CN106669169A - Multilayer rotor wing rotation plane circumferentially distributed air vehicle - Google Patents
Multilayer rotor wing rotation plane circumferentially distributed air vehicle Download PDFInfo
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- CN106669169A CN106669169A CN201510758159.4A CN201510758159A CN106669169A CN 106669169 A CN106669169 A CN 106669169A CN 201510758159 A CN201510758159 A CN 201510758159A CN 106669169 A CN106669169 A CN 106669169A
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- gear
- circumferentially distributed
- rotor wing
- travelling gear
- rotation plane
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Abstract
The invention relates to a multilayer rotor wing rotation plane circumferentially distributed air vehicle. The multilayer rotor wing rotation plane circumferentially distributed air vehicle comprises a framework, a rear portion power device connected to the back of the framework, a lower support supporting the framework, an energy supply device arranged on the framework and a central controller capable of receiving an external signal and controlling the energy supply device according to the external signal and provided with an integrated chip. The multilayer rotor wing rotation plane circumferentially distributed air vehicle achieves that one power source drive at least two airscrews to rotate simultaneously, at least one power source is omitted, the weight of the multilayer rotor wing rotation plane circumferentially distributed air vehicle is greatly decreased, and the flight performance of the multilayer rotor wing rotation plane circumferentially distributed air vehicle is improved.
Description
Technical field
The present invention relates to a kind of toy, more particularly to a kind of flying toy.
Background technology
Flying toy has been increasingly becoming the toy of people's fashion.The flying toy of existing coaxial double slurries is all to complete power supply by two sets of power sources.The weight of flying toy itself has a significant impact for the flying quality tool of flying toy, and two sets of power sources bring immeasurable impact to flying toy flying quality.
Therefore, a kind of a set of power source of our demands drives the circumferentially distributed aircraft of twin-propeller multilayer rotor wing rotation plane simultaneously.
The content of the invention
Based on the deficiencies in the prior art, problem to be solved by this invention is to provide a kind of circumferentially distributed aircraft of multilayer rotor wing rotation plane, the circumferentially distributed aircraft of multilayer rotor wing rotation plane realizes that a set of power source drives at least two screws, mitigate the circumferentially distributed aircraft own wt of multilayer rotor wing rotation plane, improve the flying quality of the circumferentially distributed aircraft of multilayer rotor wing rotation plane.
To solve the above problems, the circumferentially distributed aircraft of a kind of multilayer rotor wing rotation plane that the present invention is provided, the circumferentially distributed aircraft of multilayer rotor wing rotation plane includes a kind of circumferentially distributed aircraft of multilayer rotor wing rotation plane, the circumferentially distributed aircraft of multilayer rotor wing rotation plane includes skeleton, it is connected to the rear portion power set at skeleton rear, support the lower carriage of the skeleton, the energy supply device being arranged on the skeleton, and external signal can be received and the central controller with integrated chip of the energy supply device can be controlled according to external signal, the energy supply device includes power source, hollow main shaft, through the power transmission shaft of the hollow main shaft, the main screw being arranged on power transmission shaft and the secondary screw being arranged on hollow main shaft, the energy supply device also includes the driving gear being connected with power source, the travelling gear being connected with the driving gear, the transportation sprocket being connected with power transmission shaft and the carrier chain of connection travelling gear and transportation sprocket, the driving gear is fixed on the hollow main shaft.
Compared with prior art, the energy supply device of the circumferentially distributed aircraft of multilayer rotor wing rotation plane of the present invention has tangible improvement, its driving gear is by the drive of a set of power source come band nutating gear synchronous axial system, travelling gear drives transportation sprocket to rotate backward by carrier chain, because driving gear is fixed on hollow main shaft so as to drive the secondary screw on hollow main shaft to rotate, because transportation sprocket is connected so as to drive the main screw counter-rotating on power transmission shaft with power transmission shaft.The circumferentially distributed aircraft of multilayer rotor wing rotation plane for thus making the present invention realizes a set of power source at least two propeller rotationals of drive simultaneously, save at least a set of power source, the weight of the circumferentially distributed aircraft itself of multilayer rotor wing rotation plane is significantly reduced, the performance of the circumferentially distributed aircraft flight of multilayer rotor wing rotation plane is improve.
Used as one embodiment, the travelling gear includes coaxial and is divided into the main drive gear of two-layer and from travelling gear, and the main drive gear is connected with driving gear, and the carrier chain is socketed on from travelling gear and transportation sprocket.Travelling gear is preferably connected with driving gear, also preferably make to be connected with carrier chain.
As one embodiment, the circumferentially distributed aircraft of multilayer rotor wing rotation plane also includes the travelling gear fixed mount being installed on skeleton, the power transmission shaft is positioned on the travelling gear fixed mount by a power transmission shaft fixture, and the transportation sprocket is fixedly connected on the power transmission shaft fixture.The travelling gear fixed mount is provided with the first connecting hole, and the power transmission shaft fixture one end is connected with power transmission shaft, and its other end is positioned in first connecting hole by a bearing.One end of the power transmission shaft fixture connection power transmission shaft is socketed with the first transmission-gear cover, and the first transmission-gear cover apical grafting transportation sprocket is slid with preventing the carrier chain.
Used as one embodiment, the circumferentially distributed aircraft of multilayer rotor wing rotation plane also includes the travelling gear fixed mount being installed on skeleton, and the travelling gear is positioned on the travelling gear fixed mount by gear shaft.The travelling gear fixed mount is provided with the second connecting hole, and described gear shaft one end is connected to the travelling gear, and its other end is positioned in second connecting hole by a bearing.The second transmission-gear cover is socketed with the gear shaft, the second transmission-gear cover apical grafting travelling gear slides to prevent the carrier chain.
As one embodiment, four connection support are arranged with the travelling gear fixed mount, the travelling gear fixed mount is fixedly installed on skeleton by the connection support.The power source is connected by a master gear with driving gear.
To make the present invention easier to understand, the circumferentially distributed aircraft of multilayer rotor wing rotation plane of the present invention is expanded on further below in conjunction with accompanying drawing.
Description of the drawings
Fig. 1 is the explosive view of the circumferentially distributed aircraft of multilayer rotor wing rotation plane of a preferred embodiment of the present invention.
Fig. 2 is the connection diagram of energy supply device in part in Fig. 1.
Fig. 3 is the structural representation of Fig. 1 postmedian power set.
Specific embodiment
With reference now to Description of Drawings the preferred embodiments of the present invention,.
With reference to Fig. 1, Fig. 2, the circumferentially distributed aircraft of multilayer rotor wing rotation plane of the present embodiment includes skeleton 10, the rear portion power set 30 that are connected to the rear of skeleton 10, the lower carriage 40 for supporting the skeleton 10, the energy supply device 60 being arranged on the skeleton 10, can receive external signal and the central controller 50 with integrated chip of the energy supply device 60 can be controlled according to external signal.
With continued reference to Fig. 1, Fig. 2, the energy supply device 60 is provided with main screw 68, on the hollow main shaft 66 secondary screw 69 is provided with including a set of power source 61, hollow main shaft 66, through the power transmission shaft 67 of the hollow main shaft 66 on the power transmission shaft 67.The output end of the power source 61 is connected with motor master gear 601, and the motor master gear 601 is connected with a driving gear 62.The driving gear 62 is fixed on hollow main shaft 66.The driving gear 62 is connected with a travelling gear 64, and the travelling gear 64 is connected by a carrier chain 65 with a transportation sprocket 63.The transportation sprocket 63 includes coaxial and is divided into bilevel connecting portion 631 and gear part 632, and the connecting portion 631 is connected by a bearing 609 with driving gear 62.The travelling gear 64 includes coaxial and is divided into the main drive gear 641 of two-layer and from travelling gear 642, and the main drive gear 641 is connected with driving gear 62.The carrier chain 65 is socketed in the gear part 632 from travelling gear 642 and transportation sprocket 63 of travelling gear 64.
The energy supply device 60 also includes the travelling gear fixed mount 602 being installed on skeleton 10, and the travelling gear fixed mount 602 includes that travelling gear fixes frame body 01, is symmetricly set in four connection support 02 that the travelling gear is fixed on frame body 01.Perforate in the connection support 02 is again fixedly installed in the travelling gear fixed mount 602 on skeleton 10 by screw.The travelling gear is fixed on frame body 01 and is provided with the first connecting hole 011, the second connecting hole 012.The driving gear 62, the center drilling of transportation sprocket 63, the power transmission shaft 67 is fixed on a power transmission shaft fixture 603 through the hole.The one end of power transmission shaft fixture 603 connection power transmission shaft 67, its other end is positioned in the first connecting hole 011 of the travelling gear fixed mount 602 by a bearing 607.One end of the power transmission shaft fixture 603 connection power transmission shaft 67 is socketed with the first transmission-gear cover 605, and the apical grafting of the first transmission-gear cover 605 transportation sprocket 63 is preventing the carrier chain 65 from sliding.The transportation sprocket 63 is fixedly connected on the power transmission shaft fixture 603.
The travelling gear 64 is positioned on the travelling gear fixed mount 602 by gear shaft 604.The one end of the gear shaft 64 be connected to the travelling gear 64 from travelling gear 642, its other end is positioned in second connecting hole 012 by a bearing 608.The second transmission-gear cover 606 is socketed with the gear shaft 604, the apical grafting travelling gear 64 of the second transmission-gear cover 606 is preventing the carrier chain 65 from sliding.
Driving gear 62 drives the band synchronous axial system of nutating gear 64 by power source 61, travelling gear 64 from travelling gear 641 by carrier chain 65 drive transportation sprocket 63 rotate backward, because driving gear 62 is fixed on hollow main shaft 66 so as to drive the secondary screw 69 on hollow main shaft 66 to rotate, because transportation sprocket 63 is connected so as to drive the counter-rotating of main screw 68 on power transmission shaft 67 with power transmission shaft 67.It has been achieved in that a set of power source drives double oars to rotate simultaneously, has saved a set of power source, significantly reduced the weight of the circumferentially distributed aircraft itself of multilayer rotor wing rotation plane, has improve the performance of the circumferentially distributed aircraft flight of multilayer rotor wing rotation plane.
With reference to Fig. 1, Fig. 3, the rear portion power set 30 include the tailstock 31 being connected with skeleton 10 and the tail screw 32 being arranged on tailstock 31 and the tail motor 33 for driving the tail screw 32.
With continued reference to Fig. 1, the circumferentially distributed aircraft of the multilayer rotor wing rotation plane also includes balanced component 90, and the balanced component 90 includes the balancing pole 91 being installed on power transmission shaft 67 and the balance blade 92 for being arranged at the two ends of balancing pole 91.The balanced component 90 makes the circumferentially distributed aircraft flight of multilayer rotor wing rotation plane more steady safe and reliable.
The circumferentially distributed aircraft of the multilayer rotor wing rotation plane also includes steering assembly 80, the steering assembly 80 includes the pitch 81 being installed on hollow main shaft 67, steering wheel 82, connect the steering wheel 82 and pitch 81 pull bar 83, turning sleeve 84 and it is connected the connecting rod 85 of the turning sleeve 84 and pitch 81, the steering assembly 80 efficiently controls the circumferentially distributed aircraft of multilayer rotor wing rotation plane and flexibly turns to.The circumferentially distributed aircraft of the multilayer rotor wing rotation plane also includes the battery 70 for providing electric energy for energy supply device and steering assembly.
Above disclosed is only presently preferred embodiments of the present invention, can not limit the interest field of the present invention, therefore the equivalent variations made according to scope of the present invention patent with this certainly, still belongs to the scope that the present invention is covered.
Claims (6)
1. the circumferentially distributed aircraft of a kind of multilayer rotor wing rotation plane, it is characterised in that：It includes skeleton, it is connected to the rear portion power set at skeleton rear, support the lower carriage of the skeleton, the energy supply device being arranged on the skeleton, and external signal can be received and the central controller with integrated chip of the energy supply device can be controlled according to external signal, the energy supply device includes power source, hollow main shaft, through the power transmission shaft of the hollow main shaft, the main screw being arranged on power transmission shaft and the secondary screw being arranged on hollow main shaft, the energy supply device also includes the driving gear being connected with power source, the travelling gear engaged with the driving gear, the transportation sprocket being connected with power transmission shaft and the carrier chain for connecting the travelling gear and transportation sprocket, the travelling gear fixed mount being installed on skeleton, the power transmission shaft is positioned on the travelling gear fixed mount by a power transmission shaft fixture, the transportation sprocket is fixedly connected on the power transmission shaft fixture, the driving gear is fixed on described hollow main shaft one end.
2. the circumferentially distributed aircraft of multilayer rotor wing rotation plane as claimed in claim 1, it is characterised in that：The travelling gear includes coaxial main drive gear and from travelling gear, the main drive gear is engaged with driving gear, the carrier chain is socketed on from travelling gear and transportation sprocket, the travelling gear fixed mount is provided with the first connecting hole, the power transmission shaft fixture one end is connected with power transmission shaft, and its other end is positioned in first connecting hole by a bearing.
3. the circumferentially distributed aircraft of multilayer rotor wing rotation plane as claimed in claim 2, it is characterised in that：One end of the power transmission shaft fixture connection power transmission shaft is socketed with the first transmission-gear cover, and the first transmission-gear cover apical grafting transportation sprocket is slid with preventing the carrier chain.
4. the circumferentially distributed aircraft of multilayer rotor wing rotation plane as claimed in claim 3, it is characterised in that：The second connecting hole is additionally provided with the travelling gear fixed mount, described gear shaft one end is connected to the travelling gear, and its other end is positioned in second connecting hole by a bearing.
5. the circumferentially distributed aircraft of multilayer rotor wing rotation plane as claimed in claim 4, it is characterised in that：The second transmission-gear cover is socketed with the gear shaft, the second transmission-gear cover apical grafting travelling gear slides to prevent the carrier chain.
6. the circumferentially distributed aircraft of multilayer rotor wing rotation plane as claimed in claim 1, it is characterised in that：Four connection support are arranged with the travelling gear fixed mount, the travelling gear fixed mount is fixedly installed on skeleton by the connection support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510758159.4A CN106669169A (en) | 2015-11-07 | 2015-11-07 | Multilayer rotor wing rotation plane circumferentially distributed air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510758159.4A CN106669169A (en) | 2015-11-07 | 2015-11-07 | Multilayer rotor wing rotation plane circumferentially distributed air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106669169A true CN106669169A (en) | 2017-05-17 |
Family
ID=58864423
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510758159.4A Withdrawn CN106669169A (en) | 2015-11-07 | 2015-11-07 | Multilayer rotor wing rotation plane circumferentially distributed air vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106669169A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101116783A (en) * | 2007-08-27 | 2008-02-06 | 罗之洪 | Model airplane |
| CN204233766U (en) * | 2014-10-15 | 2015-04-01 | 许美兰 | There is the flying toy of multiple power set |
| CN105771273A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Model airplane multi-propeller control system |
| CN105797389A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Multi-propeller control system of model airplane |
-
2015
- 2015-11-07 CN CN201510758159.4A patent/CN106669169A/en not_active Withdrawn
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101116783A (en) * | 2007-08-27 | 2008-02-06 | 罗之洪 | Model airplane |
| CN204233766U (en) * | 2014-10-15 | 2015-04-01 | 许美兰 | There is the flying toy of multiple power set |
| CN105771273A (en) * | 2014-12-25 | 2016-07-20 | 许美兰 | Model airplane multi-propeller control system |
| CN105797389A (en) * | 2014-12-31 | 2016-07-27 | 马铿杰 | Multi-propeller control system of model airplane |
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| Date | Code | Title | Description |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170517 |
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| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Ma Kengjie Document name: Notification of Approving Refund |