CN106379533A - Generating device for thrust of electric roller wing - Google Patents
Generating device for thrust of electric roller wing Download PDFInfo
- Publication number
- CN106379533A CN106379533A CN201610823728.3A CN201610823728A CN106379533A CN 106379533 A CN106379533 A CN 106379533A CN 201610823728 A CN201610823728 A CN 201610823728A CN 106379533 A CN106379533 A CN 106379533A
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- China
- Prior art keywords
- main shaft
- wing
- shaft
- hand rotation
- roller
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
The invention discloses a generating device for thrust of an electric roller wing and belongs to the technical field of aviation. The generating device comprises a rack, a main shaft and two, three or four rotating wings which are uniformly distributed at the periphery of the main shaft and are identical in structure; each rotating wing comprises a left rotating arm, a right rotating arm, an electric motor, a roller shaft and a roller wing; the left end and the right end of the main shaft are arranged on the rack through bearings; all the rotating wings are arranged on the main shaft through respective left rotating arms and right rotating arms; the left rotating arms and the right rotating arms are mutually parallel and are vertically connected with the main shaft; the roller wings and the main shaft form a parallel layout; the left end and the right end of each roller shaft are respectively arranged at one end, away from the main shaft, of the corresponding left rotating arm and at one end, away from the main shaft, of the corresponding right rotating arm through bearings; the main shaft, the left rotating arms, the roller shafts and the right rotating arms are positioned in the same plane; each electric motor is arranged at the left end of the corresponding roller shaft; each electric motor can drive the corresponding roller shaft and the corresponding roller wing to rotate; the rotating speeds and the directions of the roller wings accord with a sine function rule; the device is driven by power to generate thrust and can be applied to a vertically lifting aircraft to serve as a force lifting device.
Description
Technical field
A kind of motorized pulleys wing thrust generating means, belong to technical field of aerospace, and more particularly, to a kind of cylinder wing thrust generates
Device.
Background technology
Traditional aircraft is to produce lift, the structure phase of the wing of aircraft and the rotor of helicopter by wing or rotor
Seemingly, their section is aerofoil profile, and the upper and lower surface flowing through the wing by air produces pressure reduction and produces lift, when aerofoil profile determines, it
Produce lift size relevant with the angle of attack, aerofoil size and speed of incoming flow, adjustment lift size be by change the angle of attack, speed
Degree or aerofoil size are realizing.The relative thickness of wing and rotor is all relatively thin, and structural strength is poor.Fixed wing aircraft low speed flies
Row performance is not high, and the wing area of needs is larger.The rotor rotating speed of helicopter is very high could to be produced compared with lift.Traditional propeller
Thrust direction be inconvenient to change.
Content of the invention
The purpose of the present invention is the above-mentioned deficiency overcoming traditional wing, rotor and screw, and invention one kind has more high-strength
The suitable making vertical translation aircraft of degree and the convenient motorized pulleys wing thrust generating means changing thrust direction.
A kind of motorized pulleys wing thrust generating means, including frame, main shaft and be evenly distributed on main axial two, three
Individual or four structure identical rotors, each rotor includes left-hand rotation arm, right-hand rotation arm, motor, drum shaft and the cylinder wing.Main shaft water
Plain cloth is put, and the left end of main shaft and right-hand member are arranged in frame by bearing.All rotors pass through left-hand rotation arm and the right-hand rotation arm of itself
It is arranged on main shaft.The cylinder wing is can be around the cylinder of drum shaft axis flexible rotating.The concrete structure of each rotor is：Left-hand rotation arm
It is parallel to each other with right-hand rotation arm, they are vertical with main shaft to be connected, the cylinder wing and main axis parallel layout, the left and right two ends of drum shaft are respectively
It is arranged on one end away from main shaft of left-hand rotation arm and right-hand rotation arm by bearing.Main shaft, left-hand rotation arm, drum shaft and right-hand rotation arm are in same
In one plane.Motor is arranged on the left end of drum shaft.Controller and battery are furnished with motor.Electronic function drive roller shaft
Rotate and drive the cylinder wing to rotate.The velocity of rotation of the cylinder wing and direction meet SIN function rule.From the left end of main shaft toward right-hand member
Observe, active force from main shaft input, under the drive of main shaft, rotor rotates clockwise, when the cylinder wing is in Far Left this
When the cylinder wing and main shaft with high, the rotation rotating speed of the cylinder wing is zero；Make counterclockwise certainly in the drive bottom roll wing of motor
Turn, with the rotation of main shaft, the cylinder wing revolves round the sun clockwise around main shaft, and the rotation rotating speed of the cylinder wing is gradually increased, when the cylinder wing
Revolve round the sun maximum to the rotation rotating speed of cylinder wing during highest point；Being rotated further then as main shaft, under the rotation rotating speed of the cylinder wing
Fall, is in the rotation rotating speed vanishing of cylinder wing when rightmost is in same level height with main shaft to the cylinder wing；Next, rolling
The cylinder wing continues to revolve round the sun clockwise under the drive of main shaft, makees clockwise direction rotation in the drive bottom roll wing of motor, with
The rotation of main shaft, the cylinder wing revolves round the sun clockwise around main shaft, and the rotation rotating speed of the cylinder wing is gradually increased, when the cylinder wing revolves round the sun to
During lower, the rotation rotating speed of the cylinder wing is maximum；Being rotated further then as main shaft, the rotation rotating speed of the cylinder wing declines, to cylinder
The wing is in the rotation rotating speed vanishing of cylinder wing when rightmost is in same level height with main shaft；So complete a job
Cycle.Because, above the horizontal plane crossing main shaft, the sense of rotation of the cylinder wing is counterclockwise；In the horizontal plane crossing main shaft
Lower section, the sense of rotation of the cylinder wing is clockwise.So repeat this course of work, according to Ku Ta-scholar Koffsky liter
Power law can obtain, and this device will produce thrust upwards.
This device can produce thrust, and the big I of thrust passes through to adjust the rotating speed of main shaft and regulation cylinder wing rotation rotating speed is big
Little amplitude is realizing；The direction of thrust can be realized by adjusting the phase place of cylinder wing rotation rotating speed.Easy to use and flexible, can
It is applied to make lift unit on vertical translation aircraft it is also possible to make the thrust device of the sliding aircraft running landing, its principle is also
Can be used as marine propeller.
Brief description
Fig. 1 is a kind of schematic elevation view of the thriving thrust generating means of motorized pulleys of the present invention；Fig. 2 is that the left view of Fig. 1 is shown
It is intended to；Fig. 3 is the schematic diagram of the motorized pulleys wing thrust generating means with four rotors.
In figure, 1- main shaft；The rotation direction instruction of 2- main shaft, 3- rotor, 31- left-hand rotation arm, 32- right-hand rotation arm, 33- is electronic
Machine, 34- drum shaft, the 35- cylinder wing, the rotation direction instruction of the 36- cylinder wing；The movement locus of 4- drum shaft；The 5- cylinder wing
The instruction of revolution direction；6- frame.
Specific embodiment
In conjunction with accompanying drawing, the present invention is illustrated：A kind of motorized pulleys wing thrust generating means, including frame 6,
Main shaft 1 and be evenly distributed on two, three or four structure identical rotors 3 around main shaft 1, each rotor 3 includes turning left
Arm 31, right-hand rotation arm 32, motor 33, drum shaft 34 and the cylinder wing 35.Main shaft 1 is horizontally disposed, and the left end of main shaft 1 and right-hand member pass through
Bearing is arranged in frame 6.All rotors 3 pass through left-hand rotation arm 31 itself and right-hand rotation arm 32 is arranged on main shaft 1.The cylinder wing 35
It is can be around the cylinder of drum shaft 34 axis flexible rotating.The concrete structure of each rotor 3 is：Left-hand rotation arm 31 and right-hand rotation arm 32 are mutual
Parallel, they are vertical with main shaft 1 to be connected, the cylinder wing 35 and main shaft 1 parallel arrangement, and axle is passed through at the left and right two ends of drum shaft 34 respectively
Hold the one end away from main shaft 1 being arranged on left-hand rotation arm 31 and right-hand rotation arm 32.Main shaft 1, left-hand rotation arm 31, drum shaft 34 and right-hand rotation arm 32
It is in same plane.Motor 33 is arranged on the left end of drum shaft 34.Controller and battery are furnished with motor 33.Motor
33 drive roller shaft 34 rotation can drive the cylinder wing 35 to rotate.The velocity of rotation of the cylinder wing 35 and direction meet SIN function rule
Rule.Observe toward right-hand member from the left end of main shaft 1, as shown in Figure 2, active force inputs from main shaft 1, under the drive of main shaft 1, rotor
3 rotate clockwise, when the cylinder wing 35 is in Far Left now the cylinder wing 35 and main shaft 1 with high, certainly the walking around of the cylinder wing 35
Speed is zero；Make counter clockwise direction rotation in the drive bottom roll wing 35 of motor 33, with the rotation of main shaft 1, the cylinder wing 35 encloses
Revolve round the sun clockwise around main shaft 1, the rotation rotating speed of the cylinder wing 35 is gradually increased, the cylinder wing 35 when the cylinder wing 35 revolves round the sun to highest point
Rotation rotating speed maximum；Then as being rotated further of main shaft 1, the rotation rotating speed of the cylinder wing 35 declines, and is in the cylinder wing 35
The rotation rotating speed vanishing of the cylinder wing 35 when rightmost and main shaft 1 are in same level height；Next, the cylinder wing 35 continues
Revolve round the sun clockwise under the drive of main shaft 1, make clockwise direction rotation in the drive bottom roll wing 35 of motor 33, with main shaft 1
Rotation, the cylinder wing 35 revolves round the sun clockwise around main shaft 1, and the rotation rotating speed of the cylinder wing 35 is gradually increased, when the cylinder wing 35 revolves round the sun
Maximum to the rotation rotating speed of the cylinder wing 35 during lowest part；Then as being rotated further of main shaft 1, under the rotation rotating speed of the cylinder wing 35
Fall, is in the rotation rotating speed vanishing of cylinder wing when rightmost is in same level height with main shaft 1 to the cylinder wing 35；So complete
Become a work period.Because, above the horizontal plane crossing main shaft 1, the sense of rotation of the cylinder wing 35 is counterclockwise；
In the lower section of the horizontal plane crossing main shaft 1, the sense of rotation of the cylinder wing 35 is clockwise.So repeat this course of work, root
Can obtain according to Ku Ta-scholar Koffsky lift law, this device will produce thrust upwards.
This device can produce thrust, and the big I of thrust is passed through to adjust the rotating speed of main shaft 1 and adjust the cylinder wing 35 certainly to walk around
The amplitude of fast size is realizing；The direction of thrust can be realized by adjusting the phase place of the cylinder wing 35 rotation rotating speed.Easy to use
Flexibly, can be applicable to make lift unit on vertical translation aircraft it is also possible to make the thrust device of the sliding aircraft running landing, its
Principle also acts as marine propeller.Using this identical and symmetrical device of two structures and the control system adapting to and dynamical system
When system combination makes vertical translation aircraft, the main shaft 1 of two devices is in that " one " font is horizontally arranged, the main shaft 1 of two devices
Rotate is in opposite direction.It is used as the thrust device of the sliding aircraft running landing using two this identical and symmetrical devices of structure
When, two devices are respectively symmetrically the top being arranged on the left and right main lift wing, the main shaft 1 of two devices erect arranged in parallel, two
It is in opposite direction that the main shaft 1 of device rotates.
Claims (2)
1. a kind of motorized pulleys wing thrust generating means it is characterised in that：Including frame（6）, main shaft（1）And it is evenly distributed on master
Axle（1）Two, three or four structure identical rotors of surrounding（3）, each rotor（3）Including left-hand rotation arm（31）, right-hand rotation arm
（32）, motor（33）, drum shaft（34）With the cylinder wing（35）；Main shaft（1）Horizontally disposed, main shaft（1）Left end and right-hand member lead to
Cross bearing and be arranged on frame（6）On；All rotors（3）By the left-hand rotation arm of itself（31）With right-hand rotation arm（32）It is arranged on main shaft
（1）On；Each rotor（3）Concrete structure be：Left-hand rotation arm（31）With right-hand rotation arm（32）It is parallel to each other, they and main shaft（1）Hang down
Direct-connected connect, the cylinder wing（35）With main shaft（1）Parallel arrangement, drum shaft（34）Left and right two ends respectively left-hand rotation is arranged on by bearing
Arm（31）With right-hand rotation arm（32）Away from main shaft（1）One end；Motor（33）It is arranged on drum shaft（34）Left end；Motor
（33）Can drive roller shaft（34）Rotate and drive the cylinder wing（35）Rotate；The cylinder wing（35）Velocity of rotation and direction meet sine
Function rule；During the thrust device of the aircraft being used as sliding race landing using two this identical and symmetrical devices of structure, two
Device is respectively symmetrically the top being arranged on the left and right main lift wing, the main shaft of two devices（1）Erect arranged in parallel, two devices
Main shaft（1）Rotate is in opposite direction.
2. a kind of motorized pulleys wing thrust generating means according to claim 1 it is characterised in that：Motor（33）On join
There are controller and battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610823728.3A CN106379533B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510231781.XA CN104787337B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
| CN201610823728.3A CN106379533B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510231781.XA Division CN104787337B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106379533A true CN106379533A (en) | 2017-02-08 |
| CN106379533B CN106379533B (en) | 2018-08-03 |
Family
ID=53552619
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510231781.XA Active CN104787337B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
| CN201610823728.3A Active CN106379533B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510231781.XA Active CN104787337B (en) | 2015-05-08 | 2015-05-08 | A kind of motorized pulleys wing thrust generating means |
Country Status (1)
| Country | Link |
|---|---|
| CN (2) | CN104787337B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2309401A1 (en) * | 1975-02-27 | 1976-11-26 | Chabonat Marcel | Rotary wing producing lift and thrust - has horizontal blades with pitch control, rotating about horizontal shaft |
| US20040056144A1 (en) * | 2002-09-24 | 2004-03-25 | Bass Steven M. | Dual-flight mode tandem rotor wing |
| CN202071984U (en) * | 2011-05-02 | 2011-12-14 | 刘自拔 | Movable wing airplane with wind wheels at leading edges |
| CN102887225A (en) * | 2012-10-11 | 2013-01-23 | 王志成 | Flapping wing lift force generator with wing frames unidirectionally rotating |
| CN204297056U (en) * | 2014-12-15 | 2015-04-29 | 佛山市神风航空科技有限公司 | A kind of high-lift wing |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2366355Y (en) * | 1999-01-15 | 2000-03-01 | 李世震 | Rotary wings helicopter |
| CN202481314U (en) * | 2012-03-06 | 2012-10-10 | 陈晓春 | Centrifugal air suspending platform |
| CN204021250U (en) * | 2014-07-23 | 2014-12-17 | 陈志石 | A kind of have the round wing unmanned plane blowing wing mechanism |
| CN204297090U (en) * | 2014-12-15 | 2015-04-29 | 佛山市神风航空科技有限公司 | A kind of flat-type flapping wing lift device with stepper motor |
| CN204297058U (en) * | 2014-12-15 | 2015-04-29 | 佛山市神风航空科技有限公司 | A kind of high lift hardware aircraft |
| CN204642156U (en) * | 2015-05-08 | 2015-09-16 | 佛山市神风航空科技有限公司 | A kind of motorized pulleys wing thrust generating apparatus |
-
2015
- 2015-05-08 CN CN201510231781.XA patent/CN104787337B/en active Active
- 2015-05-08 CN CN201610823728.3A patent/CN106379533B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2309401A1 (en) * | 1975-02-27 | 1976-11-26 | Chabonat Marcel | Rotary wing producing lift and thrust - has horizontal blades with pitch control, rotating about horizontal shaft |
| US20040056144A1 (en) * | 2002-09-24 | 2004-03-25 | Bass Steven M. | Dual-flight mode tandem rotor wing |
| CN202071984U (en) * | 2011-05-02 | 2011-12-14 | 刘自拔 | Movable wing airplane with wind wheels at leading edges |
| CN102887225A (en) * | 2012-10-11 | 2013-01-23 | 王志成 | Flapping wing lift force generator with wing frames unidirectionally rotating |
| CN204297056U (en) * | 2014-12-15 | 2015-04-29 | 佛山市神风航空科技有限公司 | A kind of high-lift wing |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104787337A (en) | 2015-07-22 |
| CN104787337B (en) | 2017-01-04 |
| CN106379533B (en) | 2018-08-03 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190523 Address after: 226300 North Four Formations of Tushan Village, Xingdong Town, Tongzhou District, Nantong City, Jiangsu Province Patentee after: NANTONG HUAXIA AIRPLANE ENGINEERING TECHNOLOGY CO., LTD. Address before: 528500 room 402, Fu Wan Jiangwan Road, Hecheng street, Gaoming District, Foshan, Guangdong, China, 78 Patentee before: Shenfeng science and technology of aviation Co., Ltd of Foshan City |
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| TR01 | Transfer of patent right |