CN201370967Y - Electric remote control propeller-driven aircraft - Google Patents
Electric remote control propeller-driven aircraft Download PDFInfo
- Publication number
- CN201370967Y CN201370967Y CN200920051645U CN200920051645U CN201370967Y CN 201370967 Y CN201370967 Y CN 201370967Y CN 200920051645 U CN200920051645 U CN 200920051645U CN 200920051645 U CN200920051645 U CN 200920051645U CN 201370967 Y CN201370967 Y CN 201370967Y
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- remote control
- aircraft
- wing
- drive motors
- control circuit
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Abstract
The utility model relates to an electric remote control propeller-driven aircraft, which aims to solve the problems existing in the prior and similar art that the structure is more complicated, the cost is higher; the aircraft is more bulky, and the aircraft steers horizontally. The essential technical scheme is that the electric remote propeller-driven aircraft comprises an aircraft body, a left wing, a right wing, a tail wing, a battery, a power device, a remote control circuit and a steering device, wherein the power device consists of a drive motor mounted on the inner side at the head part of the aircraft body and a propeller fixed on the driving shaft of the drive motor and positioned on the outer side at the head part of the aircraft body; and the battery carries out power supply connection with the drive motor through the remote control circuit. The electric remote propeller-driven aircraft is characterized in that the steering device consists of vertical through holes respectively arranged on the left wing and the right wing, a steering motor in which the axis of a rotating shaft mounted in each through hole is arranged vertically, and a steering impeller fixed on the shaft of the steering motor; and the battery carries out power supply connection with the steering motor through the remote control circuit.
Description
Technical field
The utility model relates to the baby plane that fixed wing is arranged by people's remote control, specifically is meant a kind of toy or aviation model propeller aircraft that can fly up and of electric remote control.
Background technology
Present existing similar electric remote control propeller aeroplane, a kind of propeller formula electric remote control toy airplane just like Chinese patent 200820043191.X number, structure comprises fuselage and is arranged at port wing, starboard wing, empennage, power supply, power set, remote control circuit, transfer on the fuselage, power set are made of a screw, drive motors and transmission shifting mechanism, and transfer is rudder and the controlling organization that is arranged on the empennage.The shortcoming of this toy airplane is: the transfer complex structure, cause the toy airplane price higher.Again just like the Single-chip Controlling electric remote control aircraft of No. the 200320119026.5th, Chinese patent; structure comprises fuselage and is arranged at port wing on the fuselage; starboard wing; empennage; power supply; power set; remote control circuit; undercarriage; elevating mechanism; power set by about two screws and about two drive motors constitute; left-hand airscrew and left drive motors are arranged on the port wing; right-hand screw oar and right drive motors are arranged on the starboard wing; elevating mechanism is by the elevator on the empennage; steering wheel and kinematic link constitute; aircraft turns to the rotating speed difference of the right-hand screw oar that keeps left to realize; the shortcoming of this model plane or toy airplane is: respectively be mounted with screw and drive motors on the wing of the left and right sides; so the necessary rigidity of aircraft is bigger; aircraft can compare heaviness like this; another problem is that aircraft turns to level and turns to; with real aircraft turn to form different, emulation or interest are lower.
Summary of the invention
Complicated in order to overcome the existing existing structure of similar electric remote control propeller aeroplane, price is higher and relatively heavier, aircraft turns to the defective that turns to for level, the purpose of this utility model provides a kind of propeller aeroplane of improved electric remote control, can overcome the defective of prior art.
The utility model for the technical scheme that solves its technical problem and adopt is: a kind of propeller aeroplane of electric remote control, comprise fuselage and be arranged at port wing on the fuselage, starboard wing, empennage, battery, power set, remote control circuit, transfer, power set by on a drive motors that is installed in the fuselage head inboard and the driving shaft that is fixed on drive motors and the screw that is in the fuselage head outside constitute, battery is done power supply by remote control circuit and drive motors and is connected, it is characterized in that: transfer by be located at respectively on the wing of the left and right sides be upper and lower to port, be installed on the shaft axis in each port steer motor of roughly arranging in vertical direction and the impeller that turns to that is fixed on the steer motor axle and constitute, battery is done power supply by remote control circuit and steer motor and is connected.
The port wing of technique scheme and starboard wing all can be modes such as single-wing, the two-shipper wing or the multimachine wing.
The empennage of technique scheme can be modes such as single vertical fin wing, the twin vertical fin wing, many vertical fins wing or vee tail.
The power set of technique scheme can also include transmission shifting mechanism, and drive motors is done to drive by transmission shifting mechanism and screw and is connected.
The driving shaft of the drive motors of technique scheme, can be the rotating shaft of drive motors, also can be with transmission shifting mechanism that drive motors is connected on power output shaft.
The beneficial effects of the utility model: since transfer by respectively be located on the wing of the left and right sides be upper and lower to port, be installed on the steer motor that the shaft axis in each port roughly arranges in vertical direction and the impeller that turns to that is fixed on the steer motor axle constitutes, by controlling the different rotating speeds that turns to impeller on the wing of the left and right sides or turning to, aircraft just can be leaned to one side to move and be realized turning to, this turns to form similar with real aircraft, its emulation or interesting higher; Because the steer motor on the wing of the left and right sides and turn to that the impeller volume is very little just can be used, thereby aircraft can be made very lightly; Transfer of the present utility model is simple in structure, and the price of aircraft is reduced.
The utility model is described in further detail below in conjunction with drawings and Examples.
Description of drawings
Fig. 1 is the schematic perspective view of an embodiment of the utility model, omits the connection lead between each electricity consumption device among the figure.
Among the figure: 1, fuselage; 2, port wing; 3, starboard wing; 4, empennage; 5, battery; 6, power set; 7, remote control circuit; 8, drive motors; 9, driving shaft; 10, screw; 11 and 12, port; 13 and 14, steer motor; 15 and 16, turn to impeller; 17, transmission shifting mechanism.
The specific embodiment
With reference to Fig. 1, the propeller aeroplane of this electric remote control, comprise fuselage 1 and be arranged at port wing 2 on the fuselage 1, starboard wing 3, empennage 4, battery 5, power set 6, remote control circuit 7, transfer, power set 6 by on a drive motors 8 that is installed in fuselage 1 inner portion and the driving shaft 9 that is fixed on drive motors 8 and the screw 10 that is in the fuselage 1 head outside constitute, battery 5 is done power supply by remote control circuit 7 with drive motors 8 and is connected, it is characterized in that: transfer is by being located at left and right sides wing 2 respectively, on 3 be upper and lower to port 11,12, be installed on each port 11, the steer motor 13 that shaft axis in 12 is roughly arranged in vertical direction, 14 and be fixed in steer motor 13, turn to impeller 15 on 14 the axle, 16 constitute, and battery 5 is by remote control circuit 7 and steer motor 13,14 do power supply connects.
In addition, power set 6 also include transmission shifting mechanism 17, and drive motors 8 is done to drive with screw 10 by transmission shifting mechanism 17 and is connected; The driving shaft 9 of drive motors 8 is the power output shaft on the transmission shifting mechanism 17.
In the use, after remote control circuit 7 is accepted remote signal, just control battery 5 to drive motors 8 power supplies, drive motors 8 drives screw 10 rotations by transmission shifting mechanism 17, when being devoted to, aircraft just flown when aerial, when remote control circuit 7 receives turn signal, just control battery 5 to steer motor 13,14 or 13 and 14 power supplies, one of them rotation of turning to impeller 15,16 or two are rotated, and difference turns to but different rotating speeds or two rotate, at this moment aircraft will be made the action of leaning to one side, thereby realizes turning to.
Claims (3)
1, a kind of propeller aeroplane of electric remote control, comprise fuselage and be arranged at port wing on the fuselage, starboard wing, empennage, battery, power set, remote control circuit, transfer, power set by on a drive motors that is installed in the fuselage head inboard and the driving shaft that is fixed on drive motors and the screw that is in the fuselage head outside constitute, battery is done power supply by remote control circuit and drive motors and is connected, it is characterized in that: transfer by be located at respectively on the wing of the left and right sides be upper and lower to port, be installed on the shaft axis in each port steer motor of roughly arranging in vertical direction and the impeller that turns to that is fixed on the steer motor axle and constitute, battery is done power supply by remote control circuit and steer motor and is connected.
2, by the propeller aeroplane of the described electric remote control of claim 1, it is characterized in that described power set also include transmission shifting mechanism, drive motors is done to drive by transmission shifting mechanism and screw and is connected.
3, by the propeller aeroplane of claim 1 or 2 described electric remote controls, the driving shaft that it is characterized in that described drive motors be drive motors rotating shaft or with transmission shifting mechanism that drive motors is connected on power output shaft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920051645U CN201370967Y (en) | 2009-02-19 | 2009-02-19 | Electric remote control propeller-driven aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200920051645U CN201370967Y (en) | 2009-02-19 | 2009-02-19 | Electric remote control propeller-driven aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201370967Y true CN201370967Y (en) | 2009-12-30 |
Family
ID=41497046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200920051645U Expired - Lifetime CN201370967Y (en) | 2009-02-19 | 2009-02-19 | Electric remote control propeller-driven aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201370967Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105797394A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Aerial mould having strong power and lasting endurance |
| CN106267839A (en) * | 2015-05-15 | 2017-01-04 | 上海九鹰电子科技有限公司 | Propeller connector, model aerial vehicle for model aerial vehicle |
| CN106540459A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Rotor blade, rotor, aircraft and method |
| CN106540460A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Quadrotor rotor characteristic integrated test system |
-
2009
- 2009-02-19 CN CN200920051645U patent/CN201370967Y/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105797394A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Aerial mould having strong power and lasting endurance |
| CN106267839A (en) * | 2015-05-15 | 2017-01-04 | 上海九鹰电子科技有限公司 | Propeller connector, model aerial vehicle for model aerial vehicle |
| CN106540459A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Rotor blade, rotor, aircraft and method |
| CN106540460A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Quadrotor rotor characteristic integrated test system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20091230 Effective date of abandoning: 20090219 |