CN201959566U - Wing for three-way fixed wing airplane - Google Patents
Wing for three-way fixed wing airplane Download PDFInfo
- Publication number
- CN201959566U CN201959566U CN2011200182209U CN201120018220U CN201959566U CN 201959566 U CN201959566 U CN 201959566U CN 2011200182209 U CN2011200182209 U CN 2011200182209U CN 201120018220 U CN201120018220 U CN 201120018220U CN 201959566 U CN201959566 U CN 201959566U
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- wing
- plate
- airplane
- way fixed
- model
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Abstract
The utility model relates to a wing for a three-way fixed wing airplane, in particular to a wing for a three-way fixed wing airplane, which is used for a model airplane. The wing for the three-way fixed wing airplane comprises a wing plate and wing display plates, wherein two ends of the wing plate are respectively provided with the wing display plates, and the wing display plates are obliquely distributed. The wing for the three-way fixed wing airplane has simple structure, high stationarity and strong gliding ability.
Description
Technical field
The utility model patent relates to a kind of wing of the model of an airplane, relates in particular to a kind of wing that is used for the threeway fixed wing aircraft that is used for model plane.
Background technology
The present model of an airplane of the prior art, common dynamic instability and the irrational situation of airframe structure of existing, wayward in the process of flight, the structure relative complex bothers during assembling relatively simultaneously, and is more time-consuming.
Chinese patent CN200920110220.4, a kind of wing of the model of an airplane is disclosed, form by the thin aluminum top integral manufacturing, wing is formed by the thin aluminum top integral manufacturing, the upper and lower cambered surface of the aerofoil profile of wing is the streamlined sealing arc of tadpole shape, tadpole S shape, convex-concave shape, plano-convex shape or biconvex shape, and arc inside is hollow structure.The described wing of this utility model, though simple, practical operating effect is not very good, stationarity is poor.
Summary of the invention
The utility model mainly is to solve the deficiencies in the prior art, provides a kind of simple in structure, the wing that is used for the threeway fixed wing aircraft that stationarity is high during flight.
Above-mentioned technical problem of the present utility model is mainly solved by following technical proposals:
A kind of wing that is used for the threeway fixed wing aircraft comprises wing plate and span plate, and the two ends of described wing plate are respectively equipped with span plate, and described span plate is skewed distribution.The wing of this structure, practical, the stability and the balance of wing are good when flight, have certain glide ability.
As preferably, the end of described span plate is an arcuation, and the angle of inclination of described span plate is 30 degree～45 degree.Strengthened the flowing water of wing, the resistance of wind is little during flight.
As preferably, described wing plate and span plate are working of plastics.Make simply, and help taking off fast.
Therefore, the wing that is used for the threeway fixed wing aircraft of the present utility model, simple in structure, the stationarity height, the glide ability is strong.
Description of drawings
Fig. 1 is a plan structure schematic diagram of the present utility model;
Fig. 2 structural representation of the present utility model.
The specific embodiment
Below by embodiment, and in conjunction with the accompanying drawings, the technical solution of the utility model is described in further detail.
Embodiment 1: as depicted in figs. 1 and 2, a kind of wing that is used for the threeway fixed wing aircraft, comprise wing plate 1 and span plate 2, the two ends of described wing plate 1 are respectively equipped with span plate 2, described span plate 2 is skewed distribution, the end of described span plate 2 is an arcuation, and the angle of inclination of described span plate 2 is 30 degree, and described wing plate 1 and span plate 2 are working of plastics.
Claims (3)
1. wing that is used for the threeway fixed wing aircraft, it is characterized in that: comprise wing plate (1) and span plate (2), the two ends of described wing plate (1) are respectively equipped with span plate (2), and described span plate (2) is skewed distribution.
2. the wing that is used for the threeway fixed wing aircraft according to claim 1 is characterized in that: the end of described span plate (2) is an arcuation, and the angle of inclination of described span plate (2) is 30 degree～45 degree.
3. the wing that is used for the threeway fixed wing aircraft according to claim 1 and 2 is characterized in that: described wing plate (1) and span plate (2) are working of plastics.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200182209U CN201959566U (en) | 2011-01-20 | 2011-01-20 | Wing for three-way fixed wing airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200182209U CN201959566U (en) | 2011-01-20 | 2011-01-20 | Wing for three-way fixed wing airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201959566U true CN201959566U (en) | 2011-09-07 |
Family
ID=44522089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200182209U Expired - Lifetime CN201959566U (en) | 2011-01-20 | 2011-01-20 | Wing for three-way fixed wing airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201959566U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105797392A (en) * | 2014-12-27 | 2016-07-27 | 张向东 | A foldable tilted aeromodel support component |
| CN108211376A (en) * | 2018-01-11 | 2018-06-29 | 北京涌阔科技有限公司 | Shape-adjustable arch form wing rubber band model propeller aircraft |
-
2011
- 2011-01-20 CN CN2011200182209U patent/CN201959566U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105797392A (en) * | 2014-12-27 | 2016-07-27 | 张向东 | A foldable tilted aeromodel support component |
| CN108211376A (en) * | 2018-01-11 | 2018-06-29 | 北京涌阔科技有限公司 | Shape-adjustable arch form wing rubber band model propeller aircraft |
| CN108211376B (en) * | 2018-01-11 | 2020-05-15 | 泉州憨鼠教育咨询有限公司 | Plastic model airplane with arch-shaped wing rubber band propeller |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20110907 |