CN106492476A - The high-altitude vehicle of tailspin oar control azimuth - Google Patents
The high-altitude vehicle of tailspin oar control azimuth Download PDFInfo
- Publication number
- CN106492476A CN106492476A CN201510559797.3A CN201510559797A CN106492476A CN 106492476 A CN106492476 A CN 106492476A CN 201510559797 A CN201510559797 A CN 201510559797A CN 106492476 A CN106492476 A CN 106492476A
- Authority
- CN
- China
- Prior art keywords
- level
- gear
- propeller
- tailspin
- swash plate
- 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.)
- Pending
Links
Landscapes
- Toys (AREA)
Abstract
A kind of high-altitude vehicle of tailspin oar control azimuth of the present invention, including main body frame, empennage, landing gear, the mechanism for providing power and remote receiver, include the power of the first described motor while passing to the belt gear reduction gearing mechanism of the first propeller, the second propeller and tail propeller in the described mechanism that power is provided；Present invention achieves first motor drives the first propeller, the second propeller and tail propeller rotational simultaneously, eliminate two power motors, the weight of the high-altitude vehicle itself of tailspin oar control azimuth is greatly reduced, so as to improve the mobility of the high-altitude vehicle of tailspin oar control azimuth.
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 vehicle of tailspin oar control azimuth.
Background technology
As requirement of the people to the high-altitude vehicle of tailspin oar control azimuth is improved constantly，Often require that the high-altitude vehicle of tailspin oar control azimuth has good flying quality，To increase the interest of the high-altitude vehicle for manipulating tailspin oar control azimuth，The weight of the high-altitude vehicle for being tailspin oar control azimuth far-reaching to the flying quality of the high-altitude vehicle of tailspin oar control azimuth，The high-altitude vehicle of double oar tailspin oar control azimuths is typically all to complete power supply by two first motors，It is also required to two sets of each independent actuating units，Tail propeller is also required to an independent motor to drive simultaneously，This makes the high-altitude vehicle of tailspin oar control azimuth considerably increase weight，Therefore in order to mitigate the weight of the high-altitude vehicle of tailspin oar control azimuth，Need to provide a kind of mechanism section parts of the high-altitude vehicle offer power for omitting tailspin oar control azimuth in prior art to mitigate the high-altitude vehicle of the tailspin oar control azimuth of the high-altitude vehicle weight of whole tailspin oar control azimuth.
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, can improve the high-altitude vehicle of the tailspin oar control azimuth of model plane mobility again.
Solving the technical scheme that adopted of present invention problem is：A kind of high-altitude vehicle of tailspin oar control azimuth, including main body frame, with the back-connected empennage of main body frame, the landing gear that supports the main body frame is connected to 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 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 weight of the high-altitude vehicle itself of tailspin oar control azimuth, so as to improve the mobility of the high-altitude vehicle of tailspin oar control azimuth, while also reducing the manufacturing cost of the high-altitude vehicle of tailspin oar control azimuth.
As the preferred implementation of the high-altitude vehicle of tailspin oar control azimuth 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, the two grades of driven gears for engaging with one-level driven gear and being connected with described power transmission shaft one end, two grades of 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 band gear with tailing axle, one-level band gear is connected with three-level band gear by level synchronization transporter, two grades of band gears are connected with level Four band gear by secondary synchronization transporter.
As another preferred implementation of high-altitude vehicle of tailspin oar control azimuth of the present invention, the described two grades both sides for being respectively placed in two grades of driven gears with gear and three-level with gear.
As another preferred implementation of high-altitude vehicle of tailspin oar control azimuth 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 two grades of pulley covers with gear side, 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 for preventing level synchronization transporter from slipping, two grades of described pulley covers, level Four pulley cover is used for preventing secondary synchronization transporter from slipping.
As another preferred implementation of high-altitude vehicle of tailspin oar control azimuth of the present invention, described belt gear reduction gearing mechanism is additionally provided with makes roller devices of two grades of the connection with gear Yu secondary synchronization transporter tensioning of the level Four with gear, the roller devices make secondary synchronization transporter be stretched on two grades of band gears and level Four band gear at any time, to prevent synchronous belt from sliding on two grades of band gears and level Four band gear.
As another preferred implementation of high-altitude vehicle of tailspin oar control azimuth of the present invention, which 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 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 the main body frame and connects the master link of lean forward swash plate leading truck and the swash plate that leans forward at swash plate leading truck, described rear level controller includes the hypsokinesis swash plate on tailing axle, steering wheel afterwards, the slave connecting rod of steering wheel and hypsokinesis swash plate after connection, the hypsokinesis swash plate leading truck being arranged on empennage frame and the secondary connecting rod for connecting the hypsokinesis swash plate leading truck and hypsokinesis swash plate, main, rear level controller more neatly realizes the steering of the high-altitude vehicle of tailspin oar control azimuth.
As another preferred implementation of high-altitude vehicle of tailspin oar control azimuth of the present invention, which 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 by gimbal lever's union joint installed in the upper end of rotary shaft, its whole body is balanced during the high-altitude vehicle flight of the dynamic balancer tailspin oar control azimuth, makes the high-altitude vehicle of tailspin oar control azimuth more can safety and steady flight.
Below in conjunction with drawings and Examples, technical scheme is described in further detail.
Description of the drawings
Structural representations of the Fig. 1 for the high-altitude vehicle of the tailspin oar control azimuth 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 high-altitude vehicle of tailspin oar control azimuth 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, the remote receiver 5 that can receive external control signal on main body frame 1.
The mechanism 4 of described offer power includes the first motor、Power transmission shaft、Rotary shaft through the power transmission shaft、Installation the first propeller on the rotary shaft and the second propeller by back blades folder on power transmission shaft are pressed from both sides by primary blades，First motor is 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 at by bearing on the bearing block of main body frame 1，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，The two grades of driven gears for engaging with one-level driven gear and being connected 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，Two grades of 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 at by bearing on the bearing block of main body frame 1，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 with three-level band gear by level synchronization transporter，Two grades of band gears are connected with level Four band gear by secondary synchronization transporter，Tail propeller is by caudal lobe piece folder on tailing axle，Tailing axle is positioned on the bearing block of tailstock by bearing，One-level pulley cover and bearing three-level pulley cover are used for the slippage for preventing the first belt pulley，Two grades of pulley covers and level Four pulley cover are used for the slippage for preventing 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 roller devices also can be replaced with other devices in other embodiments certainly.
Motor gear rotation of the first described Motor drive in its drive shaft, motor gear rotation rotates the one-level driven gear for engaging, so as to drive engage two grades of driven gear rotations with one-level driven gear, 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 rotarily drive rotary shaft of the three-level with gear rotates, 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.First motor is achieved in that while driving the rotation of the first propeller, the second propeller and tail propeller, two motors has been eliminated, is significantly reduced the weight of model plane itself, improve the flying quality of model plane, while also saving manufacturing cost.
The high-altitude vehicle of described tailspin oar control azimuth 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 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 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 high-altitude vehicle of level controller and rear level controller co- controlling tailspin oar control azimuth in front of this, make the steering of the high-altitude vehicle of tailspin oar control azimuth more flexible.
The high-altitude vehicle of the tailspin oar control azimuth 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 by gimbal lever's union joint installed in the upper end of rotary shaft, the dynamic balancer makes to balance its whole body during the high-altitude vehicle flight of tailspin oar control azimuth, makes the high-altitude vehicle of tailspin oar control azimuth more can safety and steady flight.
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 high-altitude vehicle of tailspin oar control azimuth, 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、Rotary shaft through 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，The two grades of driven gears for engaging with one-level driven gear and being connected with described power transmission shaft one end，Two grades of 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 with three-level band gear by level synchronization transporter，Two grades of band gears are connected with level Four band gear by secondary synchronization transporter.
2. the high-altitude vehicle of tailspin oar control azimuth 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 two grades of pulley covers with gear side, 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. the high-altitude vehicle of tailspin oar control azimuth as claimed in claim 2, it is characterised in that：Described belt gear reduction gearing mechanism is additionally provided with makes device of two grades of the connection with gear Yu synchronous belt tensioning of the level Four with gear.
4. the high-altitude vehicle of tailspin oar control azimuth as claimed in claim 3, it is characterised in that：The device of the synchronous belt tensioning is roller.
5. the high-altitude vehicle of tailspin oar control azimuth as claimed in claim 1, it is characterised in that：Which also includes that dynamic balancer, described dynamic balancer include gimbal lever's union joint, the gimbal lever and be 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. the high-altitude vehicle of tailspin oar control azimuth as claimed in claim 1, it is characterised in that：Which 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 on power transmission shaft, front steering wheel, the front rod of steering wheel and the swash plate that leans forward before 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, described rear level controller includes hypsokinesis swash plate on tailing axle, rear steering wheel, connect after the connecting rod of steering wheel and hypsokinesis swash plate, hypsokinesis swash plate leading truck and be connected the secondary connecting rod of the hypsokinesis swash plate leading truck and hypsokinesis swash plate.
7. the high-altitude vehicle of tailspin oar control azimuth 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 the described rotary shaft by first propeller, the second propeller folder is provided with described power transmission shaft, the second described propeller is clamping on the power transmission shaft by second propeller, it is additionally provided with tail propeller folder on described tailing axle, described tail propeller is clamping on the described tailing axle by the tail propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510559797.3A CN106492476A (en) | 2015-09-03 | 2015-09-03 | The high-altitude vehicle of tailspin oar control azimuth |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510559797.3A CN106492476A (en) | 2015-09-03 | 2015-09-03 | The high-altitude vehicle of tailspin oar control azimuth |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106492476A true CN106492476A (en) | 2017-03-15 |
Family
ID=58286594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510559797.3A Pending CN106492476A (en) | 2015-09-03 | 2015-09-03 | The high-altitude vehicle of tailspin oar control azimuth |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106492476A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106546438A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Four-degree-of-freedom Aerospace vehicle test platform based on one-dimensional force transducer |
| CN106540460A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Quadrotor rotor characteristic integrated test system |
| CN106552427A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple stage gear reduction system model plane |
| CN106552426A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple propeller propulsion system high-altitude flight device |
| CN106563271A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | High-altitude aircraft capable of controlling orientation by using tail propeller |
| CN106606876A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A flight machine with a plurality of propulsion devices |
-
2015
- 2015-09-03 CN CN201510559797.3A patent/CN106492476A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106546438A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Four-degree-of-freedom Aerospace vehicle test platform based on one-dimensional force transducer |
| CN106540460A (en) * | 2015-09-20 | 2017-03-29 | 许美兰 | Quadrotor rotor characteristic integrated test system |
| CN106552427A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple stage gear reduction system model plane |
| CN106552426A (en) * | 2015-09-25 | 2017-04-05 | 郑华耀 | Multiple propeller propulsion system high-altitude flight device |
| CN106563271A (en) * | 2015-10-09 | 2017-04-19 | 马铿杰 | High-altitude aircraft capable of controlling orientation by using tail propeller |
| CN106606876A (en) * | 2015-10-23 | 2017-05-03 | 许美兰 | A flight machine with a plurality of propulsion devices |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106492476A (en) | The high-altitude vehicle of tailspin oar control azimuth | |
| CN106474747A (en) | New flight system with ultra-light-weight | |
| CN106552427A (en) | Multiple stage gear reduction system model plane | |
| CN106492475A (en) | The aerial device that multiple propeller drives | |
| CN106540460A (en) | Quadrotor rotor characteristic integrated test system | |
| CN106552426A (en) | Multiple propeller propulsion system high-altitude flight device | |
| CN205931254U (en) | Through controlling device that eccentric some position changes cycloid oar lift orientation | |
| CN106563270A (en) | Multistage gear reduction novel model plane | |
| CN201139952Y (en) | Model aerial vehicle | |
| CN106563271A (en) | High-altitude aircraft capable of controlling orientation by using tail propeller | |
| CN109099114A (en) | Carry transmission mechanism and helicopter reducer | |
| CN106468627A (en) | Quadrotor rotor characteristic integrated test system | |
| CN106563273A (en) | High-altitude flight toy | |
| CN204121761U (en) | There is multiple screw flying toy | |
| CN206968962U (en) | A kind of VUAV motor horn folds drive mechanism | |
| CN106468626A (en) | Four-degree-of-freedom Aerospace vehicle test platform based on one-dimensional force transducer | |
| CN106606876A (en) | A flight machine with a plurality of propulsion devices | |
| CN106823397A (en) | Quadruple screw propeller aircraft | |
| CN106606872A (en) | A multi-stage decelerator model airplane | |
| CN106546438A (en) | Four-degree-of-freedom Aerospace vehicle test platform based on one-dimensional force transducer | |
| CN106621376A (en) | Novel model airplane with multi-stage gear speed reduction | |
| CN106552431A (en) | Flight system with gear clutch | |
| CN108261781A (en) | Quadrotor rotor characteristic integrated test system | |
| CN106823399A (en) | Multiple-stage reduction unit model plane | |
| CN109091891A (en) | The aerial device that multiple propeller drives |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170315 |
|
| WD01 | Invention patent application deemed withdrawn after publication |