right floor It is fixed with positioning pin, is filled with foam core material in the wing inner cavity between lower covering and upper covering.
Description
Technical field
The utility model belongs to unmanned plane field, specifically a kind of built-in steering engine formula composite material unmanned plane wing.
Background technique
Currently, unmanned plane is in the stage of rapid development, application field as unmanned plane flies the development of control avionics system
Also more and more extensive.Electronic unmanned plane has the characteristics that easy to operate, environmental protection and energy saving are favored by market deeply, but due to the short time
It is interior to have revolutionary breakthrough to the energy density of battery, then when increasing starting efficiency optimization housing construction to continuation of the journey is improved
Between for be just particularly important.The aileron steering engine of current small-sized fixed-wing unmanned plane mostly uses drawbar structure, will certainly be
One piece of raised pull rod control structure is reserved on wing, is not only influenced appearance and is also seriously affected pneumatic efficiency, causes unnecessary
Energy consumption.
Summary of the invention
For overcome the deficiencies in the prior art, the utility model provides a kind of built-in steering engine formula composite material unmanned plane machine
The wing can effectively improve the pneumatic efficiency of wing, increase cruise duration.
The technical scheme adopted by the utility model to solve the technical problem is as follows: a kind of built-in steering engine formula composite material nobody
Machine wing is equipped with left floor and right floor, which is characterized in that the upper side and downside of left floor and right floor are fitted with illiteracy
Skin and lower covering, left floor, right floor, upper covering and lower covering have collectively constituted wing, have been machined with steering engine cartridge apertures on lower covering,
Steering engine box is installed in steering engine cartridge apertures, steering engine is fixed in steering engine box, the port of steering engine box is equipped with steering engine box cover, steering engine box cover
Outer surface it is consistent with the outer surface curvature of lower covering, inboard is machined with long strip type aileron slot, is equipped with pair in aileron slot
The wing is hinged together between aileron and wing through kevlar fabric narrowband, the telescopic rod phase of the steering box and steering engine installed in aileron
It is hinged, wing inner transverse is fixed with wing girder pipe, and fuselage connection girder, wing inner transverse are fitted in wing girder pipe
It is also equipped with steering engine penetration pipe, steering engine penetration pipe is connected with steering engine box, and positioning pin, lower covering and upper illiteracy are fixed on right floor
Foam core material is filled in wing inner cavity between skin.
The beneficial effect of the utility model tool is that a whole set of steering engine control structure is built in inside wing, aerofoil surface light
Cunning is smooth can be effectively ensured pneumatic efficiency without any concave-convex mechanism, increase cruise duration, easy for assemble or unload.
Detailed description of the invention
Fig. 1 is the utility model structure diagram.
1. wing in figure, 2. turn to boxes, 3. ailerons, 4. left floors, 5. steering engines, 6. steering engine boxes, 7. wing girder pipes, under 8.
Covering, covering on 9., 10. fuselages connect girder, 11. steering engine penetration pipes, 12. right floors, 13. positioning pins.
Specific embodiment
The utility model is equipped with left floor 4 and right floor 12, and left floor is bonded with the upper side of 4 right floors 12 and downside
There are upper covering 9 and a lower covering 8, left floor 4, right floor 12, upper covering 9 and lower covering 8 have collectively constituted wing 1, on lower covering 8
It is machined with steering engine cartridge apertures, steering engine box 6 is installed in steering engine cartridge apertures, steering engine 5, steering engine 5 and 6 bottom of steering engine box are fixed in steering engine box 6
Portion's plate is fixed by screw, replacement easy to disassemble.The port of steering engine box 6 is equipped with steering engine box cover, the outer surface of steering engine box cover
It is consistent with the outer surface curvature of lower covering 8, it is machined with long strip type aileron slot on the inside of wing 1, aileron 3 is installed in aileron slot, it is secondary
It is hinged together between the wing 3 and wing 1 through kevlar fabric narrowband, aileron 3 and wing 1 pass through one continuous kevlar fabric of laying
Narrowband is as linkage, to guarantee that aileron 3 completes 5 instruction action of steering engine.The steering box 2 installed in aileron 3 is stretched with steering engine 5
Contracting bar is mutually hinged, and 1 inner transverse of wing is fixed with wing girder pipe 7, and fuselage connection girder 10 is fitted in wing girder pipe 7,
1 inner transverse of wing is also equipped with steering engine penetration pipe 11, and steering engine penetration pipe 11 is connected with steering engine box 6, fixed on right floor 12
There is positioning pin 13, foam core material is filled in the wing inner cavity between lower covering 8 and upper covering 9, fuselage connects 10 both ends of girder
Be inserted in inside the wing girder pipe of left and right, centre is fuselage, play the role of connecting left and right wing and fuselage, at the same with positioning pin 13
Connection positioning is collectively formed, this structure facilitates installing and dismounting.
Claims (1)
1. a kind of built-in steering engine formula composite material unmanned plane wing, is equipped with left floor and right floor, which is characterized in that left floor with
The upper side of right floor and downside are fitted with covering and lower covering, left floor, right floor, upper covering and common group of lower covering
At wing, it is machined with steering engine cartridge apertures on lower covering, steering engine box is installed in steering engine cartridge apertures, steering engine, rudder are fixed in steering engine box
The port of machine box is equipped with steering engine box cover, and the outer surface of steering engine box cover is consistent with the outer surface curvature of lower covering, and inboard adds
Work has long strip type aileron slot, is equipped with aileron in aileron slot, is hinged together between aileron and wing through kevlar fabric narrowband, secondary
The steering box and the telescopic rod of steering engine installed in the wing are mutually hinged, and wing inner transverse is fixed with wing girder pipe, wing girder pipe
It is inside fitted with fuselage connection girder, wing inner transverse is also equipped with steering engine penetration pipe, and steering engine penetration pipe is connected with steering engine box,
It is fixed with positioning pin on right floor, is filled with foam core material in the wing inner cavity between lower covering and upper covering.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116566.0U CN208530832U (en) | 2018-07-16 | 2018-07-16 | Built-in steering engine formula composite material unmanned plane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821116566.0U CN208530832U (en) | 2018-07-16 | 2018-07-16 | Built-in steering engine formula composite material unmanned plane wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208530832U true CN208530832U (en) | 2019-02-22 |
Family
ID=65387387
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821116566.0U Active CN208530832U (en) | 2018-07-16 | 2018-07-16 | Built-in steering engine formula composite material unmanned plane wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208530832U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268093A (en) * | 2020-01-21 | 2020-06-12 | 湖北吉利太力飞车有限公司 | Steering wheel mounting structure and aircraft |
| CN112009667A (en) * | 2020-07-31 | 2020-12-01 | 彩虹无人机科技有限公司 | Low-magnetism magnetic detection special wing |
| CN112339986A (en) * | 2020-09-22 | 2021-02-09 | 成都飞机工业（集团）有限责任公司 | Skin skeleton integrated intermediate-temperature rapid molding composite material structure and method |
-
2018
- 2018-07-16 CN CN201821116566.0U patent/CN208530832U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111268093A (en) * | 2020-01-21 | 2020-06-12 | 湖北吉利太力飞车有限公司 | Steering wheel mounting structure and aircraft |
| CN111268093B (en) * | 2020-01-21 | 2021-09-14 | 湖北吉利太力飞车有限公司 | Steering wheel mounting structure and aircraft |
| CN112009667A (en) * | 2020-07-31 | 2020-12-01 | 彩虹无人机科技有限公司 | Low-magnetism magnetic detection special wing |
| CN112339986A (en) * | 2020-09-22 | 2021-02-09 | 成都飞机工业（集团）有限责任公司 | Skin skeleton integrated intermediate-temperature rapid molding composite material structure and method |
| CN112339986B (en) * | 2020-09-22 | 2022-10-25 | 成都飞机工业（集团）有限责任公司 | Skin skeleton integrated intermediate-temperature rapid molding composite material structure and method |
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