CN106563270A - Multistage gear reduction novel model plane - Google Patents
Multistage gear reduction novel model plane Download PDFInfo
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- CN106563270A CN106563270A CN201510649065.3A CN201510649065A CN106563270A CN 106563270 A CN106563270 A CN 106563270A CN 201510649065 A CN201510649065 A CN 201510649065A CN 106563270 A CN106563270 A CN 106563270A
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- level
- gear
- propeller
- gear reduction
- swash plate
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Abstract
The invention relates to a multistage gear reduction novel model plane. A third installation seat in a testing platform is fixedly connected with a pedestal. A connection disc of a torque sensor is connected to a sleeve and a guide rod of the third installation seat. The interior of a central cavity of a connection part is provided with a first ball bearing, an internal sleeve ring and a second ball bearing, and an external ring is disposed between the second ball bearing and the first ball bearing. The upper part of the connection part is connected with an upper bearing upper end cover, and the bottom of the connection part is connected with an upper bearing lower end cover. The upper rods of four connection rods are disposed in convex lugs of the connection part, and the lower ends of the four connection rods are disposed in convex lugs of the third installation seat. A second installation seat is connected to an upper panel surface of a connecting shaft, and three tension and pressure sensors are disposed on the second installation seat. The testing platform serves as an indirect output type measurement platform, and employs three one-dimensional tension and pressure sensors and one force moment sensor to obtain four-dimensional information.
Description
Technical field
The present invention relates to a kind of electronic toy, more particularly, the present invention relates to a kind of multiple stage gear reduction Novel model airplane.
Background technology
As requirement of the people to multiple stage gear reduction Novel model airplane is improved constantly，Often require that multiple stage gear reduction Novel model airplane has good flying quality，To increase the interest for manipulating multiple stage gear reduction Novel model airplane，Far-reaching to the flying quality of multiple stage gear reduction Novel model airplane is the weight of multiple stage gear reduction Novel model airplane，Double oar multiple stage gear reduction Novel model airplanes 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 multiple stage gear reduction Novel model airplane considerably increase weight，Therefore in order to mitigate the weight of multiple stage gear reduction Novel model airplane，Need to provide a kind of multiple stage gear reduction Novel model airplane of mechanism section parts that multiple stage gear reduction Novel model airplane offer power in prior art is provided to mitigate whole multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane of model plane mobility can be improved again.
Solving the technical scheme that adopted of present invention problem is：A kind of multiple stage gear reduction Novel model airplane, 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 multiple stage gear reduction Novel model airplane weight of itself, so as to improve the mobility of multiple stage gear reduction Novel model airplane, while also reducing the manufacturing cost of multiple stage gear reduction Novel model airplane.
As the preferred implementation of multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane 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 is used to prevent level synchronization transporter from slipping, two grades of described pulley covers, level Four pulley cover is used to prevent secondary synchronization transporter from slipping.
As another preferred implementation of multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane.
As another preferred implementation of multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane flight, make multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane 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, multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane, make the steering of multiple stage gear reduction Novel model airplane more flexible.
The multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane flight, make multiple stage gear reduction Novel model airplane 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 multiple stage gear reduction Novel model airplane, 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. multiple stage gear reduction Novel model airplane 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. multiple stage gear reduction Novel model airplane 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. multiple stage gear reduction Novel model airplane as claimed in claim 3, it is characterised in that：The device of the synchronous belt tensioning is roller.
5. multiple stage gear reduction Novel model airplane 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. multiple stage gear reduction Novel model airplane 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. multiple stage gear reduction Novel model airplane 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 |
|---|---|---|---|
| CN201510649065.3A CN106563270A (en) | 2015-10-09 | 2015-10-09 | Multistage gear reduction novel model plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510649065.3A CN106563270A (en) | 2015-10-09 | 2015-10-09 | Multistage gear reduction novel model plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106563270A true CN106563270A (en) | 2017-04-19 |
Family
ID=58506045
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510649065.3A Withdrawn CN106563270A (en) | 2015-10-09 | 2015-10-09 | Multistage gear reduction novel model plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106563270A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606872A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A multi-stage decelerator model airplane |
| CN106621376A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Novel model airplane with multi-stage gear speed reduction |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106552427A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple stage gear reduction system model plane |
-
2015
- 2015-10-09 CN CN201510649065.3A patent/CN106563270A/en not_active Withdrawn
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106552427A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple stage gear reduction system model plane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106606872A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A multi-stage decelerator model airplane |
| CN106621376A (en) * | 2015-10-29 | 2017-05-10 | 马铿钧 | Novel model airplane with multi-stage gear speed reduction |
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| 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: 20170419 |
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| WW01 | Invention patent application withdrawn after publication | ||
| DD01 | Delivery of document by public notice |
Addressee: Ma Kengjie Document name: Notification of Approving Refund |
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| DD01 | Delivery of document by public notice |