CN202446809U - Airfoil of airplane model - Google Patents
Airfoil of airplane model Download PDFInfo
- Publication number
- CN202446809U CN202446809U CN2011205145583U CN201120514558U CN202446809U CN 202446809 U CN202446809 U CN 202446809U CN 2011205145583 U CN2011205145583 U CN 2011205145583U CN 201120514558 U CN201120514558 U CN 201120514558U CN 202446809 U CN202446809 U CN 202446809U
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- model
- aileron
- wing
- airfoil
- hinge
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Abstract
The utility model relates to an airfoil of an airplane model. The airfoil comprises a model airfoil and a model aileron. A wingtip of the model airfoil is provided with a sliding cavity, the model aileron is provided with a hinge matched with the sliding cavity, the model airfoil is in sliding connection with the model aileron by the sliding cavity and the hinge, and the tail end of the hinge is provided with an emergence-stopping heave. With the adoption of the airfoil of the airplane model, simulation activity function of the left aileron and the right aileron of the airplane model is achieved and blank of a model airplane and a toy airplane in the technical field is filled by designing an axle-center-less track type rotation sliding structure.
Description
Technical field
The utility model relates to a kind of wing of model aircraft.
Background technology
The aileron movable function of the existing model of an airplane and toy airplane has following two kinds of method for expressing usually in the same industry, and one, aileron made by single part, rotating shaft and wing assembling through the aileron two ends let aileron rotate up and down; Two, aileron and wing are used hinge assemblies, let aileron rotate up and down.
More than two kinds of technique of expressions only be applicable to partly fighter plane model, be not suitable for the passenger plane model, can not show the aileron movable function of the passenger plane class model and the transporter of partly fighting.
The utility model content
The primary and foremost purpose of the utility model is to provide a kind of also wing of the model aircraft of rotation downwards when realizing that aileron stretches backward, and the concrete scheme of the utility model is following:
A kind of wing of model aircraft comprises model wing, model aileron; The wingtip of said model wing is provided with the slip cavity; Said model aileron is provided with the hinge with said slip cavity coupling; Said model wing and said model aileron are slidingly connected through said slip cavity and said hinge; Said hinge end is provided with ends convexity.
Preferably, said model wing comprises model top wing, model lower wing; Said model top wing and said model lower wing are spliced into said model wing.
Preferably, said model aileron comprises aileron on the model, model lower aileron; Aileron and said model lower aileron are spliced into said model aileron on the said model; Said hinge is connected in aileron or said model lower aileron on the said model.
Preferably, the wingtip of said model aileron is provided with aileron and disassembles, and said aileron is disassembled with said model aileron and is slidingly connected.
The wing of the model aircraft that the utility model provides through the no axle center rail mounted rotational slide structure of design, thereby has solved model aircraft left and right sides aileron artificial activity function, has filled up the model of an airplane and the toy airplane blank in this technical field.
Description of drawings
Accompanying drawing described herein is used to provide the further understanding to the utility model, constitutes the application's a part, does not constitute the improper qualification to the utility model, in the accompanying drawings:
Fig. 1 is the utility model embodiment model aircraft grounding status architecture sketch map;
Fig. 2 is the utility model embodiment model aircraft state of flight structural representation.
The specific embodiment
To combine accompanying drawing and specific embodiment to specify the utility model below, be used for explaining the utility model in the illustrative examples and the explanation of this utility model, but not as the qualification to the utility model.
Embodiment
Like Fig. 1～shown in Figure 2, a kind of wing of model aircraft comprises model wing 1, model aileron 2; The wingtip of said model wing 1 is provided with slip cavity 11; Said model aileron 2 is provided with the hinge 21 with said slip cavity 11 couplings; Said model wing 1 is slidingly connected through said slip cavity 11 and said hinge 21 with said model aileron 2; Said hinge 21 ends are provided with and end convexity 211, prevent that hinge 21 from skidding off slip cavity 11 and causing model wing 1 and model aileron 2 to break away from.
As the part preferred version of the foregoing description scheme, said model wing 1 comprises model top wing 12, model lower wing 13; Said model top wing 12 and said model lower wing 13 are spliced into said model wing 1.Through model top wing 12 splicing, make model wing 1 inside after being shaped have cavity alleviating weight own, and be easy to mould design, economical with materials with model lower wing 13.
As the part preferred version of the foregoing description scheme, said model aileron 2 comprises aileron 22 on the model, model lower aileron 23; Aileron 22 and said model lower aileron 23 are spliced into said model aileron 2 on the said model; Said hinge 21 is connected in aileron 22 or said model lower aileron 23 on the said model.
Improvement as the foregoing description scheme; The wingtip of said model aileron 2 is provided with aileron and disassembles 3; Aileron is disassembled 3 and is slidingly connected with model aileron 2, after the wingtip of the wingtip of aileron 22 and said model lower aileron 23 merges on the said model aileron is disassembled 3 spacing and connect.
As shown in Figure 1, when the model of an airplane was in grounding state, hinge 21 stretched in the slip cavity 11, and model aileron 2 is fixedly connected with the model wing; As shown in Figure 2; When the model of an airplane is in state of flight; Hinge 21 is pulled out from slip cavity 11, and this moment, aileron 2 can be done rail mounted rotation of no axle center and sliding action through hinge 21, in like manner; Aileron is disassembled 3 from model aileron 2, pull out, aileron is disassembled 3 and is done rail mounted rotation of no axle center and sliding action.
More than technical scheme that the utility model embodiment is provided carried out detailed introduction; Used concrete example among this paper principle and the embodiment of the utility model embodiment are set forth, the explanation of above embodiment only is applicable to the principle that helps to understand the utility model embodiment; Simultaneously, for one of ordinary skill in the art, according to the utility model embodiment, the part that on the specific embodiment and range of application, all can change, in sum, this description should not be construed as the restriction to the utility model.
Claims (4)
1. the wing of a model aircraft is characterized in that:
Comprise model wing, model aileron;
The wingtip of said model wing is provided with the slip cavity;
Said model aileron is provided with the hinge with said slip cavity coupling;
Said model wing and said model aileron are slidingly connected through said slip cavity and said hinge;
Said hinge end is provided with ends convexity.
2. the wing of model aircraft as claimed in claim 1 is characterized in that:
Said model wing comprises model top wing, model lower wing;
Said model top wing and said model lower wing are spliced into said model wing.
3. the wing of model aircraft as claimed in claim 1 is characterized in that:
Said model aileron comprises aileron on the model, model lower aileron;
Aileron and said model lower aileron are spliced into said model aileron on the said model;
Said hinge is connected in aileron or said model lower aileron on the said model.
4. the wing of model aircraft as claimed in claim 1 is characterized in that:
The wingtip of said model aileron is provided with aileron and disassembles, and said aileron is disassembled with said model aileron and is slidingly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205145583U CN202446809U (en) | 2011-12-12 | 2011-12-12 | Airfoil of airplane model |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205145583U CN202446809U (en) | 2011-12-12 | 2011-12-12 | Airfoil of airplane model |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202446809U true CN202446809U (en) | 2012-09-26 |
Family
ID=46862705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205145583U Expired - Fee Related CN202446809U (en) | 2011-12-12 | 2011-12-12 | Airfoil of airplane model |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202446809U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113748450A (en) * | 2019-05-03 | 2021-12-03 | 3D打印骨公司 | Surgical training simulator |
-
2011
- 2011-12-12 CN CN2011205145583U patent/CN202446809U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113748450A (en) * | 2019-05-03 | 2021-12-03 | 3D打印骨公司 | Surgical training simulator |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120926 Termination date: 20121212 |