CN201260893Y - Model airplane - Google Patents
Model airplane Download PDFInfo
- Publication number
- CN201260893Y CN201260893Y CNU2008200517696U CN200820051769U CN201260893Y CN 201260893 Y CN201260893 Y CN 201260893Y CN U2008200517696 U CNU2008200517696 U CN U2008200517696U CN 200820051769 U CN200820051769 U CN 200820051769U CN 201260893 Y CN201260893 Y CN 201260893Y
- Authority
- CN
- China
- Prior art keywords
- fuselage
- model
- hole
- fastener
- empennage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a model plane which comprises a fuselage, greater wings and an empennage. The fuselage and the greater wings are respectively provided with an upper joint mechanism and a lower joint mechanism which are mutually cooperated to each other. The fuselage and the greater wings of the model plane can be separately placed during transportation, storage and sale, so the storage space is greatly saved, and a customer can assemble the fuselage and the greater wings together for use.
Description
Technical field
The utility model relates to a kind of model of an airplane.
Background technology
The model of an airplane is the toy that a lot of adults and child like, it is accompanied by the generation of aircraft and occurs, and long time has been arranged till now.Though the model of an airplane is had nothing in common with each other along with the variation of aircraft pattern, but there is a shortcoming substantially in traditional model of an airplane, the wing of aircraft is fixed together and can not separates with fuselage when producing exactly, in transportation, storage and sales process, must occupy bigger space, cause many inconvenience.
Summary of the invention
The technical problems to be solved in the utility model provides a kind of model of an airplane, and its fuselage separates with wing, just with both combinations, saves the space when buying use.
In order to solve the problems of the technologies described above, a kind of model of an airplane of the present utility model comprises fuselage, the big wing and empennage, is respectively arranged with the upper and lower engaging mechanism of working in coordination on the described fuselage and the big wing.
As improvement of the technical scheme, described upward engaging mechanism is arranged on the fastener base of underbelly, this fastener base cooperates fixing with the counterbore of underbelly by two vertical through holes, the sidewall of described through hole is provided with breach, described engaging mechanism down comprises fastener, fastener is provided with the reference column that is installed on the mushroom-shaped in the through hole, and the top external diameter of this reference column is bigger than lower outer diameter.
As further improvement in the technical proposal, described reference column comprises vertical installing hole and the plug that is arranged on the fastener, and plug is inlaid in the installing hole by the extension rod of its underpart, and the diameter of this plug is bigger than the external diameter of installing hole.
As further improvement in the technical proposal, described afterbody is provided with the locating hole that runs through two sides, and described empennage middle part is provided with deep gouge, and this empennage is installed in the locating hole by deep gouge.
The beneficial effects of the utility model are: owing to adopted said structure, the fuselage of this model of an airplane and the big wing are by upper and lower engaging mechanism combination, fuselage can be separated placement with the big wing in transportation, storage and sale, client just with both combinations, can save the storage area greatly when buying use.
Description of drawings
Below in conjunction with the drawings and specific embodiments the utility model is described in further detail.
Fig. 1 is STRUCTURE DECOMPOSITION figure of the present utility model;
Fig. 2 is the surface structure schematic diagram of fuselage.
The specific embodiment
With reference to Fig. 1, Fig. 2, a kind of model of an airplane of the present utility model comprises fuselage 1, the big wing 2 and empennage 3, is respectively arranged with the upper and lower engaging mechanism of working in coordination on the described fuselage 1 and the big wing 2.Owing to adopted said structure, the fuselage 1 of this model of an airplane and the big wing 2 are by upper and lower engaging mechanism combination, fuselage 1 can be separated placement with the big wing 2 in transportation, storage and sale, client just makes up both when buying use, can save the storage area greatly.
Described upward engaging mechanism is arranged on the fastener base 4 of fuselage 1 bottom, this fastener base 4 cooperates fixing with the counterbore 11 of fuselage 1 bottom by two vertical through holes 41, the sidewall of described through hole 41 is provided with breach 411, described engaging mechanism down comprises fastener 5, fastener 5 is provided with the reference column that is installed on the mushroom-shaped in the through hole 41, and the top external diameter of this reference column is bigger than lower outer diameter.
In the present embodiment, described reference column comprises vertical installing hole 511 and the plug 512 that is arranged on the fastener 5, and plug 512 is inlaid in the installing hole 511 by the extension rod 513 of its underpart, and the diameter of this plug 512 is bigger than the external diameter of installing hole 511.When fuselage 1 and the big wing 2 and combination, reference column is injected in the through hole 41, because the sidewall of through hole 41 is provided with breach 411, when reference column enters through hole 41, plug 512 struts the sidewall of through hole 41, after plug 512 passed through through hole 41 fully, the sidewall of through hole 41 resetted again plug 512 is blocked, and realized the combination that clamps of the fuselage 1 and the big wing 2.
Described fuselage 1 afterbody is provided with the locating hole 12 that runs through two sides, and described empennage 3 middle parts are provided with deep gouge 31, and this empennage 3 is installed in the locating hole 12 by deep gouge 31.Adopt this structure, also realized separating of empennage 3 and fuselage 1, again with the two assembling, more save the space in use.
Claims (4)
1. a model of an airplane comprises fuselage (1), the big wing (2) and empennage (3), it is characterized in that being respectively arranged with the upper and lower engaging mechanism of working in coordination on the described fuselage (1) and the big wing (2).
2. the model of an airplane according to claim 1, it is characterized in that the described fastener base (4) that engaging mechanism is arranged on fuselage (1) bottom of going up, this fastener base (4) cooperates fixing with the counterbore (11) of fuselage (1) bottom by two vertical through holes (41), the sidewall of described through hole (41) is provided with breach (411), described engaging mechanism down comprises fastener (5), fastener (5) is provided with the reference column that is installed on the mushroom-shaped in the through hole (41), and the top external diameter of this reference column is bigger than lower outer diameter.
3. the model of an airplane according to claim 2, it is characterized in that described reference column comprises vertical installing hole (511) and the plug (512) that is arranged on the fastener (5), plug (512) is inlaid in the installing hole (511) by the extension rod (513) of its underpart, and the diameter of this plug (512) is bigger than the external diameter of installing hole (511).
4. the model of an airplane according to claim 1, it is characterized in that described fuselage (1) afterbody is provided with the locating hole (12) that runs through two sides, described empennage (3) middle part is provided with deep gouge (31), and this empennage (3) is installed in the locating hole (12) by deep gouge (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200517696U CN201260893Y (en) | 2008-07-30 | 2008-07-30 | Model airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008200517696U CN201260893Y (en) | 2008-07-30 | 2008-07-30 | Model airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201260893Y true CN201260893Y (en) | 2009-06-24 |
Family
ID=40807359
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008200517696U Expired - Fee Related CN201260893Y (en) | 2008-07-30 | 2008-07-30 | Model airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201260893Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591073A (en) * | 2020-12-23 | 2021-04-02 | 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 |
-
2008
- 2008-07-30 CN CNU2008200517696U patent/CN201260893Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112591073A (en) * | 2020-12-23 | 2021-04-02 | 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: 20090624 Termination date: 20150730 |
|
| EXPY | Termination of patent right or utility model |