CN203816220U - Soft kite - Google Patents
Soft kite Download PDFInfo
- Publication number
- CN203816220U CN203816220U CN201420102771.7U CN201420102771U CN203816220U CN 203816220 U CN203816220 U CN 203816220U CN 201420102771 U CN201420102771 U CN 201420102771U CN 203816220 U CN203816220 U CN 203816220U
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- CN
- China
- Prior art keywords
- aerofoil
- pair
- described front
- sides
- wing surface
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Abstract
The utility model discloses a soft kite, which comprises a front wing surface, a back wing surface, a plurality of lattice blocking parts, a pair of upper wing cutters, a pair of lower wing cutters and two pairs of connected air tubes, wherein the two side ends of the lattice blocking parts are connected with the two ends and the lower ends of the front wing surface and the back wing surface, and the front wing surface and the back wing surface form a semi-sealed cavity structure with openings at the upper ends; a plurality of lattice blocking parts are also connected between the front wing surface and the back wing surface, the semi-sealed cavity arranged between the front wing surface and the back wing surface is separated into a plurality of independent spaces, and the two sides of the upper end of the back wing surface are backwards recessed for forming air inlet tube; the pair of upper wing cutters are connected with the two sides of the upper end of the front wing surface, and the pair of lower wing cutters are connected with the two sides of the lower end of the front wing surface; the two pairs of connected air tubes are arranged at the middle part and the lower end of the lattice blocking parts positioned at the two sides of the front wing surface and the back wing surface, and the two pairs of connected air tubes are communicated with the semi-sealed cavity formed by the front wing surface and the back wing surface. The soft kite provided by the utility model has the advantages that the stable flight of a framework-free kite is realized, the weight is light, damage cannot be caused when the kite falls, the size is small during storage, and the carrying is convenient.
Description
Technical field
The utility model relates to kite design and manufactures, and relates in particular to a kind of software kite.
Background technology
Kite duration waves aerial in the sky of garden and public square, and kite can be used as a hobby, and kite can be made into various shapes and color, has been subject to liking of men and women, old and young, and kiteflying can also be treated neck and shoulder disease to a certain extent.Tradition kite needs the support of skeleton, does not have the kite of skeleton to fly.
Utility model content
The purpose of this utility model: a kind of software kite is provided, can realizes stabilized flight and the production of no-skeleton kite.
To achieve these goals, the technical solution of the utility model is:
A software kite, comprises front aerofoil, rear aerofoil, multi-disc lattice gear, a pair of upper wing fence, a pair of lower wing fence and two pairs of disjunctor air ducts; Described multi-disc lattice gear is list structure, and the two side ends of described multi-disc lattice gear is connected with described front aerofoil and two ends and the lower end of rear aerofoil respectively, makes the semiclosed cavity structure of described front aerofoil and a upper end open of rear aerofoil formation; Between described front aerofoil and described rear aerofoil, be also connected with multi-disc lattice gear, described lattice gear is symmetrical about the axis of described front aerofoil and rear aerofoil, described lattice gear extends to lower end from described aerofoil and the upper end of rear aerofoil, semiclosed cavity between described front aerofoil and rear aerofoil is separated into a plurality of separate spaces, and described multi-disc lattice gear is vertical with described front aerofoil and rear aerofoil respectively; The both sides, upper end of described rear aerofoil are recessed to form respectively air intake cylinder backward, and described air intake cylinder is arranged on the both sides of the lattice gear that is positioned at described front aerofoil and rear aerofoil and symmetrical about the axis of described front aerofoil and rear aerofoil; The upper end-face edge of described front aerofoil, rear aerofoil, lattice gear and air intake cylinder is positioned at same plane; Described a pair of upper wing fence is connected to the both sides, upper end of described front aerofoil, and described a pair of lower wing fence is connected to the both sides, lower end of described front aerofoil; Described a pair of disjunctor air duct is separately positioned on the middle part of the lattice gear that is positioned at described front aerofoil and rear aerofoil both sides and symmetrical about described front aerofoil and rear wing face, described a pair of disjunctor air duct extends respectively laterally, described another is separately positioned on the lower end of the lattice gear that is positioned at described front aerofoil and rear aerofoil both sides and symmetrical about described front aerofoil and rear wing face to disjunctor air duct, described another extends downwards respectively disjunctor air duct, and two pairs of described disjunctor air ducts are communicated with the semiclosed cavity that described front aerofoil and rear aerofoil form respectively.
Above-mentioned software kite, wherein, described a pair of upper wing fence and a pair of lower wing fence are triangular structures, and described a pair of upper wing fence and a pair of lower wing fence are vertical with described front aerofoil, and described a pair of upper wing fence and a pair of lower wing fence extend to the place ahead or the both sides of described front aerofoil.
Above-mentioned software kite, wherein, the both sides, lower end of described front aerofoil are respectively equipped with ribbon junction button, the junction of the disjunctor air duct described in described ribbon junction button lays respectively at and described front aerofoil.
The utility model has been realized the extremely stable flight of no-skeleton kite; No-skeleton kite is lightweight, even if drop, also can not damage; After taking in, volume is little, is convenient for carrying.
Accompanying drawing explanation
Fig. 1 is the utility model software kite structural representation.
The specific embodiment
Below in conjunction with accompanying drawing, further illustrate embodiment of the present utility model.
Refer to shown in accompanying drawing 1, a kind of software kite, comprises front aerofoil 1, rear aerofoil 2, multi-disc lattice gear 3, a pair of upper wing fence 4, a pair of lower wing fence 5 and two pairs of disjunctor air ducts 6, described multi-disc lattice gear 3 is list structures, and the two side ends of described multi-disc lattice gear 3 is connected with described front aerofoil 1 and two ends and the lower end of rear aerofoil 2 respectively, makes the semiclosed cavity structure of described front aerofoil 1 and a upper end open of rear aerofoil 2 formation, between described front aerofoil 1 and described rear aerofoil 2, be also connected with multi-disc lattice gear 3, described lattice gear 3 axis about described front aerofoil 1 and rear aerofoil 2 are symmetrical, described lattice gear 3 extends to lower end from the upper end of described aerofoil 1 and rear aerofoil 2, semiclosed cavity between described front aerofoil 1 and rear aerofoil 2 is separated into a plurality of separate spaces, and described multi-disc lattice gear 3 is vertical with described front aerofoil 1 and rear aerofoil 2 respectively, the both sides, upper end of described rear aerofoil 2 are recessed to form respectively air intake cylinder 7 backward, and described air intake cylinder 7 is arranged on the both sides of the lattice gear 3 that is positioned at described front aerofoil 1 and rear aerofoil 2 and symmetrical about the axis of described front aerofoil 1 and rear aerofoil 2, the upper end-face edge of described front aerofoil 1, rear aerofoil 2, lattice gear 3 and air intake cylinder 7 is positioned at same plane, described a pair of upper wing fence 4 is connected to the both sides, upper end of described front aerofoil 1, and described a pair of lower wing fence 5 is connected to the both sides, lower end of described front aerofoil 1, described a pair of disjunctor air duct 6 is separately positioned on the middle part of the lattice gear 3 that is positioned at described front aerofoil 1 and rear aerofoil 2 both sides and about described front aerofoil 1 and rear aerofoil 2 symmetries, described a pair of disjunctor air duct 6 extends respectively laterally, described another is separately positioned on the lower end of the lattice gear 3 that is positioned at described front aerofoil 1 and rear aerofoil 2 both sides to disjunctor air duct 6 and about described front aerofoil 1 and rear aerofoil 2 symmetries, described another extends downwards respectively disjunctor air duct 6, two pairs of described disjunctor air ducts 6 are communicated with the semiclosed cavity that described front aerofoil 1 and rear aerofoil 2 form respectively.
The upper end of the semiclosed cavity that wind the past aerofoil 1 and rear aerofoil 2 form enters, in the semiclosed cavity that front aerofoil 1 and rear aerofoil 2 form, be full of air pressure, by lattice, keeping off 3 props up kite, lattice gear 3 totally 5, a pair of upper wing fence 4 and a pair of lower wing fence 5 form the angle of attack, the stressed flight of kite, a pair of upper wing fence 4 can be connected kite string with a pair of lower wing fence 5, guarantees that flight of kites is stable; Air intake cylinder 7 can help the rapid air intake of semiclosed cavity, and simultaneously effective filtered airflow, plays the effect of stablizing flight of kites; Two pairs of disjunctor air ducts 6 can beautify kite, and have the effect of certain stabilized flight.
Described a pair of upper wing fence 4 and a pair of lower wing fence 5 are triangular structures, and described a pair of upper wing fence 4 and a pair of lower wing fence 5 are vertical with described front aerofoil 1, and described a pair of upper wing fence 4 and a pair of lower wing fence 5 extend to the place ahead or the both sides of described front aerofoil 1.
The both sides, lower end of described front aerofoil 1 are respectively equipped with ribbon junction button 8, the junction of the disjunctor air duct 7 described in described ribbon junction button 8 lays respectively at and described front aerofoil 1.Ribbon junction button 8 can be used for connecting kite's tail or ribbon, can make flight of kites effect more stable and attractive in appearance.
In sum, the utility model has been realized the extremely stable flight of no-skeleton kite; No-skeleton kite is lightweight, even if drop, also can not damage; After taking in, volume is little, is convenient for carrying.
Claims (3)
1. a software kite, is characterized in that: comprise front aerofoil, rear aerofoil, multi-disc lattice gear, a pair of upper wing fence, a pair of lower wing fence and two pairs of disjunctor air ducts; Described multi-disc lattice gear is list structure, and the two side ends of described multi-disc lattice gear is connected with described front aerofoil and two ends and the lower end of rear aerofoil respectively, makes the semiclosed cavity structure of described front aerofoil and a upper end open of rear aerofoil formation; Between described front aerofoil and described rear aerofoil, be also connected with multi-disc lattice gear, described lattice gear is symmetrical about the axis of described front aerofoil and rear aerofoil, described lattice gear extends to lower end from described aerofoil and the upper end of rear aerofoil, semiclosed cavity between described front aerofoil and rear aerofoil is separated into a plurality of separate spaces, and described multi-disc lattice gear is vertical with described front aerofoil and rear aerofoil respectively; The both sides, upper end of described rear aerofoil are recessed to form respectively air intake cylinder backward, and described air intake cylinder is arranged on the both sides of the lattice gear that is positioned at described front aerofoil and rear aerofoil and symmetrical about the axis of described front aerofoil and rear aerofoil; The upper end-face edge of described front aerofoil, rear aerofoil, lattice gear and air intake cylinder is positioned at same plane; Described a pair of upper wing fence is connected to the both sides, upper end of described front aerofoil, and described a pair of lower wing fence is connected to the both sides, lower end of described front aerofoil; Described a pair of disjunctor air duct is separately positioned on the middle part of the lattice gear that is positioned at described front aerofoil and rear aerofoil both sides and symmetrical about described front aerofoil and rear wing face, described a pair of disjunctor air duct extends respectively laterally, described another is separately positioned on the lower end of the lattice gear that is positioned at described front aerofoil and rear aerofoil both sides and symmetrical about described front aerofoil and rear wing face to disjunctor air duct, described another extends downwards respectively disjunctor air duct, and two pairs of described disjunctor air ducts are communicated with the semiclosed cavity that described front aerofoil and rear aerofoil form respectively.
2. software kite according to claim 1, it is characterized in that: described a pair of upper wing fence and a pair of lower wing fence are triangular structures, described a pair of upper wing fence and a pair of lower wing fence are vertical with described front aerofoil, and described a pair of upper wing fence and a pair of lower wing fence extend to the place ahead or the both sides of described front aerofoil.
3. software kite according to claim 1, is characterized in that: the both sides, lower end of described front aerofoil are respectively equipped with ribbon junction button, the junction of the disjunctor air duct described in described ribbon junction button lays respectively at and described front aerofoil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420102771.7U CN203816220U (en) | 2014-03-08 | 2014-03-08 | Soft kite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420102771.7U CN203816220U (en) | 2014-03-08 | 2014-03-08 | Soft kite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203816220U true CN203816220U (en) | 2014-09-10 |
Family
ID=51471765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420102771.7U Expired - Fee Related CN203816220U (en) | 2014-03-08 | 2014-03-08 | Soft kite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203816220U (en) |
-
2014
- 2014-03-08 CN CN201420102771.7U patent/CN203816220U/en not_active Expired - Fee Related
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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: 20140910 Termination date: 20150308 |
|
| EXPY | Termination of patent right or utility model |