CN206809766U - Electric capacity model aircraft - Google Patents
Electric capacity model aircraft Download PDFInfo
- Publication number
- CN206809766U CN206809766U CN201720458801.1U CN201720458801U CN206809766U CN 206809766 U CN206809766 U CN 206809766U CN 201720458801 U CN201720458801 U CN 201720458801U CN 206809766 U CN206809766 U CN 206809766U
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- CN
- China
- Prior art keywords
- plate
- electric capacity
- hollow
- socket
- cup motor
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- 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
A kind of electric capacity model aircraft, including body plate, wing plate and tail plate are the utility model is related to, wing plate and tail plate grafting are arranged on body plate, it is characterised in that：Upper end is provided with least one hollow-cup motor and the propeller being connected with hollow-cup motor output end in the middle part of described body plate, fuselage prelaminar part is embedded with electric capacity, circuit board and DC socket, the socket of DC socket is located on the bottom surface of body plate, the front portion of body plate and top both sides are additionally provided with protective plate, and the securing plate of engraved structure is additionally provided with described wing plate bottom surface；The utility model is reasonable in design, by using electric capacity and the motor plane of hollow-cup motor fit structure, with cost it is low, simple to operate, safe to use the advantages of, can be used as popular science teaching aid be used for popularize children for electricity, mechanics, aerodynamic understanding.
Description
Technical field
It the utility model is related to model aircraft technical field, more particularly to a kind of electric capacity model aircraft.
Background technology
Model aircraft mainly provides onward impulse using rubber band or battery for aircraft used at present, following lack be present
Point：First, the model aircraft potential energy storage using rubber band as power resources is less, and power is weaker, and flying distance is shorter；2nd, with
Battery is excessive as the model aircraft fuselage weight of power resources, and the explosive force that takes off is small, while cruising time long may cause
Aircraft flies to lose, and charging flow is complicated in addition, and cost is high.
The content of the invention
In order to solve deficiency of the prior art, it is low, simple to operate, safe to use that the utility model provides a kind of cost
Electric capacity model aircraft.
Technical scheme is used by the utility model solves its technical problem：
A kind of electric capacity model aircraft, including body plate, wing plate and tail plate, wing plate and tail plate grafting are arranged on machine
On body, it is characterised in that：Upper end is provided with least one hollow-cup motor and defeated with hollow-cup motor in the middle part of described body plate
Go out the propeller of end connection, fuselage prelaminar part is embedded with electric capacity, circuit board and DC socket, and the socket of DC socket is located at body plate
On bottom surface, the front portion of body plate and top both sides are additionally provided with protective plate, and engraved structure is additionally provided with described wing plate bottom surface
Securing plate.
Described electric capacity, DC socket, hollow-cup motor are electrically connected with circuit board.
Described electric capacity, circuit board and DC socket is between protective plate.
Described body plate, wing plate, tail plate, protective plate and securing plate uses PP cystosepiments.
Described hollow-cup motor is provided with two, it is identical with the propeller turning direction of two hollow-cup motor output ends connection or
It is reversed.
The beneficial effects of the utility model are：It is reasonable in design, by using electric capacity and hollow-cup motor fit structure
Motor plane, have cost it is low, simple to operate, safe to use the advantages of, can be used as popular science teaching aid be used for popularize children
For electricity, mechanics, aerodynamic understanding.
Brief description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural representation of body plate and protective plate.
Fig. 3 is tail plate and the structural representation of securing plate.
In figure：1 body plate, 2 wing plates, 3 tail plates, 4 protective plates, 5 electric capacity, 6 circuit boards, 7DC sockets, 8 power lines, 9
Hollow-cup motor, 10 propellers, 11 securing plates.
Embodiment
Embodiment of the present utility model is illustrated by particular specific embodiment below, those skilled in the art can be by this
Content disclosed by specification understands other advantages and effect of the present utility model easily.
With reference to the accompanying drawings shown in 1,2,3：A kind of electric capacity model aircraft, including body plate 1, wing plate 2 and tail plate 3, wing
Plate 2 and the grafting of tail plate 3 are arranged on body plate 1, wherein：
The described middle part upper end of body plate 1 is provided with the hollow-cup motor 9 of rear side setting and exported with hollow-cup motor 9
The propeller 10 of connection is held, the front portion of body plate 1 is embedded with electric capacity 5, circuit board 6 and DC socket 7, and the socket of DC socket 7 is located at machine
On the bottom surface of body 1, electric capacity 5, DC socket 7, hollow-cup motor 9 are electrically connected with circuit board 6, and circuit board 6 passes through DC socket 7
Charged for electric capacity 5, while can be by the electrical energy transportation of electric capacity 5 to hollow-cup motor 9, without configuring charging electricity by circuit board 6
Pond, sliding piece is set in DC socket 7, automatically powering off for electric capacity 5 and hollow-cup motor 9 can be realized in charging, when charging terminates
It is powered afterwards between electric capacity 5 and hollow-cup motor 9；
The front portion of described body plate 1 and top both sides are additionally provided with protective plate 4, and electric capacity 5, circuit board 6 and DC socket 7 are located at
Between protective plate 4, wherein being located at the inner side of protective plate 4 for connecting the power line 8 of circuit board 6 and hollow-cup motor 9, pass through protection
Plate 4 is protected each component and body plate 1；
The securing plate 11 of engraved structure is additionally provided with the described bottom surface of wing plate 2, the knot of wing plate 2 is strengthened by securing plate 11
Structure intensity, while keep minimum weight.
Described body plate 1, wing plate 2, tail plate 3, protective plate 4 and securing plate 11 uses PP cystosepiments, has resistance to
Fall, the advantages of plasticity is strong.
Meanwhile hollow-cup motor 9 can also be provided with two as needed, be connected with two output ends of hollow-cup motor 9
Propeller 10 is turned to identical or is reversed, and the flight of electric capacity model aircraft can be made when propeller 10, which turns to, to be reversed more
Steadily.
When in use, the charging of the short time of electric capacity 5 and slowly electric discharge make operation become simple to electric capacity model aircraft, can be in pole
(5-10 seconds) charges in the short time, while take-off process has enough power, and airborne period both exceeds well over extensible motor,
Also unlike battery long-time power flies to lose aircraft.
Preferred embodiments of the present utility model are the foregoing is only, as long as realizing that this practicality is new with essentially identical means
The purpose technical scheme of type, is belonged within the scope of protection of the utility model.
Claims (5)
1. a kind of electric capacity model aircraft, including body plate, wing plate and tail plate, wing plate and tail plate grafting are arranged on fuselage
On plate, it is characterised in that：Upper end is provided with least one hollow-cup motor and exported with hollow-cup motor in the middle part of described body plate
The propeller of connection is held, fuselage prelaminar part is embedded with electric capacity, circuit board and DC socket, and the socket of DC socket is located at the bottom of body plate
On face, the front portion of body plate and top both sides are additionally provided with protective plate, and adding for engraved structure is additionally provided with described wing plate bottom surface
Gu plate.
2. electric capacity model aircraft according to claim 1, it is characterised in that：Described electric capacity, DC socket, hollow-cup motor
It is electrically connected with circuit board.
3. electric capacity model aircraft according to claim 1, it is characterised in that：Described electric capacity, circuit board and DC socket position
Between protective plate.
4. electric capacity model aircraft according to claim 1, it is characterised in that：Described body plate, wing plate, tail plate,
Protective plate and securing plate use PP cystosepiments.
5. electric capacity model aircraft according to claim 1, it is characterised in that：Described hollow-cup motor is provided with two, with
The propeller turning direction of two hollow-cup motor output end connections is identical or is reversed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720458801.1U CN206809766U (en) | 2017-04-22 | 2017-04-22 | Electric capacity model aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720458801.1U CN206809766U (en) | 2017-04-22 | 2017-04-22 | Electric capacity model aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206809766U true CN206809766U (en) | 2017-12-29 |
Family
ID=60754060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720458801.1U Expired - Fee Related CN206809766U (en) | 2017-04-22 | 2017-04-22 | Electric capacity model aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206809766U (en) |
-
2017
- 2017-04-22 CN CN201720458801.1U patent/CN206809766U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171229 Termination date: 20200422 |