CN109649638A - It is coaxial to turn double cycloid paddle together - Google Patents
It is coaxial to turn double cycloid paddle together Download PDFInfo
- Publication number
- CN109649638A CN109649638A CN201910000808.2A CN201910000808A CN109649638A CN 109649638 A CN109649638 A CN 109649638A CN 201910000808 A CN201910000808 A CN 201910000808A CN 109649638 A CN109649638 A CN 109649638A
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- China
- Prior art keywords
- paddle
- steering engine
- cycloid
- cycloidal
- hypocycloid
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
本发明提供了一种共轴同转双摆线桨，包括摆线桨操纵机构以及在摆线桨操纵机构控制下绕传动轴共轴同向旋转的外摆线桨和内摆线桨，所述的外摆线桨和内摆线桨均由八片摆线桨叶片组成，外摆线桨通过外侧摆线桨固定板与旋转轴固定，内摆线桨通过内侧摆线桨固定板与旋转轴固定，外摆线桨安装在内摆线桨外侧，相邻的外摆线桨叶片和内摆线桨叶片之间通过桨叶连杆连接形成摆线桨组，实现外摆线桨和内摆线桨的联动。本发明设计有内外两套摆线桨，同时内外摆线桨同向旋转，减少气动干扰，与相同尺寸单摆线桨相比能产生更大的升力。
The invention provides a coaxial co-rotating double cycloid paddle, comprising a cycloidal paddle control mechanism, and an epicycloid paddle and a hypocycloidal paddle coaxially rotated around a transmission shaft under the control of the cycloidal paddle control mechanism. The epicycloidal paddle and the hypocycloidal paddle described above are both composed of eight cycloidal paddle blades, the epicycloidal paddle is fixed to the rotating shaft by the outer cycloidal paddle fixing plate, and the hypocycloidal paddle is connected to the rotating shaft by the inner cycloidal paddle fixing plate. The shaft is fixed, the epicycloidal propeller is installed on the outside of the inner cycloidal propeller, and the adjacent epicycloidal propeller blades and the inner cycloidal propeller blades are connected by the blade connecting rod to form a cycloidal propeller group, realizing the outer cycloidal propeller and the inner cycloidal propeller. Cycloidal paddle linkage. The present invention is designed with two sets of cycloid paddles inside and outside, and the inner and outer cycloid paddles rotate in the same direction at the same time, so as to reduce aerodynamic interference, and can generate larger lift force than monocycloidal paddles of the same size.
Description
Technical field
It is specifically a kind of coaxial with turning double cycloid paddle the present invention relates to cycloid propeller, wing control system regions.
Background technique
Cycloid propeller is a kind of device of novel generation aerodynamic lift, and blade is while around the revolution of cycloid propeller shaft also around hinge
Chain does vertical dip mining movement, provides lift by the angle of attack of different location blade in cyclomorphosis rotary blade system, passes through
It controls the phase angle of cycloid propeller blade cyclic pitch and then changes net vector direction of pull, since the period rotation of cycloid propeller is brought
Nonstationary flow dynamic characteristic, increase the stalling angle of blade so that cycloid propeller have it is high-efficient, noise is low, vectored thrust become
Change the features such as fast.
The Chinese patent of Publication No. CN103434627A discloses the pendulum using a kind of rocker arm sliding block as control mechanism
Line paddle.The purpose of the invention is the reliability for avoiding trying to improve mechanism using conventional cam mechanism and the mechanical effect of raising
Rate, the control mechanism in the patent be by using in mechanism the fixed upright bar of inner ring and transmitting lateral displacement；In sliding block drives
Ring lateral displacement makes blade obtain deflection angle, and inner ring, which circumferentially rotates, makes blade obtain phase angle, the cycloid propeller control in the patent
Mechanism is relative complex, while overall mechanism is huge, heavy, is only applicable to study cycloid propeller aerodynamic characteristic as experiment porch, no
It is suitble to aircraft.
By the United States Patent (USP) NO.6/939 of valley western work great Hu et al. application, 888 (publication number GB939888 (A)) are mentioned
It is a kind of to control vertical axis propeller eccentric circle mechanism using pitch.The mechanism controls the inclination angle of side plate and a series of by steering engine
Link transmission, to realize the control to blade pitch angles.The control mechanism has the response that is exceedingly fast, lighter weight, and at
Function applies to miniature cycloid propeller unmanned plane.But the solution is more due to contacting between component, causes mechanical loss larger.
Currently, cycloid propeller is typically designed as single cycloid propeller, if the coaxial design thought of coaxal helicopter is applied to pendulum
In the design of line paddle, cycloid propeller is designed as inside and outside two sets of blades, the pneumatic efficiency of cycloid propeller is can be further improved, enhances cycloid
The practicability of paddle.
Summary of the invention
The present invention in order to solve problems in the prior art, provides a kind of coaxial with double cycloid paddle is turned, and design has inside and outside two
Cycloid propeller, while internal and external cycloids paddle rotating Vortex are covered, aerodynamic interference is reduced, can be generated compared with identical size list cycloid propeller bigger
Lift.
The present invention include cycloid propeller operating mechanism and cycloid propeller operating mechanism control under around the coaxial rotation in the same direction of transmission shaft
The epicycloid paddle and hypocycloid paddle turned, the epicycloid paddle and hypocycloid paddle are made of eight cycloidal oar blades, epicycloid
Paddle is fixed by outside cycloid propeller fixed plate with rotary shaft, and hypocycloid paddle is fixed by inside cycloid propeller fixed plate with rotary shaft,
Epicycloid paddle is mounted on the outside of hypocycloid paddle, is connected between adjacent epicycloid paddle blade and hypocycloid paddle blade by blade connecting rod
It connects to form cycloid propeller group, realizes the linkage of epicycloid paddle and hypocycloid paddle.
It is further improved, the cycloid propeller operating mechanism includes control link, l-shaped rod, inclinator connecting rod, and connecting rod inclines
Oblique device, steering engine fixed plate and steering engine group, wherein steering engine group is fixed by steering engine fixed plate, and steering engine group controls inclinator by connecting rod
Movement, the movement of inclinator is by the cooperative movement of eight groups of inclinator connecting rods and l-shaped rod to the fortune of eight control links of control
Dynamic, every connecting rod is connect with a hypocycloid paddle, controls the change in angle of attack of the hypocycloid paddle.
It is further improved, the steering engine fixed plate includes the first steering engine fixed plate and the second steering engine fixed plate, and two pieces solid
Steering engine group is clipped in the middle by fixed board；Steering engine group includes identical first steering engine, the second steering engine and third steering engine.
The cycloid propeller operating mechanism mainly by steering engine group provide steering force, and by inclinator control sheet cycloid propeller always away from
It is operated with feathering.
The beneficial effects of the invention are that:
1, coaxial with double cycloid paddle is turned, design has inside and outside two sets of cycloid propellers, can generate compared with identical size list cycloid propeller bigger
Lift.
2, cycloidal propeller control mechanism proposed by the present invention is simple with structure, response is fast, transmission efficiency is high and light-weight
Advantage.
3, mechanism of the present invention has fast response, and no sluggishness, when the variation of eccentricity small range, blade pitch angles can be fast
Speed improves.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention.
Fig. 2 is cycloid propeller operating mechanism structural schematic diagram.
Specific embodiment
The present invention will be further explained below with reference to the attached drawings.
Structure of the invention as shown in Figure 1, include cycloid propeller operating mechanism and cycloid propeller operating mechanism control under around biography
The epicycloid paddle 1 and hypocycloid paddle 2 of the coaxial rotating Vortex of moving axis 4, the epicycloid paddle 1 and hypocycloid paddle 2 are put by eight
Line paddle blade composition, epicycloid paddle 1 is fixed by outside cycloid propeller fixed plate 7 and rotary shaft 4, and hypocycloid paddle 2 passes through interior side-sway
Line paddle fixed plate 3 is fixed with rotary shaft, and epicycloid paddle 1 is mounted on the outside of hypocycloid paddle 2, adjacent 1 blade of epicycloid paddle and interior
Cycloid propeller group is formed by the connection of blade connecting rod 5 between 2 blade of cycloid propeller, realizes the linkage of epicycloid paddle 1 and hypocycloid paddle 2.
The cycloid propeller operating mechanism is as shown in Fig. 2, include control link 6, l-shaped rod 8, inclinator connecting rod 9, connecting rod
10, inclinator 11, steering engine fixed plate and steering engine group, wherein steering engine group is fixed by steering engine fixed plate, and steering engine group passes through connecting rod 10
It controls inclinator 11 to move, the movement of inclinator 11 passes through eight groups of inclinator connecting rods 9 with the cooperative movement of l-shaped rod 8 to control
The movement of eight control links 6, every connecting rod 6 are connect with a hypocycloid paddle 2, control the change in angle of attack of the hypocycloid paddle 2.
The steering engine fixed plate includes the first steering engine fixed plate 12 and the second steering engine fixed plate 13, and two fixed plates are by rudder
Unit is clipped in the middle.Steering engine group includes identical first steering engine 14, the second steering engine 16 and third steering engine 17.
The cycloid propeller operating mechanism mainly provides steering force by steering engine group, and controls 8 cycloid propellers by inclinator 11
Always away from being operated with feathering.
There are many concrete application approach of the present invention, the above is only a preferred embodiment of the present invention, it is noted that for
For those skilled in the art, without departing from the principle of the present invention, it can also make several improvements, this
A little improve also should be regarded as protection scope of the present invention.
Claims (3)
1. one kind is coaxial to turn together double cycloid paddle, it is characterised in that: including cycloid propeller operating mechanism and in cycloid propeller operating mechanism
Around the epicycloid paddle and hypocycloid paddle of the coaxial rotating Vortex of transmission shaft under control, the epicycloid paddle and hypocycloid paddle are by eight
Piece cycloidal oar blade composition, epicycloid paddle are fixed by outside cycloid propeller fixed plate with rotary shaft, and hypocycloid paddle passes through interior side-sway
Line paddle fixed plate is fixed with rotary shaft, and epicycloid paddle is mounted on the outside of hypocycloid paddle, adjacent epicycloid paddle blade and hypocycloid
It connects to form cycloid propeller group by blade connecting rod between paddle blade, realizes the linkage of epicycloid paddle and hypocycloid paddle.
2. according to claim 1 coaxial with turning double cycloid paddle, it is characterised in that: the cycloid propeller operating mechanism includes
Control link, l-shaped rod, inclinator connecting rod, connecting rod, inclinator, steering engine fixed plate and steering engine group, wherein steering engine group is solid by steering engine
Fixed board is fixed, and steering engine group controls inclinator by connecting rod and moves, and the movement of inclinator passes through eight groups of inclinator connecting rods and l-shaped rod
To control the movement of eight control links, every connecting rod is connect cooperative movement with a hypocycloid paddle, controls the hypocycloid paddle
Change in angle of attack.
3. according to claim 1 coaxial with turning double cycloid paddle, it is characterised in that: the steering engine fixed plate includes first
Steering engine group is clipped in the middle by steering engine fixed plate and the second steering engine fixed plate, two fixed plates；Steering engine group includes identical
One steering engine, the second steering engine and third steering engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910000808.2A CN109649638A (en) | 2019-01-02 | 2019-01-02 | It is coaxial to turn double cycloid paddle together |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910000808.2A CN109649638A (en) | 2019-01-02 | 2019-01-02 | It is coaxial to turn double cycloid paddle together |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109649638A true CN109649638A (en) | 2019-04-19 |
Family
ID=66118706
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910000808.2A Pending CN109649638A (en) | 2019-01-02 | 2019-01-02 | It is coaxial to turn double cycloid paddle together |
Country Status (1)
| Country | Link |
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| CN (1) | CN109649638A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5462406A (en) * | 1993-08-19 | 1995-10-31 | Vitron Systems Inc. | Cyclodial propulsion system |
| KR20050034485A (en) * | 2003-10-09 | 2005-04-14 | 재단법인서울대학교산학협력재단 | A vertical takeoff and landing aircraft |
| US20050082422A1 (en) * | 2003-10-21 | 2005-04-21 | Tierney Glenn M. | Cycloidal VTOL UAV |
| KR20110010241A (en) * | 2009-07-24 | 2011-02-01 | 최홍곤 | Wind power generator that implements multi-cycloidal curve system with eccentric shaft |
| CN103434627A (en) * | 2013-08-30 | 2013-12-11 | 西北工业大学 | Automatic control mechanism of rocker sliding block type cycloid paddle |
| CN107628245A (en) * | 2017-10-24 | 2018-01-26 | 陈晓春 | Sheave commutation type rotary flapping wing power plant system |
| CN109018342A (en) * | 2018-08-24 | 2018-12-18 | 南京航空航天大学 | One kind is verted cycloid fan swing device, vert cycloid fan rotor aircraft and its control method |
| CN210258813U (en) * | 2019-01-02 | 2020-04-07 | 南京航空航天大学 | Coaxial co-rotating double-cycloid paddle |
-
2019
- 2019-01-02 CN CN201910000808.2A patent/CN109649638A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5462406A (en) * | 1993-08-19 | 1995-10-31 | Vitron Systems Inc. | Cyclodial propulsion system |
| KR20050034485A (en) * | 2003-10-09 | 2005-04-14 | 재단법인서울대학교산학협력재단 | A vertical takeoff and landing aircraft |
| US20050082422A1 (en) * | 2003-10-21 | 2005-04-21 | Tierney Glenn M. | Cycloidal VTOL UAV |
| KR20110010241A (en) * | 2009-07-24 | 2011-02-01 | 최홍곤 | Wind power generator that implements multi-cycloidal curve system with eccentric shaft |
| CN103434627A (en) * | 2013-08-30 | 2013-12-11 | 西北工业大学 | Automatic control mechanism of rocker sliding block type cycloid paddle |
| CN107628245A (en) * | 2017-10-24 | 2018-01-26 | 陈晓春 | Sheave commutation type rotary flapping wing power plant system |
| CN109018342A (en) * | 2018-08-24 | 2018-12-18 | 南京航空航天大学 | One kind is verted cycloid fan swing device, vert cycloid fan rotor aircraft and its control method |
| CN210258813U (en) * | 2019-01-02 | 2020-04-07 | 南京航空航天大学 | Coaxial co-rotating double-cycloid paddle |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190419 |
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| RJ01 | Rejection of invention patent application after publication |