CN106563278A - Model airplane capable of driving rotation of multiple propellers with single power - Google Patents
Model airplane capable of driving rotation of multiple propellers with single power Download PDFInfo
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- CN106563278A CN106563278A CN201510651060.4A CN201510651060A CN106563278A CN 106563278 A CN106563278 A CN 106563278A CN 201510651060 A CN201510651060 A CN 201510651060A CN 106563278 A CN106563278 A CN 106563278A
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Abstract
The invention discloses a gear clutch system and an aircraft of the same. The structure comprises a main body framework, a tail direction control device, a landing mechanism, a source power mechanism and an integral remote control device, wherein the source power mechanism comprises a gear speed-reduction clutch mechanism which can transmit power of a power source to a front propeller and a rear propeller simultaneously. According to the invention, rotation of the two propellers or multiple propellers can be driven by one power source at the same time, so the weight of a model airplane of which the rotation of the multiple propellers is driven by the single power can be reduced greatly. In this way, maneuvering performance and endurance of the model airplane of which the rotation of the multiple propellers is driven by the single power can be enhanced.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly, the present invention relates to a kind of single-power drives the model plane of multiple propeller rotation.
Background technology
As people drive the requirement of the model plane of multiple propeller rotation to improve constantly to single-power, often require that single-power drives the model plane of multiple propeller rotation to have good flying quality, to increase the interest for manipulating the model plane that single-power drives multiple propeller rotation, the weight of the far-reaching model plane for being single-power drive multiple propeller rotation of flying quality of the model plane of multiple propeller rotation is driven to single-power, it is typically all to complete power supply by two power sources that coaxial double oar single-powers drive the model plane of multiple propeller rotation, it is also required to two sets of actuating units, this makes single-power drive the model plane of multiple propeller rotation to considerably increase weight, therefore mitigating single-power drives the weight of the model plane of multiple propeller rotation to become industry urgent problem.
The content of the invention
The technical problem to be solved is the defect and provide can mitigate the model plane own wt that single-power drives multiple propeller rotation being directed to existing for above-mentioned prior art, and the single-power that reduces cost is capable of again drives the model plane of multiple propeller rotation.
Solving the technical scheme that adopted of present invention problem is：A kind of single-power drives the model plane of multiple propeller rotation to include main body framework, it is connected caudal directions control device with main body framework rear, it is connected to support the landing mechanism of the main body framework with main body framework lower section, the driving source mechanism being arranged in the main body framework and the integrated remote control device that external control signal can be received, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, the front propeller being arranged on power transmission shaft, the rear screw shaft that is arranged on axle sleeve and by the power of described power source while passing to the The gear deceleration clutch of front propeller and rear screw shaft.
The beneficial effects of the present invention is：Single-power drives the power driving source of the model plane of multiple propeller rotation to pass to front propeller and rear screw shaft simultaneously by The gear deceleration clutch, front propeller and rear screw shaft is set to reversely rotate simultaneously, so make present invention achieves a power source drive pair oars rotation simultaneously, greatly reduces the weight and manufacturing cost of the model plane itself of single-power drive multiple propeller rotation.
The preferred implementation of the model plane of multiple propeller rotation is driven as single-power of the present invention, described The gear deceleration clutch includes the power source gear being fixed on power source output shaft, the driving gear on described axle sleeve is engaged and is fixed on the power source gear, the driving gear has planet internal ring gear, at least one planetary gear engaged with driving gear planet internal ring gear, the central gear for engaging with described planetary gear and being fixed on power transmission shaft.
Another preferred implementation of model plane of multiple propeller rotation is driven as single-power of the present invention, it also includes dynamic balancer, described dynamic balancer includes gimbal lever's union joint, the gimbal lever and is arranged at the balance weight at gimbal lever two ends, described dynamic balancer is arranged on the upper end of power transmission shaft by gimbal lever's union joint, the dynamic balancer single-power balances its whole body when driving the model plane flight of multiple propeller rotation, makes single-power drive the model plane of multiple propeller rotation more can safety and steady flight.
The model plane further embodiment of multiple propeller rotation is driven as single-power of the present invention, it also includes steering assembly, described steering assembly includes the pitch being arranged on axle sleeve, steering wheel, the connecting rod of connection steering wheel and pitch, pitch leading truck and is connected the connecting rod of the pitch leading truck and pitch, and the steering assembly efficiently controls single-power and drives the model plane that multiple propeller rotates to flexibly turn to.
Below in conjunction with drawings and Examples, technical scheme is described in further detail.
Description of the drawings
Fig. 1 drives the explosive view of the model plane of multiple propeller rotation for the single-power of a preferred embodiment of the present invention.
Specific embodiment
With reference now to Description of Drawings the preferred embodiments of the present invention,.
With reference to Fig. 1, single-power of the present invention drives the landing mechanism 3 that the caudal directions control device 2 that the model plane of multiple propeller rotation include that main body framework 1 and main body framework rear connect and main body framework bottom be connected to support the main body framework, the driving source mechanism 4 being arranged in the main body framework 1, can receive external control signal integrated remote control device 5 and provide the battery 6 of electric energy for consuming parts in main body framework.
Described driving source mechanism 4 includes power source, axle sleeve, the power transmission shaft through the axle sleeve, front propeller, rear screw shaft, power source gear, driving gear, planetary gear, central gear.Front propeller is arranged on power transmission shaft by front vane folder, rear screw shaft is arranged on axle sleeve by rear blade folder, power source gear is installed on described power source output shaft, described driving gear is engaged with power source gear and is fixed on described axle sleeve, driving gear has planet internal ring gear, there are three planetary gears engaged with driving gear planet internal ring gear, described central gear is engaged and is fixed on power transmission shaft with three planetary gears, central gear is provided with planet carrier, and three planetary gear bearings are mutually in 120 degree of positioning planet carriers.Certainly, in other embodiments planetary gear can be one or more.Power transmission shaft lower end is positioned on the bearing block of main body framework by bearing, and axle sleeve upper end is provided with bearing block, and the bearing on power transmission shaft is arranged in bearing block.Power source drive is arranged on the power source gear on power source output shaft，The driving gear that drive is engaged with power source gear，The rotation of driving gear rotates axle sleeve，So that the rear screw shaft rotation being fixed on axle sleeve，And drive three planetary gears engaged with driving gear planet internal ring gear to rotate，Three planetary gears rotarily drive central gear rotation，Central gear rotation rotates power transmission shaft，So that the front propeller being fixed on power transmission shaft is rotated with the direction contrary with rear screw shaft，It has been achieved in that a power source drives front propeller and rear screw shaft while rotating in the opposite direction simultaneously by gear drive，Eliminate a power source and its actuating device，Greatly reduce the weight that single-power drives the model plane itself of multiple propeller rotation，The flying quality of model plane of multiple propeller rotation and cost-effective is driven so as to improve single-power.
The single-power drives the model plane of multiple propeller rotation also to include dynamic balancer; the dynamic balancer includes gimbal lever's union joint, the gimbal lever and is arranged at the balance weight at gimbal lever two ends; the gimbal lever is arranged on the upper end of power transmission shaft by gimbal lever's union joint; the dynamic balancer make single-power drive multiple propeller rotation model plane flight when balance its whole body, make single-power drive multiple propeller rotation model plane more can safety and steady flight.
Described single-power drives the model plane of multiple propeller rotation also to include steering assembly; the steering assembly includes the pitch being arranged on axle sleeve, steering wheel, the connecting rod of connection steering wheel and pitch, pitch leading truck and is connected the connecting rod of the pitch leading truck and pitch, and the steering assembly efficiently controls model plane and flexibly turns to.
The caudal directions control device includes the tailstock being connected with main body framework, the tail propeller being arranged on tailstock and the tail power source for driving the tail propeller.
Finally should be noted that; above example is only to illustrate technical scheme rather than limiting the scope of the invention; although being explained in detail to the present invention with reference to preferred embodiment; but it will be understood by those within the art that; technical scheme can be modified or equivalent, without deviating from the spirit and scope of technical solution of the present invention.
Claims (7)
1. a kind of single-power drives the model plane of multiple propeller rotation,
It is characterized in that：Including main body framework, caudal directions control device, landing mechanism, driving source mechanism and integrated remote control device, the caudal directions control device is connected to the main body framework rear portion, the landing mechanism is connected to below the main body framework, the driving source mechanism and integrated remote control device are arranged on inside the main body framework, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, the front propeller being arranged on power transmission shaft and the rear screw shaft being arranged on axle sleeve, and the power of described power source is passed to into the The gear deceleration clutch of front propeller and rear screw shaft simultaneously.
2. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：Described The gear deceleration clutch includes the power source gear being fixed on power source output shaft, the driving gear on described axle sleeve is engaged and is fixed on the power source gear, the driving gear has planet internal ring gear, at least one planetary gear engaged with driving gear planet internal ring gear, the central gear for engaging with described planetary gear and being fixed on power transmission shaft.
3. single-power as claimed in claim 2 drives the model plane of multiple propeller rotation, it is characterised in that：Planet carrier is fixed with described central gear, described planetary gear is positioned on the planet carrier.
4. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：It also includes dynamic balancer, and described dynamic balancer includes gimbal lever's union joint, the gimbal lever and is arranged at the balance weight at gimbal lever two ends, and described dynamic balancer is arranged on the upper end of power transmission shaft by gimbal lever's union joint.
5. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：It also includes steering assembly, and described steering assembly includes the pitch being arranged on axle sleeve, steering wheel, the connecting rod of connection steering wheel and pitch, pitch leading truck and is connected the connecting rod of the pitch leading truck and pitch.
6. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：Front propeller folder is additionally provided with described power transmission shaft, described front propeller is clamping on described power transmission shaft by the front propeller, rear screw shaft folder is provided with described axle sleeve, described rear screw shaft is clamping on axle sleeve by the rear screw shaft.
7. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：Described hollow pipe top is provided with bearing block, and described power transmission shaft top is additionally provided with the bearing being placed in hollow pipe upper axis bearing, and lower end is provided with the positioning bearing being placed in main body framework bearing block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510651060.4A CN106563278A (en) | 2015-10-10 | 2015-10-10 | Model airplane capable of driving rotation of multiple propellers with single power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510651060.4A CN106563278A (en) | 2015-10-10 | 2015-10-10 | Model airplane capable of driving rotation of multiple propellers with single power |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106563278A true CN106563278A (en) | 2017-04-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510651060.4A Pending CN106563278A (en) | 2015-10-10 | 2015-10-10 | Model airplane capable of driving rotation of multiple propellers with single power |
Country Status (1)
| Country | Link |
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| CN (1) | CN106563278A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606873A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Planetary gear deceleration system model airplane |
| CN110047355A (en) * | 2019-05-09 | 2019-07-23 | 刘沁沁 | A kind of rotation bottom of the model aircraft of school science teaching |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03268780A (en) * | 1990-03-20 | 1991-11-29 | Takara Co Ltd | Floating body |
| JP2000167261A (en) * | 1998-12-02 | 2000-06-20 | Marusho:Kk | Rotation transmission airplane toy for multiple jet fan |
| CN204050974U (en) * | 2014-06-26 | 2014-12-31 | 许美兰 | There is the remote control distributor toy of multiple power set |
| CN204355275U (en) * | 2014-08-29 | 2015-05-27 | 深圳市艾特航空科技股份有限公司 | There is the aircraft of safe propulsion system |
| CN106492477A (en) * | 2015-09-03 | 2017-03-15 | 马铿杰 | Single-power drives the model plane of multiple propeller rotation |
-
2015
- 2015-10-10 CN CN201510651060.4A patent/CN106563278A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03268780A (en) * | 1990-03-20 | 1991-11-29 | Takara Co Ltd | Floating body |
| JP2000167261A (en) * | 1998-12-02 | 2000-06-20 | Marusho:Kk | Rotation transmission airplane toy for multiple jet fan |
| CN204050974U (en) * | 2014-06-26 | 2014-12-31 | 许美兰 | There is the remote control distributor toy of multiple power set |
| CN204355275U (en) * | 2014-08-29 | 2015-05-27 | 深圳市艾特航空科技股份有限公司 | There is the aircraft of safe propulsion system |
| CN106492477A (en) * | 2015-09-03 | 2017-03-15 | 马铿杰 | Single-power drives the model plane of multiple propeller rotation |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606873A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Planetary gear deceleration system model airplane |
| CN110047355A (en) * | 2019-05-09 | 2019-07-23 | 刘沁沁 | A kind of rotation bottom of the model aircraft of school science teaching |
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Application publication date: 20170419 |
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