CN104276279A

CN104276279A - S-shaped flight paddle mechanism

Info

Publication number: CN104276279A
Application number: CN201410577114.2A
Authority: CN
Inventors: 任孝忠
Original assignee: Individual
Current assignee: Individual
Priority date: 2014-10-24
Filing date: 2014-10-24
Publication date: 2015-01-14

Abstract

The invention provides an S-shaped flight paddle mechanism which is composed of S-shaped blades arranged on a machine seat, a guide wheel is used for adjusting the angles of two blades under the guide function of a molded line, and the air is continuously compressed from top to bottom, so that the lift force is generated, and a fuselage is driven to lift off by the lift force. The S-shaped flight paddle mechanism can be used for manufacturing an aircraft, and has the characteristics of being simple in structure, low in manufacturing cost, wide in application scope, and the like.

Description

A kind of S-ing blade mechanism

The present invention relates to " a kind of S-ing blade mechanism ".Aircraft originally much all have employed traditional screw propeller and rotates and improve lift, its shortcoming that Here it is.

" a kind of S-ing blade mechanism " proposed by the invention just solves above shortcoming, original " screw propeller ", make the device of " blade of S shape " into, under the effect that track adjusting wheel leads at molded line, make the continuous translation-angle of two panels blade, pressurized air creates lift from top to bottom, just can play the effect of screw propeller.

" a kind of S-ing blade mechanism " provided by the present invention its be a kind of S shape by being located at above support blade combination, under the effect that track adjusting wheel leads at molded line, the angle of adjustment two blades, constantly compresses air from top to bottom and creates the lift-off of lift drive fuselage.

" a kind of S-ing blade mechanism " provided by the present invention, its for a kind of by primary blades 1, A blade 2, lobus dexter sheet turning joint 3, B blade 4, lobus sinister sheet turning joint 5, power input shaft 6, line style 7, A blade guide wheel shaft 8, A Leaf Conductance to wheel bearing bore 9, A blade track adjusting wheel 10, B blade guide wheel shaft 11, B Leaf Conductance to wheel bearing bore 12, B Leaf Conductance to the mechanism formed to wheel 13, fuselage 14, power input shaft hole 15, support 16.Architectural feature of the present invention and object is further illustrated below in conjunction with accompanying drawing.

Brief Description Of Drawings:

Fig. 1 is the main schematic diagram of basic structure of a kind of S-ing blade mechanism provided by the present invention.

Fig. 2 is that the basic structure side of a kind of S-ing blade mechanism provided by the present invention is attempted

Fig. 3, Fig. 4 are rotation 180 ° of action diagram of a kind of S-ing blade mechanism provided by the present invention

See shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4, it mainly drives primary blades 1, A blade 2 and B blade 4 to rotate clockwise at rotary power input shaft 6, at this moment, under the track of line style 7 guides, track adjusting wheel 10 on A blade 2 and the track adjusting wheel 13 on B blade 4 be translation-angle constantly, and when often rotating 180 °, two blades are opened or unifys secondary, make two blades from top to bottom pressurized air time, create lift, continuous rotation makes fuselage 14, support 16 lifts off.

Be somebody's turn to do the manufacture that " a kind of S-ing blade mechanism " can be used for aircraft, structure is simple, manufacturing expense is cheap, the features such as applied range.

Claims

1. a kind of S-ing blade mechanism provided by the present invention its be a kind of S shape by being located at above support blade combination, under the effect that track adjusting wheel leads at molded line, the angle of adjustment two blades, constantly compresses air from top to bottom and creates the lift-off of lift drive fuselage.

2. a kind of S-ing blade mechanism according to claim 1 its for a kind of by primary blades 1, A blade 2, lobus dexter sheet turning joint 3, B blade 4, lobus sinister sheet turning joint 5, power input shaft 6, line style 7, A blade guide wheel shaft 8, A Leaf Conductance to wheel bearing bore 9, A blade track adjusting wheel 10, B blade guide wheel shaft 11, B Leaf Conductance to wheel bearing bore 12, B Leaf Conductance to the mechanism formed to wheel 13, fuselage 14, power input shaft hole 15, support 16.It is characterized in that being combined by the blade of the S shape be located at above support, under the effect that track adjusting wheel leads at molded line, the angle of adjustment two blades, constantly compresses air from top to bottom and creates lift and drive fuselage lift-off.

3. a kind of S-ing blade mechanism according to claim 2 is below in conjunction with Brief Description Of Drawings:

Fig. 3, Fig. 4 are rotation 180 ° of action diagram of a kind of S-ing blade mechanism provided by the present invention.

4. a kind of S-ing blade mechanism according to claim 3 sees shown in Fig. 1, Fig. 2, Fig. 3, Fig. 4, it mainly drives primary blades 1, A blade 2 and B blade 4 to rotate clockwise at rotary power input shaft 6, at this moment, under the track of line style 7 guides, track adjusting wheel 10 on A blade 2 and the track adjusting wheel 13 on B blade 4 constantly translation-angle, often during rotation 180 °, two blades are opened or unify secondary, make two blades from top to bottom pressurized air time, create lift, continuous rotation makes fuselage 14, support 16 lifts off.

5. a kind of S-ing blade mechanism according to claim 4 can Multiple Combination to reach scope and the requirement of design.