CN201643701U - Shooting aircraft - Google Patents
Shooting aircraft Download PDFInfo
- Publication number
- CN201643701U CN201643701U CN2009202018432U CN200920201843U CN201643701U CN 201643701 U CN201643701 U CN 201643701U CN 2009202018432 U CN2009202018432 U CN 2009202018432U CN 200920201843 U CN200920201843 U CN 200920201843U CN 201643701 U CN201643701 U CN 201643701U
- Authority
- CN
- China
- Prior art keywords
- plastic tube
- aircraft
- large plastic
- buckle
- small
- 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 mode relates to a shooting aircraft capable of flying in aid of blowing the air to provide the power. The shooting aircraft is mounted on an aircraft and composed of a small plastic tube, a large plastic tube, and two fasteners, wherein the outer diameter of the large plastic tube (1) is about 11.3 mm and the inner diameter is about 10.8 mm; the outer diameter of the small plastic tube (1) slightly smaller than the inner diameter of the large plastic tube (1) is about 10.7 mm and the inner diameter is about 10.2 mm and a weighting head (3) is sleeved on one end of the large plastic tube (1) and seals the opening to make the large plastic tube no ventilated and a sleeve ring (4) is sleeved on the large plastic tube (1) and the position of the sleeve ring can be adjusted as required; the weighting head is used for making the aircraft balanced when weighting the aircraft and the fasteners (5,6) fasten a shooting device on an aircraft machine body (7); the weighting head (3) is integrated with the fastener (5) and the sleeve ring (4) is integrated with the fastener (6); the small plastic tube (2) is inserted into the large plastic tube (1) and the small plastic tube (2) is inserted into the large plastic tube (1) and when the small plastic tube reaches to the bottom of the large plastic tube, the small plastic tube (2) flows out from the tail of the aircraft.
Description
Affiliated technical field
The utility model belongs to toy, and being specifically related to a kind ofly can provide blowing that power takes off to penetrate aircraft by air blowing.
Background technology
Toy aircraft in the market has a variety of, useful hand is thrown, and launches with rubber band, but does not also have and can provide blowing that power takes off to penetrate aircraft by air blowing.
Summary of the invention
In order to make toy aircraft more joyful, the utility model provides a kind of blowing to penetrate aircraft, and this blowing penetrated aircraft and can be provided power to take off by air blowing, also can directly throw and take off.
The technical scheme that its technical problem that solves the utility model adopts is: be equipped with on aircraft and blow injection device, this device is made up of small one and large one two plastic tubes and buckle, wherein counterweight head (3) is enclosed within of big plastic tube (1) and seals opening part and makes it stuffiness, the collar (4) is enclosed within on the big plastic tube (1), can be adjusted in the position on the big plastic tube (1) as required, buckle (5) and buckle (6) will blow injection device and be assembled on the aircraft, little plastic tube (2) inserts in the big plastic tube (1), little plastic tube (2) insert big plastic tube (1) interpolation on earth the time little plastic tube (2) grow the afterbody of aircraft.When little plastic tube is blown, the pressure that produces in the pipe forces big plastic tube to break away from little plastic tube to be blown to penetrate and go, thereby makes aircraft takeoff.
The beneficial effects of the utility model are, low cost of manufacture is simply joyful, can temper lung capacity to the people in joyful.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is an assembling side elevation of the present utility model
Fig. 2 is an exploded perspective view of the present utility model
1. big plastic tube 2. little plastic tube 3. counterweights, 4. collars, 5. buckles, 6. buckles, 7. aircraft fuselages, 8. wings, 9. empennage among the figure
The specific embodiment
In the drawings, aircraft comprises aircraft fuselage (7), wing (8), empennage (9).
Blow injection device and comprise big plastic tube (1), little plastic tube (2), counterweight head (3), the collar (4), buckle (5), buckle (6), wherein big plastic tube (1) external diameter is about the 11.3mm internal diameter and is about 10.8mm, the external diameter of little plastic tube (2) is slightly less than the internal diameter of big plastic tube (1), be about the 10.7mm internal diameter and be about 10.2mm, wherein counterweight head (3) is enclosed within of big plastic tube (1) and seals opening part and makes it stuffiness, the collar (4) is enclosed within on the big plastic tube (1), can be adjusted in the position on the big plastic tube (1) as required, the effect of counterweight head (3) is to make aircraft keep balance to the aircraft counterweight, and buckle (5) and buckle (6) will blow injection device and be anchored on the aircraft fuselage (7), counterweight head (3) and buckle (5) are one, the collar (4) and buckle (6) are one, and little plastic tube (2) inserts in the big plastic tube (1), little plastic tube (2) insert big plastic tube (1) interpolation on earth the time little plastic tube (2) grow the afterbody of aircraft.
Claims (1)
1. one kind is blown and penetrates aircraft, it is characterized in that on aircraft, being equipped with and blow injection device, this device is made up of small one and large one two plastic tubes and buckle, wherein counterweight head (3) is enclosed within of big plastic tube (1) and seals opening part and makes it stuffiness, the collar (4) is enclosed within on the big plastic tube (1), can be adjusted in the position on the big plastic tube (1) as required, buckle (5) and buckle (6) will blow injection device and be assembled on the aircraft, little plastic tube (2) inserts in the big plastic tube (1), little plastic tube (2) insert big plastic tube (1) interpolation on earth the time little plastic tube (2) grow the afterbody of aircraft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009202018432U CN201643701U (en) | 2009-12-02 | 2009-12-02 | Shooting aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009202018432U CN201643701U (en) | 2009-12-02 | 2009-12-02 | Shooting aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201643701U true CN201643701U (en) | 2010-11-24 |
Family
ID=43108895
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2009202018432U Expired - Fee Related CN201643701U (en) | 2009-12-02 | 2009-12-02 | Shooting aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201643701U (en) |
-
2009
- 2009-12-02 CN CN2009202018432U patent/CN201643701U/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: 20101124 Termination date: 20111202 |