CN203710689U - Kite framework - Google Patents
Kite framework Download PDFInfo
- Publication number
- CN203710689U CN203710689U CN201420108756.3U CN201420108756U CN203710689U CN 203710689 U CN203710689 U CN 203710689U CN 201420108756 U CN201420108756 U CN 201420108756U CN 203710689 U CN203710689 U CN 203710689U
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- CN
- China
- Prior art keywords
- kite
- pole
- securing member
- framework
- left wing
- 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 relates to a kite framework, particularly to a wide adjustable kite framework. The kite framework mainly comprises a framework body, a left wing support rod, a right wing support rod, a front fastening assembly, a rear fastening assembly, an adjustable fixing drawbar and opening holes and is characterized in that the appearance of the kite frame is in a triangular shape. The kite framework is reasonable in design and simple in structure; by assembling the kite frame body with the left wing support rod and the right wing support rod, adjustment and change of the width of the kite framework can be achieved, and further adjustment of the wind area of a kite can be achieved, so that the kite can be flown under different wind forces and interference of the wind forces can be reduced.
Description
Technical field
The utility model relates to a kind of kite skeleton, relates in particular the adjustable kite skeleton of a kind of wide cut.
Background technology
Kite is a kind of folk art, is also adult and children a kind of recreation loved by all.The necessary condition of kiteflying, will have certain wind-force exactly.Wind-force size has very large relation with kiteflying, in general, when wind-force is during in 2-6 level, even can kiteflying; 2-3 level wind is applicable to putting area at the kite of 0.1-0.5 square metre; When wind-force is 3-4 level, can let area fly away is the various kites of 1 square metre of left and right; When wind-force reaches 5-6 level, can put area and reach 2 square metres of above various large-scale kites.Due to every day, the size of wind-force is not changeless, and for a kite, wind-force is excessive or too smallly can cause it not fly normally, has certain limitation, thereby has had influence on people's amusement mood.
Utility model content
For the problem of above-mentioned existence, the kite skeleton that the utility model provides a kind of wide cut to regulate, in order to manufacturing kite in the situation that of different wind-force size, also can allow its normal flight.
For achieving the above object, the technical scheme that the utility model is taked is, a kind of kite skeleton, mainly comprise skeleton main body, left wing's pole, right flank pole, front securing member group, rear securing member group, adjustable steady brace and open pore, it is characterized in that, the profile of this kite skeleton is triangular in shape, in skeleton main body, be positioned at upper side top, by corresponding hinge of front securing member group, left wing's pole and right flank pole be installed, two adjustable steady braces respectively movable sleeve are joined on left wing's pole and right flank pole, on two adjustable steady braces, be respectively equipped with open pore, rear securing member assembly is contained in skeleton main body, two adjustable steady braces clamp with rear securing member group by open pore or plug-in mounting is connected cooperation.
The utility model is reasonable in design, simple in structure, adopt kite skeleton main body and left wing's pole and the assembling of right flank pole, the variation that has realized kite skeleton fabric width regulates, with reach regulate kite be subject to wind-force area size, can be the in the situation that of different wind-force, let kite fly away, reduced the interference of wind-force size.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in further detail.
Fig. 1 is structural representation of the present utility model.
In figure: 1, skeleton main body; 2, front securing member group; 3, left wing's pole; 4, adjustable steady brace; 5, open pore; 6, rear securing member group; 7, right flank pole.
The specific embodiment
In Fig. 1, a kind of kite skeleton that the utility model provides, mainly comprise skeleton main body (1), left wing's pole (3), right flank pole (7), front securing member group (2), rear securing member group (6), adjustable steady brace (4) and open pore (5), it is characterized in that, the profile of this kite skeleton is triangular in shape, in skeleton main body (1), be positioned at upper side top, by corresponding hinge of front securing member group (2), left wing's pole (3) and right flank pole (7) be installed, two adjustable steady braces (4) respectively movable sleeve are joined on left wing's pole (3) and right flank pole (7), on two adjustable steady braces (4), be respectively equipped with open pore (5), rear securing member group (6) is fitted in skeleton main body (1), two adjustable steady braces (4) clamp with rear securing member group (6) by open pore (5) or plug-in mounting is connected cooperation.
While regulating skeleton fabric width, rear securing member (6) is opened, two adjustable fixed heads (4) are departed from the annexation of rear securing member group (6), with hand, move left wing's pole (3) and right flank pole (7), it is moved as camber line around front securing member group (2), regulate between left wing's pole (3) and right flank pole (7) stretching degree in skeleton main body (1), then use affixed locking between adjustable steady brace (4) and rear securing member group (6), realize the adjusting of wide cut, finally fixing by rear securing member group (6).
Claims (1)
1. a kite skeleton, mainly comprise skeleton main body, left wing's pole, right flank pole, front securing member group, rear securing member group, adjustable steady brace and open pore, it is characterized in that, the profile of this kite skeleton is triangular in shape, in skeleton main body, be positioned at upper side top, by corresponding hinge of front securing member group, left wing's pole and right flank pole be installed, two adjustable steady braces respectively movable sleeve are joined on left wing's pole and right flank pole, on two adjustable steady braces, be respectively equipped with open pore, rear securing member assembly is contained in skeleton main body, two adjustable steady braces clamp with rear securing member group by open pore or plug-in mounting is connected cooperation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420108756.3U CN203710689U (en) | 2014-03-04 | 2014-03-04 | Kite framework |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420108756.3U CN203710689U (en) | 2014-03-04 | 2014-03-04 | Kite framework |
Publications (1)
Publication Number | Publication Date |
---|---|
CN203710689U true CN203710689U (en) | 2014-07-16 |
Family
ID=51149892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201420108756.3U Expired - Fee Related CN203710689U (en) | 2014-03-04 | 2014-03-04 | Kite framework |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN203710689U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104375200A (en) * | 2014-11-13 | 2015-02-25 | 陕西煤业化工技术研究院有限责任公司 | Modularized analog simulation experiment device achieving rapid installation, excavation and disassembly and operation method thereof |
US10336412B2 (en) | 2015-10-01 | 2019-07-02 | Clayton Morris | Adjustable area kite or wing |
CN110665239A (en) * | 2019-09-04 | 2020-01-10 | 北京航空航天大学 | Remotely-controllable electric kite based on solar sail and control method thereof |
-
2014
- 2014-03-04 CN CN201420108756.3U patent/CN203710689U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104375200A (en) * | 2014-11-13 | 2015-02-25 | 陕西煤业化工技术研究院有限责任公司 | Modularized analog simulation experiment device achieving rapid installation, excavation and disassembly and operation method thereof |
US10336412B2 (en) | 2015-10-01 | 2019-07-02 | Clayton Morris | Adjustable area kite or wing |
CN110665239A (en) * | 2019-09-04 | 2020-01-10 | 北京航空航天大学 | Remotely-controllable electric kite based on solar sail and control method thereof |
CN110665239B (en) * | 2019-09-04 | 2021-06-11 | 北京航空航天大学 | Remotely-controllable electric kite based on solar sail and control method thereof |
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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: 20140716 Termination date: 20150304 |
|
EXPY | Termination of patent right or utility model |