CN207708524U - Foam composition formula hand-thrown convolution aircraft - Google Patents
Foam composition formula hand-thrown convolution aircraft Download PDFInfo
- Publication number
- CN207708524U CN207708524U CN201721833183.0U CN201721833183U CN207708524U CN 207708524 U CN207708524 U CN 207708524U CN 201721833183 U CN201721833183 U CN 201721833183U CN 207708524 U CN207708524 U CN 207708524U
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- wing
- thrown
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- aircraft
- fuselage
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Abstract
The utility model discloses a kind of foam composition formula hand-thrown convolution aircrafts, by fuselage, big wing, machine rear wing, head counterweight original paper composition, the hand-thrown convolution aircraft is equipped with small wing, small wing is located at the top of big wing, and the utility model is all connected by inserting mode, easy to carry, it is easily assembled and stores, being thrown out can circuitous flight.
Description
Technical field
The utility model is related to toy airplane technical fields, more particularly to a kind of foam composition formula hand-thrown convolution aircraft.
Background technology
Foam hand-thrown toy airplane currently on the market generally all by fuselage, wing and machine rear wing composition, works as toy airplane
After throwing out, drop landing after flight a distance, and flight path is relatively simple, interesting relatively low, and is torn open in carrying process
Divide inconvenience, is easily damaged.
Utility model content
In order to solve the above technical problems existing in the prior art, the utility model provides a kind of easy to carry, easily
Assembling and storage thrown out after can circuitous flight foam composition formula hand-thrown convolution aircraft.
The utility model is achieved through the following technical solutions:Foam composition formula hand-thrown convolution aircraft, by fuselage, big wing,
Machine rear wing, head counterweight original paper composition, head counterweight original paper are located at fuselage front end, and big wing vertical is inserted into the big of front fuselage
It is connected in wing card slot, machine rear wing is inserted perpendicularly into the machine rear wing card slot of back body and connects, and the hand-thrown convolution aircraft is equipped with
Small wing, small wing are located at the top of big wing, and small wing vertical is inserted into the small machine being located above the big wing card slot of front fuselage
Connection in wing card slot.
Further, the small wing both ends are equipped with the buckle that can be bent downward, and the buckle being folded around is inserted on big wing
Connection in the card slot being equipped with.
Further, the big wing left and right rear portion is respectively equipped with wing flap.
The utility model has the beneficial effects that:The utility model product is easy to carry, is easily assembled and stores, can after being thrown out
Circuitous flight, it is interesting strong.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the orthographic drawing of the utility model fuselage.
Fig. 3 is the orthographic drawing of the small wing of the utility model.
Fig. 4 is the orthographic drawing of the big wing of the utility model.
Fig. 5 is the orthographic drawing of the utility model machine rear wing.
Reference numeral:1- fuselages, the big wings of 2-, the small wings of 3-, 4- machine rear wings, 5- head counterweight original papers, 6- wing flaps.7- is small
Wing card slot, the big wing card slots of 8-, 9- machine rear wing card slots, 10- buckles, 11- card slots.
Specific implementation mode
Below in conjunction with attached drawing, the utility model is described in further detail.
As shown in Figure 1:The utility model is made of fuselage 1, big wing 2, machine rear wing 4, head counterweight original paper 5, and head is matched
Weight original paper 5 is located at 1 front end of fuselage, and big wing 2 is inserted perpendicularly into the big wing card slot 8 of 1 front end of fuselage and connects, and machine rear wing 4 hangs down
Straight cutting enters to be connected in the machine rear wing card slot 9 of 1 rear end of fuselage, and the hand-thrown convolution aircraft is equipped with small wing 3, and small wing 3 is located at big
The top of wing 2, small wing 3 is inserted perpendicularly into 3 card slot of small wing above the big wing card slot in 1 front end of fuselage 8 and connects, small
3 both ends of wing are equipped with the buckle 10 that can be bent downward, and the buckle 10 being folded around, which is inserted into the card slot 11 that big wing 2 is equipped with, to be connected
It connects, 2 left and right rear portion of the big wing is respectively equipped with wing flap 6.
Each component is connected into shown in Fig. 1 when use, fuselage 1 is held, is thrown out, since the utility model is equipped with small machine
The wing 3, after throwing out can circuitous flight can be with because the utility model is all connected by inserting mode, in carrying process
It is easily split into fuselage 1, big wing 2, small wing 3, machine rear wing 4, this five parts of head counterweight original paper 5 can
To save space, can be easily assembled again when using next time.
Claims (3)
- The aircraft 1. foam composition formula hand-thrown circles round, by fuselage(1), big wing(2), machine rear wing(4), head counterweight original paper(5)Group At head counterweight original paper(5)Positioned at fuselage(1)Front end, big wing(2)It is inserted perpendicularly into fuselage(1)The big wing card slot of front end (8)Middle connection, machine rear wing(4)It is inserted perpendicularly into fuselage(1)The machine rear wing card slot of rear end(9)Interior connection, it is characterised in that:The hand It throws back spin-off machine and is equipped with small wing(3), small wing(3)Positioned at big wing(2)Top, small wing(3)It is inserted perpendicularly into and is located at machine Body(1)The big wing card slot in front end(8)The small wing card slot of top(7)Interior connection.
- The aircraft 2. foam composition formula hand-thrown as described in claim 1 circles round, it is characterised in that:The small wing(3)Both ends are set There is the buckle that can be bent downward(10), the buckle that is folded around(10)It is inserted into big wing(2)The card slot being equipped with(11)Interior connection.
- The aircraft 3. foam composition formula hand-thrown as described in claim 1 circles round, it is characterised in that:The big wing(2)Left and right Rear portion is respectively equipped with wing flap(6).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721833183.0U CN207708524U (en) | 2017-12-25 | 2017-12-25 | Foam composition formula hand-thrown convolution aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721833183.0U CN207708524U (en) | 2017-12-25 | 2017-12-25 | Foam composition formula hand-thrown convolution aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207708524U true CN207708524U (en) | 2018-08-10 |
Family
ID=63049642
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201721833183.0U Expired - Fee Related CN207708524U (en) | 2017-12-25 | 2017-12-25 | Foam composition formula hand-thrown convolution aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN207708524U (en) |
-
2017
- 2017-12-25 CN CN201721833183.0U patent/CN207708524U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180810 Termination date: 20201225 |
|
CF01 | Termination of patent right due to non-payment of annual fee |