CN106621375A - Model airplane provided with swash plate controllers - Google Patents
Model airplane provided with swash plate controllers Download PDFInfo
- Publication number
- CN106621375A CN106621375A CN201510732626.6A CN201510732626A CN106621375A CN 106621375 A CN106621375 A CN 106621375A CN 201510732626 A CN201510732626 A CN 201510732626A CN 106621375 A CN106621375 A CN 106621375A
- Authority
- CN
- China
- Prior art keywords
- gear
- pitch
- model airplane
- fixed
- disk controller
- Prior art date
- 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.)
- Withdrawn
Links
Landscapes
- Toys (AREA)
Abstract
The invention discloses a model airplane provided with swash plate controllers. The model airplane comprises a fuselage main body, a tail direction control device, a source power mechanism and an integrated remote control direction, wherein the source power mechanism comprises a gear reduction clutch mechanism which is used for simultaneously transmitting power of a power source to a first three-propeller rotating component and a second three-propeller rotating component. According to the model airplane provided with the double three-propeller components, the two independent three-propeller rotating components are arranged at two ends of a fuselage of the model airplane; the two three-propeller rotating components are driven by a same motor and are capable of simultaneously rotating; the two three-propeller rotating components are provided with independent steering engines and the swash plate controllers, and the two three-propeller rotating components can be mutually matched, so that the purpose of controlling the stable flight of the model airplane is achieved; in addition, the model airplane provided with the double three-propeller components is different from a conventional single linear two-propeller rotating mechanism in structural setting; the entire balance of the fuselage of the model airplane can be easily controlled, so that the model airplane is especially suitable for green hands; and moreover, the model airplane, since three blades are distributed by 120 degrees, is strong in anti-wind capacity.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly, the present invention relates to a kind of with the model plane for inclining disk controller.
Background technology
As people improve constantly to the requirement with the model plane for inclining disk controller, often require that and there is good flying quality with the model plane for inclining disk controller, the interest with the model plane for inclining disk controller is manipulated to increase, far-reaching to the flying quality with the model plane for inclining disk controller is the weight of the model plane with inclination disk controller, there are coaxial double oars the model plane for inclining disk controller typically all to complete power supply by two power sources, it is also required to two sets of actuating units, this makes that there are the model plane for inclining disk controller to considerably increase weight, therefore mitigating the weight with the model plane for inclining disk controller becomes industry urgent problem.
The content of the invention
The technical problem to be solved is the defect and can mitigating with the model plane own wt for inclining disk controller for providing being directed to existing for above-mentioned prior art, and the model plane with inclination disk controller of reduces cost are capable of again.
Solving the technical scheme that adopted of present invention problem is：A kind of model plane with inclination disk controller, including fuselage main body, caudal directions control device and driving source mechanism, the caudal directions control device is connected to the fuselage main body rear portion, the landing mechanism is connected to below the fuselage main body, the driving source mechanism and integrated remote control device are arranged on inside the fuselage main body, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, the one or three oar rotary components being arranged on power transmission shaft and the two or three oar rotary components being arranged on axle sleeve, and the power of described power source is passed into the The gear deceleration clutch of the one or three oar rotary components and the two or three oar rotary components simultaneously, three described oar rotary components include main shaft, blade, blade is pressed from both sides, the headstock, pitch, pull bar and steering wheel, the headstock is fixed on the top of main shaft, blade folder is fixed on around the headstock, blade is fixed on blade folder, pitch is fixed on the main shaft below the headstock, steering wheel is fixed on main frame, blade pressed from both sides and all connected by pull bar and pitch between and between pitch and steering wheel.
There is the preferred embodiment of the model plane for inclining disk controller as 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.
There is another preferred embodiment of model plane for inclining disk controller as the present invention, it 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 arranged on the upper end of power transmission shaft by balancing pole connector, the dynamic balancer balances its whole body when having the model plane flight for inclining disk controller, and making more can safety and steady flight with the model plane for inclining disk controller.
There is the model plane further embodiment for inclining disk controller as 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 the model plane with inclination disk controller and flexibly turns to.
The beneficial effects of the present invention is：The dual-three-propeller model airplane of the present invention adopts two three independent oar rotary components, it is separately positioned on the two ends of model plane fuselage, two or three oar rotary components are driven by same motor, can synchronous rotary, two or three oar rotary components each independently possess steering wheel and pitch control, can cooperate between it and reach the purpose of control model plane smooth flight, the dual-three-propeller model airplane of the other present invention, structure setting is different from traditional single oar rotating mechanism of orthoscopic two, model plane fuselage whole machine balancing is easily controlled, especially suitable new hand, and three blades are in 120 degree of arrangements, wind loading rating is also very strong, whole model plane structure is novel, fuselage cover is set to simulation shell, fan can be allowed also to have more rich reverie space while flight is played.
Below in conjunction with drawings and Examples, technical scheme is described in further detail.
Description of the drawings
Fig. 1 is the explosive view with the model plane for inclining disk controller 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, the present invention has the landing mechanism 3 that the caudal directions control device 2 that the model plane for inclining disk controller include that fuselage main body 1 and fuselage main body rear connect and fuselage main body bottom be connected to support the fuselage main body, the driving source mechanism 4 being arranged in the fuselage main body 1, can receive external control signal integrated remote control device 5 and provide the battery 6 of electric energy for consuming parts in fuselage main body.
Described driving source mechanism 4 includes power source, axle sleeve, the power transmission shaft through the axle sleeve, the one or three oar rotary components, the two or three oar rotary components, power source gear, driving gear, planetary gear, central gear.One or three oar rotary components are arranged on power transmission shaft by front vane folder, two or three oar rotary components are 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, 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 fuselage main body 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 two or the three oar rotary components 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 one or three oar rotary components being fixed on power transmission shaft are rotated with the direction contrary with the two or three oar rotary components, it has been achieved in that a power source drives the one or three oar rotary components and the two or three oar rotary components while rotating in the opposite direction simultaneously by gear drive, eliminate a power source and its transmission device, greatly reduce the weight with the model plane itself for inclining disk controller, so as to improve with the flying quality of model plane for inclining disk controller and cost-effective.
It is described also to include dynamic balancer with the model plane for inclining disk controller; the dynamic balancer includes balancing pole connector, balancing pole and is arranged at the balance weight at balancing pole two ends; balancing pole is arranged on the upper end of power transmission shaft by balancing pole connector; the dynamic balancer makes to balance its whole body when having the model plane flight for inclining disk controller, and making more can safety and steady flight with the model plane for inclining disk controller.
Described also includes steering assembly with the model plane for inclining disk controller; 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 fuselage main body, the tail screw being arranged on tailstock and the tail power source for driving the tail screw.
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 (4)
1. a kind of with the model plane for inclining disk controller, it is characterised in that：Including fuselage main body, caudal directions control device and driving source mechanism, the caudal directions control device is connected to the fuselage main body rear portion, the driving source mechanism and integrated remote control device are arranged on inside the fuselage main body, described driving source mechanism includes power source, axle sleeve, through the power transmission shaft of the axle sleeve, the one or three oar rotary components being arranged on power transmission shaft and the two or three oar rotary components being arranged on axle sleeve, and the power of described power source is passed into the The gear deceleration clutch of the one or three oar rotary components and the two or three oar rotary components simultaneously, three described oar rotary components include main shaft, blade, blade is pressed from both sides, the headstock, pitch, pull bar and steering wheel, the headstock is fixed on the top of main shaft, blade folder is fixed on around the headstock, blade is fixed on blade folder, pitch is fixed on the main shaft below the headstock, steering wheel is fixed on main frame, blade pressed from both sides and all connected by pull bar and pitch between and between pitch and steering wheel.
It is 2. as claimed in claim 1 that there are the model plane for inclining disk controller, 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；Planet carrier is fixed with described central gear, described planetary gear is positioned on the planet carrier.
It is 3. as claimed in claim 1 that there are the model plane for inclining disk controller, it is characterised in that：It also includes dynamic balancer, and described dynamic balancer includes balancing pole connector, balancing pole and is 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.
It is 4. as claimed in claim 1 that there are the model plane for inclining disk controller, 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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510732626.6A CN106621375A (en) | 2015-10-29 | 2015-10-29 | Model airplane provided with swash plate controllers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510732626.6A CN106621375A (en) | 2015-10-29 | 2015-10-29 | Model airplane provided with swash plate controllers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106621375A true CN106621375A (en) | 2017-05-10 |
Family
ID=58809713
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510732626.6A Withdrawn CN106621375A (en) | 2015-10-29 | 2015-10-29 | Model airplane provided with swash plate controllers |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106621375A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4087934A (en) * | 1977-01-10 | 1978-05-09 | Gibson Thomas P | Glider |
| CN201175582Y (en) * | 2008-01-07 | 2009-01-07 | 罗之洪 | Model aircraft |
| CN101757792A (en) * | 2009-12-24 | 2010-06-30 | 罗之洪 | Dual-three-propeller model airplane |
-
2015
- 2015-10-29 CN CN201510732626.6A patent/CN106621375A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4087934A (en) * | 1977-01-10 | 1978-05-09 | Gibson Thomas P | Glider |
| CN201175582Y (en) * | 2008-01-07 | 2009-01-07 | 罗之洪 | Model aircraft |
| CN101757792A (en) * | 2009-12-24 | 2010-06-30 | 罗之洪 | Dual-three-propeller model airplane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104760696B (en) | A kind of multi-rotor aerocraft | |
| EP2062627B1 (en) | A model helicopter | |
| CN106492477A (en) | Single-power drives the model plane of multiple propeller rotation | |
| CN104691753A (en) | Oil-relay multi-rotor helicopter driving system | |
| CN106628154A (en) | Multiple-rotor-wing unmanned aerial vehicle with double rotor wing systems | |
| CN101177167A (en) | Power-driven system of aircraft | |
| CN106741904A (en) | A kind of compound unmanned vehicle | |
| CN201175582Y (en) | Model aircraft | |
| CN106474745A (en) | There is the flight instruments of Remote The gear deceleration clutch system | |
| CN207466966U (en) | A kind of dynamic displacement quadrotor unmanned plane of oil | |
| CN107757904A (en) | A kind of dynamic rotor wing unmanned aerial vehicle of displacement four of oil | |
| CN106466528A (en) | Rotor blade, rotor, aircraft and method | |
| CN204121761U (en) | There is multiple screw flying toy | |
| CN106621375A (en) | Model airplane provided with swash plate controllers | |
| CN201139953Y (en) | Model aerial vehicle | |
| CN106563278A (en) | Model airplane capable of driving rotation of multiple propellers with single power | |
| CN106492480A (en) | Gear clutch system and its aircraft | |
| CN106606883A (en) | A model airplane with a multi-propeller propulsion system | |
| CN107187593A (en) | A kind of multiple degrees of freedom unmanned plane with twin rotor system | |
| CN106606882A (en) | Composite propeller flight system | |
| CN108657449B (en) | Power device of double-rotor aircraft | |
| CN106563275A (en) | Single-power driven multi-propeller rotating model airplane | |
| CN106563269A (en) | Model airplane gear clutch system | |
| CN106552433A (en) | Intelligent model plane | |
| CN106606873A (en) | Planetary gear deceleration system model airplane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170510 |
|
| WW01 | Invention patent application withdrawn after publication |