CN201586388U - Double-layer glider airplane kite - Google Patents
Double-layer glider airplane kite Download PDFInfo
- Publication number
- CN201586388U CN201586388U CN2009201990037U CN200920199003U CN201586388U CN 201586388 U CN201586388 U CN 201586388U CN 2009201990037 U CN2009201990037 U CN 2009201990037U CN 200920199003 U CN200920199003 U CN 200920199003U CN 201586388 U CN201586388 U CN 201586388U
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- kite
- fuselage
- double
- wing panel
- fin
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Abstract
Disclosed is a double-layer glider airplane kite, which belongs to the technical field of kites. The utility model comprises a barrel-shaped body, a wing panel which is arranged on the body, and a horizontal tail and a vertical tail which are arranged at the tail of the body, which is characterized in that: the wing panel comprises an upper wing panel arranged on the back of the body and a lower wing panel arranged on the abdomen of the body, wherein a wing panel supporting frame is arranged between the upper wing panel and the lower wing panel. The double-layer glider airplane kite has novel structure and reasonable design. Due to the arrangement of the upper wing panel on the back of the body of the airplane and to the arrangement of the lower wing panel on the abdomen of the body, and by using the functions of the framework and supporting rod, the whole kite has strong stereoscopic sensation. Due to the arrangement of the upper and lower wing panels, the kite has two windward surfaces, while a good air exhaust passage is formed in the middle of two upper and lower layers of wing panels. Due to the flight test, the kite flies more steadily, and when the wind direction and wind speed change, the self-regulation capacity of the kite is stronger.
Description
Technical field
The utility model belongs to the kite technical field, is specifically related to a kind of kite of solid type structure.
Background technology
Kite is a kind of traditional folk art, and the structure of kite has all comprised kite main body and the bracing frame that is distributed on the kite main body substantially.Existing kite is generally the plane kite, and third dimension and aesthetic measure are all relatively poor, and now along with people to the things each side require raising, the aesthetic measure of kite is also had higher requirement.And wind-engaging is to very big with Influences on Wind Velocity in flight for existing kite, and himself can not be regulated.
The utility model content
At the problem that prior art exists, the purpose of this utility model is to design the technical scheme that a kind of double-deck aerodone aircraft kite is provided.
Described a kind of double-deck aerodone aircraft kite, comprise the tubular fuselage, be arranged on the fin on the fuselage and be arranged on the tailplane and the vertical tail of afterbody, it is characterized in that described fin comprises upper panel that is arranged on fuselage back and the lower panel that is arranged on belly, is provided with the fin bracing frame between upper panel and the lower panel.
Described a kind of double-deck aerodone aircraft kite is characterized in that described fuselage head is provided with ventilating opening, and fuselage interior is symmetrical arranged fuselage framework.
Described a kind of double-deck aerodone aircraft kite is characterized in that described upper panel and lower panel are symmetrical arranged up and down, and upper panel and lower panel edge side are provided with sleeve, interts in the sleeve fin skeleton is set.
Described a kind of double-deck aerodone aircraft kite, it is characterized in that described fin bracing frame is symmetricly set between upper panel and the lower panel, the fin bracing frame comprises vertical supporting rod arranged in a crossed manner and the transverse supporting rod that is arranged on the fin, and vertical supporting rod is connected by the connector that is provided with transverse supporting rod and is fixed on upper panel and the lower panel.
Described a kind of double-deck aerodone aircraft kite is characterized in that described fuselage framework becomes the radian structure, and intersects at nearly ventilating opening place.
Above-mentioned a kind of double-deck aerodone aircraft kite, novel structure, reasonable in design, fuselage back at aircraft is provided with upper panel, belly is provided with lower panel, and utilize the effect of skeleton and support bar, make whole kite have stronger third dimension, upper panel and lower panel must be provided with, and make kite that two wind surfaces be arranged, and have formed a good air exhaust passage in the middle of the two-layer up and down lower panel, behind test flight, this flight of kites is more steady, and when wind direction and wind velocity changed, self regulating power of kite was stronger.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the vertical view of Fig. 1.
Among the figure: the 1-ventilating opening; The 2-upper panel; The 3-lower panel; The 4-fuselage; The 5-tailplane; The 6-vertical tail; The 7-vertical supporting rod; The 8-transverse supporting rod; 9-fin skeleton; 10,10a-fuselage framework.
The specific embodiment
As shown in the figure, a kind of double-deck aerodone aircraft kite comprises tubular fuselage 4, is arranged on the fin on the fuselage 4 and is arranged on the tailplane 5 and the vertical tail 6 of fuselage 4 afterbodys, fuselage 4 heads are provided with ventilating opening 1, fuselage 4 inside are symmetrical arranged fuselage framework 10,10a, fuselage framework 10,10a becomes the radian structure, and in nearly ventilating opening 1 place intersection, fuselage framework 10,10a have been propped up fuselage 4; Fin comprises upper panel 2 that is arranged on fuselage 4 backs and the lower panel 3 that is arranged on fuselage 4 bellies, upper panel 2 and lower panel 3 are symmetrically arranged, and between upper panel 2 and lower panel 3, the fin bracing frame is set, upper panel 2 and lower panel 3 edge sides are provided with sleeve, intert in the sleeve fin skeleton 9 is set, the fin bracing frame comprises vertical supporting rod arranged in a crossed manner 7 and the transverse supporting rod 8 that is arranged on the fin, vertical supporting rod 7 is connected by the knuckle connector that is provided with transverse supporting rod 8 and is fixed on upper panel 2 and the lower panel 3, the specification of this kite is 120*90cm, and this kite is fit to that children let fly away more than 8 years old.
Claims (5)
1. double-deck aerodone aircraft kite, comprise tubular fuselage (4), be arranged on the fin on the fuselage (4) and be arranged on the tailplane (5) and the vertical tail (6) of fuselage (4) afterbody, it is characterized in that described fin comprises the upper panel (2) that is arranged on fuselage (4) back and is arranged on the lower panel (3) of fuselage (4) belly, is provided with the fin bracing frame between upper panel (2) and the lower panel (3).
2. a kind of double-deck aerodone aircraft kite as claimed in claim 1 is characterized in that described fuselage (4) head is provided with ventilating opening (1), fuselage (4) inside be symmetrical arranged fuselage framework (10,10a).
3. a kind of double-deck aerodone aircraft kite as claimed in claim 1 is characterized in that described upper panel (2) and lower panel (3) are symmetrical arranged up and down, and upper panel (2) and lower panel (3) edge side are provided with sleeve, interts in the sleeve fin skeleton (9) is set.
4. a kind of double-deck aerodone aircraft kite as claimed in claim 1, it is characterized in that described fin bracing frame is symmetricly set between upper panel (2) and the lower panel (3), the fin bracing frame comprises vertical supporting rod arranged in a crossed manner (7) and is arranged on transverse supporting rod (8) on the fin that vertical supporting rod (7) is connected by the connector that is provided with transverse supporting rod (8) and is fixed on upper panel (2) and the lower panel (3).
5. a kind of double-deck aerodone aircraft kite as claimed in claim 2, it is characterized in that described fuselage framework (10,10a) become the radian structure, and locate to intersect at nearly ventilating opening (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201990037U CN201586388U (en) | 2009-10-22 | 2009-10-22 | Double-layer glider airplane kite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009201990037U CN201586388U (en) | 2009-10-22 | 2009-10-22 | Double-layer glider airplane kite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201586388U true CN201586388U (en) | 2010-09-22 |
Family
ID=42746155
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009201990037U Expired - Fee Related CN201586388U (en) | 2009-10-22 | 2009-10-22 | Double-layer glider airplane kite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201586388U (en) |
-
2009
- 2009-10-22 CN CN2009201990037U patent/CN201586388U/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 | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100922 Termination date: 20111022 |