CN106492477A - Single-power drives the model plane of multiple propeller rotation - Google Patents
Single-power drives the model plane of multiple propeller rotation Download PDFInfo
- Publication number
- CN106492477A CN106492477A CN201510559980.3A CN201510559980A CN106492477A CN 106492477 A CN106492477 A CN 106492477A CN 201510559980 A CN201510559980 A CN 201510559980A CN 106492477 A CN106492477 A CN 106492477A
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- power
- gear
- model plane
- drives
- propeller rotation
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Abstract
Single-power drives the model plane of multiple propeller rotation, a kind of gear clutch system of the present invention and its aircraft, including main body framework, caudal directions control device, landing mechanism, driving source mechanism and integrated remote control device, include the power of described power source in described driving source mechanism while passing to the The gear deceleration clutch of front propeller and rear screw shaft；Present invention achieves the power source double oars of drive or a rotation of many oars simultaneously, greatly reduces the weight that single-power drives the model plane itself of multiple propeller rotation, so as to improve the mobility and endurance of the model plane of single-power drive multiple propeller rotation.
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 that there is 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 the flying quality of the model plane for driving multiple propeller to rotate 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.
Content of the invention
The technical problem to be solved be for the defect existing for above-mentioned prior art and provide can mitigate single-power drive multiple propeller rotation model plane own wt, be capable of again reduces cost single-power drive multiple propeller rotation model plane.
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, with the landing mechanism for being connected to support the main body framework below main body framework, 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 are made while reversely rotating, so make present invention achieves a power source is while the double oars rotations of drive, greatly reduce the weight and manufacturing cost of the model plane itself of single-power drive multiple propeller rotation.
The preferred embodiment 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 embodiment of the model plane of multiple propeller rotation is driven as single-power of the present invention, which also includes dynamic balancer, described dynamic balancer includes balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends, described dynamic balancer is by balancing pole connector installed in the upper end of power transmission shaft, the dynamic balancer single-power balances its whole body when driving the model plane flight of multiple propeller rotation, and the model plane for rotating single-power drive multiple propeller more can safety and steady flight.
As the model plane further embodiment that single-power of the present invention drives multiple propeller rotation, which also includes steering assembly, described steering assembly includes the connecting rod of pitch on axle sleeve, steering wheel, 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
Explosive views of the Fig. 1 for the model plane of the single-power drive multiple propeller rotation 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 model plane of multiple propeller rotation to include that the caudal directions control device 2 of main body framework 1 and the connection of main body framework rear and main body framework bottom are connected to support the landing mechanism 3 of 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 in main body framework for consuming parts.
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 by front vane folder on power transmission shaft, rear screw shaft is by rear blade folder on axle sleeve, 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 with three planetary gears and is fixed on power transmission shaft, central gear is provided with planet carrier, and three planetary gear bearings are mutually in 120 degree of positioning planet carriers.Certainly, planetary gear can be one or more in other embodiments.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 in bearing block.Power source gear of the power source drive on power source output shaft，Drive the driving gear 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 the three planetary gear rotations that engages with driving gear planet internal ring gear，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，A power source has been achieved in that by gear drive while front propeller and rear screw shaft is driven while rotating in the opposite direction，Eliminate a power source and its transmission 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 balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends; balancing pole is by balancing pole connector installed in the upper end of power transmission shaft; the dynamic balancer makes to balance its whole body during the model plane flight of single-power drive multiple propeller rotation, and the model plane for rotating single-power drive multiple propeller 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 connecting rod of pitch on axle sleeve, steering wheel, 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 screw being arranged on tailstock and the tail power source for driving the tail screw.
Last be should be noted that; above example is only in order to illustrating 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 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 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, and 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：Which also includes that dynamic balancer, described dynamic balancer include balancing pole connector, balancing pole and be arranged at the balance weight at balancing pole two ends, and described dynamic balancer is arranged on the upper end of power transmission shaft by balancing pole connector.
5. single-power as claimed in claim 1 drives the model plane of multiple propeller rotation, it is characterised in that：Which also includes steering assembly, and described steering assembly includes the connecting rod of pitch on axle sleeve, steering wheel, 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 being additionally provided with described power transmission shaft, described front propeller is clamping on described power transmission shaft by the front propeller, being provided with rear screw shaft folder on described axle sleeve, described rear screw shaft is clamping on the 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 |
|---|---|---|---|
| CN201510559980.3A CN106492477A (en) | 2015-09-03 | 2015-09-03 | Single-power drives the model plane of multiple propeller rotation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510559980.3A CN106492477A (en) | 2015-09-03 | 2015-09-03 | Single-power drives the model plane of multiple propeller rotation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106492477A true CN106492477A (en) | 2017-03-15 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510559980.3A Pending CN106492477A (en) | 2015-09-03 | 2015-09-03 | Single-power drives the model plane of multiple propeller rotation |
Country Status (1)
| Country | Link |
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| CN (1) | CN106492477A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106552425A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Aerial device with multiple propulsion systems |
| CN106552433A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Intelligent model plane |
| CN106563275A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Single-power driven multi-propeller rotating model airplane |
| CN106563278A (en) * | 2015-10-10 | 2017-04-19 | 马铿钧 | Model airplane capable of driving rotation of multiple propellers with single power |
| CN106606873A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Planetary gear deceleration system model airplane |
| CN112401902A (en) * | 2020-12-04 | 2021-02-26 | 山东大学 | Electrocardio identity recognition method and system based on neural network time-frequency analysis combination |
-
2015
- 2015-09-03 CN CN201510559980.3A patent/CN106492477A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106552425A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Aerial device with multiple propulsion systems |
| CN106552433A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Intelligent model plane |
| CN106563275A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | Single-power driven multi-propeller rotating model airplane |
| CN106563278A (en) * | 2015-10-10 | 2017-04-19 | 马铿钧 | Model airplane capable of driving rotation of multiple propellers with single power |
| CN106606873A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | Planetary gear deceleration system model airplane |
| CN112401902A (en) * | 2020-12-04 | 2021-02-26 | 山东大学 | Electrocardio identity recognition method and system based on neural network time-frequency analysis combination |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170315 |