CN109229370A - A kind of drum-type telescopic rotor device - Google Patents
A kind of drum-type telescopic rotor device Download PDFInfo
- Publication number
- CN109229370A CN109229370A CN201811357427.1A CN201811357427A CN109229370A CN 109229370 A CN109229370 A CN 109229370A CN 201811357427 A CN201811357427 A CN 201811357427A CN 109229370 A CN109229370 A CN 109229370A
- Authority
- CN
- China
- Prior art keywords
- roller
- drum
- blade
- limiter
- fixed
- 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
- 230000033001 locomotion Effects 0.000 claims abstract description 8
- 230000000694 effects Effects 0.000 claims abstract description 4
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 5
- 230000000712 assembly Effects 0.000 claims description 4
- 238000000429 assembly Methods 0.000 claims description 4
- 238000009434 installation Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
- B64D35/04—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission driving a plurality of propellers or rotors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
A kind of set the rolling wing, the advantage of flapping wing and screw wing respectively, flexible blade is installed in drum-type, its effect for passing through roller and the eccentric limiter of abnormity, it is co- controlling several pieces blade circulation rotatings, flexible, complete flapping wing movement, to enhance the mechanical efficiency of blade, enhance the device of aircraft mobility.
Description
Technical field
It is a kind of using the flexible blade progress flapping wing of roller drive and rotary motion the present invention relates to rolling wing machine technical field
The device of thrust or lift is provided.
Background technique
The rolling-swing device of the prior art be paddle is made into one " drum-type " combination rotate to generate thrust and liter
Power；What flapping wing device was copied is flight animal flapping motion, more flexible than fixed-wing on both airfoil theories, but structure is complicated does not tie
Real, technology is immature, it is difficult to realize high-speed flight；Spiral wing aircraft is using propeller motion as its lift system, structure
Complexity, Maintenance and Repair larger workload, higher operating costs, speed is lower, and safety is poor, and voyage is shorter.
Summary of the invention
The purpose of the present invention is set the rolling wing, the advantage of flapping wing and screw wing respectively, provides and a kind of stretch paddle in drum-type
Leaf device, is rotated by roller and the eccentric limiter of abnormity controls blade and rotates and stretch to enhance the mechanical efficiency of blade,
Enhance the device of aircraft mobility.
The technical scheme is that a kind of drum-type rotor driver for keeping blade flexible by controlling eccentric point position, it is wrapped
Include: power source, roller, inner shaft, outer shaft, blade, tension spring, connecting rod, the eccentric limiter of abnormity, transmission belt, pedestal, duct, covering,
Bracket, gyroscope, steering engine, controller assemblies；
Centre of the drum is fixed inner shaft and outer shaft by the present apparatus, rack-mount, and bracket is fixed on the base, and power source is fixed
On one pedestal of roller, power source drives roller to rotate by transmission belt；Steering engine is fixed on one pedestal of roller
On, drive drum to make divertical motion；Gyroscope and controller assemblies are mounted on steering engine side, the operation holding meanss of control device
Balance；4 (as needed, 268 etc. are ok) rectangle blades of installation are uniformly distributed in drums inside, and with drawing
Spring is fixed, and blade width is 96% or so of radius roller；The mounting bracket on the pedestal of roller other end installs abnormity on bracket
Eccentric limiter, the limiter other end are fixed on the outer axle bearing of roller；The blade installed in roller, passes through connecting rod and connection
Component is connected on special-shaped eccentric limiter；Finally, installing covering and duct on the outside of roller.The present invention is roller peace
Outer shaft and inner shaft are filled, they are concentric shafts.Inner shaft is the shaft of rolling wheel support, provides the support in structure；Outer shaft opens band
The effect of dynamic roller rotation, while being limiter bottom fixing axle.
The utility model has the advantages that
The present invention overcomes existing rolling-swing device, flapping wing device inefficiency, screw wing apparatus structure is complicated, safety is low is asked
Topic, realizes mechanical efficiency, mobility and the promotion of safety.
Specific embodiment:
The present invention will now be described in detail with reference to the accompanying drawings and examples.
Referring to a kind of roller rotor driver for keeping blade flexible by controlling eccentric point position of attached drawing 1, it include: power source (1),
The eccentric limiter (8) of roller (2), inner shaft (3), outer shaft (4), blade (5), tension spring (6), connecting rod (7), abnormity, transmission belt (9),
Pedestal (10), duct (15), covering (16), bracket (11), gyroscope (13), steering engine (12), controller assemblies (14)；By power
Source (1) drives roller (2) rotation, and the rectangle blade (5) in roller (2) also starts to rotate under the drive of roller (2), due to
The effect of the eccentric limiter (8) of the external abnormity of roller (2), first rectangle blade (5) in roller (2) have arrived certain angle
Degree will stretch out roller (2) and do the movement of downward flapping wing, after the completion of actuating length, retract roller (2) at once, and then roller (2)
Second interior rectangle blade (5) also stretches out roller (2) and makes same movement, following third, the 4th, and then again
One second recycles this actuating length, in gyroscope (13), duct (15), steering engine (12), the coordinated of control system (14)
Under, generate the thrust or lift to certain orientation.
Detailed description of the invention:
Fig. 1 is structural schematic diagram of the invention；
Fig. 2 is left side internal view of the invention；
The right side external view of the invention of Fig. 3；
The top view of the invention of Fig. 4.
In conclusion the above is merely preferred embodiments of the present invention, being not intended to limit the scope of the present invention.It is all
Within the spirit and principles in the present invention, any modification, equivalent replacement, improvement and so on should be included in protection of the invention
Within the scope of.
Claims (3)
1. a kind of drum-type telescopic rotor device, it is characterised in that: it includes: power source (1), roller (2), inner shaft (3), outer shaft
(4), the eccentric limiter (8) of blade (5), tension spring (6), connecting rod (7), abnormity, transmission belt (9), pedestal (10), duct (15), illiteracy
Skin (16), bracket (11), gyroscope (13), steering engine (12), controller assemblies (14).
2. a kind of drum-type telescopic rotor device according to claim 1, it is characterised in that: roller (2) center
Inner shaft (3), outer shaft (4) are connect, rack-mount (11), bracket is fixed on the base (10), and power source (1) is fixed on roller
On (2) pedestals (10), power source (1) drives roller (1) to rotate by transmission belt (9)；Steering engine (12) is fixed on
On (2) pedestals (10) of roller, drum (2) is driven to make divertical motion；Be uniformly distributed inside the roller (2) installation 4 (according to
Need, 268 16 32 64 are ok) rectangle blade (5), and it is fixed with tension spring (6), blade width is roller
(2) 96% or so of radius；The mounting bracket (11) on roller (2) other end pedestal (10), installation abnormity is eccentric on bracket (11)
Limiter (8), abnormity bias limiter (8) other end are fixed on the outer shaft (4) of roller (2)；The blade installed in roller (2)
(5), it is connected on special-shaped eccentric limiter (8) by connecting rod (7)；Covering (16) and duct are installed in the outer ring of roller (2)
(15).
3. a kind of drum-type telescopic rotor device according to claim 1, it is characterised in that: the roller (2) is mounted with
Outer shaft (4) and inner shaft (4), they are concentric shafts, and inner shaft (3) is drum (2) support shaft, provide the support in structure；Outer shaft (4)
Open the effect for driving roller (2) rotation, while the fixing axle as special-shaped eccentric limiter (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811357427.1A CN109229370A (en) | 2018-11-15 | 2018-11-15 | A kind of drum-type telescopic rotor device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811357427.1A CN109229370A (en) | 2018-11-15 | 2018-11-15 | A kind of drum-type telescopic rotor device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109229370A true CN109229370A (en) | 2019-01-18 |
Family
ID=65075345
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811357427.1A Pending CN109229370A (en) | 2018-11-15 | 2018-11-15 | A kind of drum-type telescopic rotor device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109229370A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2285242Y (en) * | 1995-11-29 | 1998-07-01 | 王茂春 | Vertaplane capable of using on water, land and air |
| CN103863562A (en) * | 2014-03-29 | 2014-06-18 | 郑全逸 | Vertical-lifting device with combined propellers |
| CN103899474A (en) * | 2014-03-04 | 2014-07-02 | 哈尔滨工程大学 | Telescopic variable blade device |
| CN105620749A (en) * | 2016-03-03 | 2016-06-01 | 三翼航空科技南通有限公司 | Rollin wing variable pitch mechanism |
| CN106143906A (en) * | 2015-04-13 | 2016-11-23 | 北京强度环境研究所 | A kind of coaxial Cycloidal propeller aerial vehicle |
| US20160376003A1 (en) * | 2015-06-26 | 2016-12-29 | Yuri Feldman | Aircraft |
| CN205931254U (en) * | 2016-08-16 | 2017-02-08 | 金戈 | Through controlling device that eccentric some position changes cycloid oar lift orientation |
| US20180044012A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft with tilting cross-flow fan wings |
-
2018
- 2018-11-15 CN CN201811357427.1A patent/CN109229370A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2285242Y (en) * | 1995-11-29 | 1998-07-01 | 王茂春 | Vertaplane capable of using on water, land and air |
| CN103899474A (en) * | 2014-03-04 | 2014-07-02 | 哈尔滨工程大学 | Telescopic variable blade device |
| CN103863562A (en) * | 2014-03-29 | 2014-06-18 | 郑全逸 | Vertical-lifting device with combined propellers |
| CN106143906A (en) * | 2015-04-13 | 2016-11-23 | 北京强度环境研究所 | A kind of coaxial Cycloidal propeller aerial vehicle |
| US20160376003A1 (en) * | 2015-06-26 | 2016-12-29 | Yuri Feldman | Aircraft |
| CN105620749A (en) * | 2016-03-03 | 2016-06-01 | 三翼航空科技南通有限公司 | Rollin wing variable pitch mechanism |
| US20180044012A1 (en) * | 2016-08-10 | 2018-02-15 | Bell Helicopter Textron Inc. | Aircraft with tilting cross-flow fan wings |
| CN205931254U (en) * | 2016-08-16 | 2017-02-08 | 金戈 | Through controlling device that eccentric some position changes cycloid oar lift orientation |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20190118 |
|
| WD01 | Invention patent application deemed withdrawn after publication |