CN106563273A - High-altitude flight toy - Google Patents
High-altitude flight toy Download PDFInfo
- Publication number
- CN106563273A CN106563273A CN201510651121.7A CN201510651121A CN106563273A CN 106563273 A CN106563273 A CN 106563273A CN 201510651121 A CN201510651121 A CN 201510651121A CN 106563273 A CN106563273 A CN 106563273A
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- China
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- level
- gear
- propeller
- altitude flight
- swash plate
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Abstract
The invention provides a high-altitude flight toy. The high-altitude flight toy includes a main frame, a tail wing, a landing device, a power supply mechanism, and a remote receiver; and the power supply mechanism includes a belt gear reducing driving mechanism which can transmit power of a first motor to a first propeller, a second propeller and a tail propeller. According to the high-altitude flight toy, the first propeller, the second propeller and a tail propeller can be driven to rotate by only one first motor, two power motors can be avoided, the weight of the high-altitude flight toy can be decreased, and then the maneuvering performance of the high-altitude flight toy can be improved.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly, the present invention relates to a kind of high-altitude flight toy.
Background technology
As requirement of the people to high-altitude flight toy is improved constantly, often require that high-altitude flight toy has good flying quality, to increase the interest for manipulating high-altitude flight toy, far-reaching to the flying quality of high-altitude flight toy is the weight of high-altitude flight toy, double oar high-altitude flight toys are typically all to complete power supply by two first motors, it is also required to two sets of each independent actuating units, simultaneously tail propeller is also required to an independent motor to drive, this makes high-altitude flight toy considerably increase weight, therefore in order to mitigate the weight of high-altitude flight toy, need to provide a kind of high-altitude flight toy of mechanism section parts of omission prior art high and medium flying toy offer power to mitigate whole high-altitude flight toy weight.
The content of the invention
The technical problem to be solved is provide can mitigate model plane own wt and reduces cost for the defect existing for above-mentioned prior art, and the high-altitude flight toy of model plane mobility can be improved again.
Solving the technical scheme that adopted of present invention problem is：A kind of high-altitude flight toy, including main body frame, with the back-connected empennage of main body frame, it is connected to support the landing gear of the main body frame with main body frame bottom, the mechanism of the offer power being arranged on the main body frame and empennage and the remote receiver of external control signal can be received, the mechanism of described offer power includes the first motor, power transmission shaft, through the rotary shaft of the power transmission shaft, the first propeller being arranged in rotary shaft, the second propeller being arranged on power transmission shaft and the tail propeller being arranged on tailing axle, and the power of the first described motor is passed to into the first propeller simultaneously, the belt gear reduction gearing mechanism of the second propeller and tail propeller.
The beneficial effects of the present invention is：Present invention achieves first motor drives the first propeller, the second propeller and tail propeller rotational simultaneously, significantly reduce the high-altitude flight toy weight of itself, so as to improve the mobility of high-altitude flight toy, while also reducing the manufacturing cost of high-altitude flight toy.
As the preferred implementation of high-altitude flight toy of the present invention, described belt gear reduction gearing mechanism includes the motor gear being fixed on motor output shaft, the one-level driven gear engaged with the motor gear, the one-level band gear coaxial with one-level driven gear, two grades of driven gears being connected with the engagement of one-level driven gear and with described power transmission shaft one end, the two grade band gears coaxial with two grades of driven gears, it is fixed on three-level band gear in rotary shaft, and it is connected level Four with tailing axle with gear, one-level band gear is connected by level synchronization transporter with three-level band gear, two grades of band gears are connected by secondary synchronization transporter with level Four band gear.
As another preferred implementation of high-altitude flight toy of the present invention, the described two grades both sides for being respectively placed in two grades of driven gears with gear with gear and three-level.
As another preferred implementation of high-altitude flight toy of the present invention, described belt gear reduction gearing mechanism also includes being arranged at described one-level pulley cover of the one-level with gear side, it is arranged at two grades of described with gear side two grades of pulley covers, it is arranged at described three-level pulley cover of the three-level with gear side, it is arranged at described level Four pulley cover of the level Four with gear side, described one-level pulley cover, three-level pulley cover are used to prevent level synchronization transporter from slipping, and described two grades of pulley covers, level Four pulley cover are used to prevent secondary synchronization transporter from slipping.
As another preferred implementation of high-altitude flight toy of the present invention, described belt gear reduction gearing mechanism is additionally provided with makes two grades of roller devices with the tensioning of the secondary synchronization transporter with gear of gear and level Four of connection, the roller devices make at any time secondary synchronization transporter be stretched on two grades of band gears and level Four band gear, to prevent synchronous belt from sliding on two grades of band gears and level Four band gear.
As another preferred implementation of high-altitude flight toy of the present invention, it also includes front level controller and is arranged at the rear level controller of the empennage, described front level controller includes the swash plate that leans forward being arranged on power transmission shaft, front steering wheel, connect the front rod of front steering wheel and the swash plate that leans forward, leaning forward on main body frame and connects lean forward swash plate leading truck and the master link of swash plate of leaning forward at swash plate leading truck, described rear level controller includes the hypsokinesis swash plate being arranged on tailing axle, steering wheel afterwards, the slave connecting rod of steering wheel and hypsokinesis swash plate after connection, hypsokinesis swash plate leading truck on empennage frame and connect the secondary connecting rod of the hypsokinesis swash plate leading truck and hypsokinesis swash plate, it is main, rear level controller more neatly realizes the steering of high-altitude flight toy.
As another preferred implementation of high-altitude flight toy 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 rotary shaft by gimbal lever's union joint, balance its whole body during the dynamic balancer high-altitude flight toy flying, make high-altitude flight toy more can safety and steady flight.
Below in conjunction with drawings and Examples, technical scheme is described in further detail.
Description of the drawings
Fig. 1 is the structural representation of the high-altitude flight toy 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, high-altitude flight toy of the present invention includes that main body frame 1 and the back-connected empennage 2 of main body frame and main body frame bottom are connected to support the landing gear 3 of the main body frame, the mechanism 4 of the offer power being arranged on the main body frame 1 and empennage 2, can receive on main body frame 1 remote receiver 5 of external control signal.
The mechanism 4 of described offer power includes the first motor、Power transmission shaft、Through the rotary shaft of the power transmission shaft、The first propeller installed on the rotary shaft and the second propeller being arranged on by back blades folder on power transmission shaft are pressed from both sides by primary blades，First motor is arranged on main body frame 1，Motor gear is installed on its output shaft，The one-level driven gear engaged with the motor gear，One-level driven gear is positioned on the bearing block of main body frame 1 by bearing，The one-level band gear coaxial with one-level driven gear，Side of the one-level with gear is additionally provided with one-level pulley cover，Two grades of driven gears being connected with the engagement of one-level driven gear and with described power transmission shaft one end，Two grades of driven gears are positioned on the bearing block of main body frame 1 by bearing，The two grade band gears coaxial with two grades of driven gears，Two grades of sides with gear are additionally provided with two grades of pulley covers，Three-level band gear is fixed in rotary shaft,Rotary shaft lower end is positioned on the bearing block of main body frame 1 by bearing，Three-level band gear side is additionally provided with bearing three-level pulley cover，The level Four band gear side being connected with tailing axle is additionally provided with level Four pulley cover,One-level band gear is connected by level synchronization transporter with three-level band gear，Two grades of band gears are connected by secondary synchronization transporter with level Four band gear，Tail propeller is arranged on tailing axle by caudal lobe piece folder，Tailing axle is positioned on the bearing block of tailstock by bearing，One-level pulley cover and bearing three-level pulley cover are used to prevent the slippage of the first belt pulley，Two grades of pulley covers and level Four pulley cover are used to prevent the slippage of the second belt pulley；Both sides near the second belt pulley on main body frame 1 are additionally provided with the adjustable roller devices for making belt pulley keep tensioning state at any time in position, and certainly in other embodiments roller devices also can be replaced with other devices.
The first described Motor drive is arranged on the rotation of the motor gear in its drive shaft, motor gear rotation rotates the one-level driven gear for engaging, so as to drive engage with one-level driven gear two grades of driven gear rotations, two grades of driven gear rotations rotate the power transmission shaft being fixed thereon, so as to drive the second propeller for being fixed on power transmission shaft to rotate;The rotation of one-level driven gear rotates the one-level band gear being coaxial therewith, and be rotated through first belt pulley of the one-level with gear passes to three-level band gear, and three-level rotarily drives rotary shaft rotation with gear, and rotary shaft rotarily drives the rotation of the first propeller being fixed thereon；Two grades of driven gear rotations make two grades of rotations with gear being coaxial therewith, two grades of second belt pulleys that are rotated through with gear pass on level Four band gear, the rotation that rotarily drive the tail propeller that with tail propeller 32 be fixed on tailing axle on of the level Four with gear.It has been achieved in that first motor drives the rotation of the first propeller, the second propeller and tail propeller simultaneously, has eliminated two motors, significantly reduced the weight of model plane itself, the flying quality of model plane has been improve, while also saving manufacturing cost.
Described high-altitude flight toy also includes front level controller and is arranged at the rear level controller of the empennage, described front level controller includes the swash plate that leans forward being arranged on power transmission shaft, front steering wheel, connect the front rod of front steering wheel and the swash plate that leans forward, lean forward and swash plate leading truck and connect lean forward swash plate leading truck and the master link of swash plate of leaning forward, described rear level controller includes the hypsokinesis swash plate being arranged on tailing axle, steering wheel afterwards, the slave connecting rod of steering wheel and hypsokinesis swash plate after connection, hypsokinesis swash plate leading truck and connect the secondary connecting rod of the hypsokinesis swash plate leading truck and hypsokinesis swash plate, the steering of the front level controller and rear level controller co- controlling high-altitude flight toy, make the steering of high-altitude flight toy more flexible.
The high-altitude flight toy also includes 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 rotary shaft by gimbal lever's union joint, the dynamic balancer makes to balance its whole body during high-altitude flight toy flying, make high-altitude flight toy more can safety and steady flight.
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 high-altitude flight toy, it is characterised in that：Including main body frame、Empennage、Landing gear、Mechanism and the remote receiver of the offer power of the main body frame are provided，The mechanism of described offer power includes the first motor、Power transmission shaft、Through the rotary shaft of the power transmission shaft、The first propeller being arranged in rotary shaft、The second propeller being arranged on power transmission shaft and the tail propeller being arranged on tailing axle，The mechanism of described offer power is also included the power of the first described motor while passing to the first propeller、The belt gear reduction gearing mechanism of the second propeller and tail propeller，Described belt gear reduction gearing mechanism includes the motor gear being fixed on motor output shaft，The one-level driven gear engaged with the motor gear，The one-level band gear coaxial with one-level driven gear，Two grades of driven gears being connected with the engagement of one-level driven gear and with described power transmission shaft one end，The two grade band gears coaxial with two grades of driven gears，The three-level band gear being fixed in rotary shaft，The level Four band gear being connected with tailing axle,One-level band gear is connected by level synchronization transporter with three-level band gear，Two grades of band gears are connected by secondary synchronization transporter with level Four band gear.
2. high-altitude flight toy as claimed in claim 1, it is characterised in that：Described belt gear reduction gearing mechanism also includes being arranged at described one-level pulley cover of the one-level with gear side, it is arranged at two grades of described with gear side two grades of pulley covers, described three-level pulley cover of the three-level with gear side is arranged at, described level Four pulley cover of the level Four with gear side is arranged at.
3. high-altitude flight toy as claimed in claim 2, it is characterised in that：Described belt gear reduction gearing mechanism is additionally provided with makes two grades of devices with the tensioning of the synchronous belt with gear of gear and level Four of connection.
4. high-altitude flight toy as claimed in claim 3, it is characterised in that：The device of the synchronous belt tensioning is roller.
5. high-altitude flight toy as claimed in claim 1, 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 rotary shaft by gimbal lever's union joint.
6. high-altitude flight toy as claimed in claim 1, it is characterised in that：It also includes front level controller and is arranged at the rear level controller of the empennage, described front level controller includes the front rod of steering wheel and the swash plate that leans forward before the swash plate that leans forward being arranged on power transmission shaft, front steering wheel, connection, leaning forward swash plate leading truck and is connected the master link of lean forward swash plate leading truck and the swash plate that leans forward, and described rear level controller includes the connecting rod of steering wheel and hypsokinesis swash plate, hypsokinesis swash plate leading truck after the hypsokinesis swash plate being arranged on tailing axle, rear steering wheel, connection and is connected the secondary connecting rod of the hypsokinesis swash plate leading truck and hypsokinesis swash plate.
7. high-altitude flight toy as claimed in claim 1, it is characterised in that：The first propeller folder is additionally provided with described rotary shaft, the first described propeller is clamping in described rotary shaft by first propeller, the second propeller folder is provided with described power transmission shaft, the second described propeller is clamping on power transmission shaft by second propeller, tail propeller folder is additionally provided with described tailing axle, described tail propeller is clamping on described tailing axle by the tail propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510651121.7A CN106563273A (en) | 2015-10-10 | 2015-10-10 | High-altitude flight toy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510651121.7A CN106563273A (en) | 2015-10-10 | 2015-10-10 | High-altitude flight toy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106563273A true CN106563273A (en) | 2017-04-19 |
Family
ID=58507815
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510651121.7A Pending CN106563273A (en) | 2015-10-10 | 2015-10-10 | High-altitude flight toy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106563273A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606876A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A flight machine with a plurality of propulsion devices |
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 |
| CN106552426A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple propeller propulsion system high-altitude flight device |
-
2015
- 2015-10-10 CN CN201510651121.7A patent/CN106563273A/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 |
| CN106552426A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple propeller propulsion system high-altitude flight device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606876A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A flight machine with a plurality of propulsion devices |
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Application publication date: 20170419 |
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| WD01 | Invention patent application deemed withdrawn after publication |