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The "All-in-One" Coaxial Helicopter Flight Control relates to a mechanical control mixer system integrating all the controlling input orders of the pilot to control the flight patterns of a coaxial rotor helicopter.

In particular by controlling the degrees of pitch changes of a coaxial rotor device:

- Collective Pitch
- Cyclic Pitch
- Differential Pitch


These controlling inputs are transmitted in equal and simultaneous values on the two counter-rotating rotors.

Diagrams below shows the entire coaxial swashplate control link couplings.  As seen, the "All-in-One" system is coupled and installed under the gearbox of the Coaxial Drive System (CDS).

Advantages of this "All-in-One" System:

- Very compact
- All links are straightforward & redundant for security
- High precision input order transmissions
- No parasite effects in control orders mixing
- Built-in automatic throttle compensation maintaining constant rotor RPM for Collective control
- Built-in automatic collective pitch compensation maintaining constant altitude level for Yaw control

   

The EzyCopter Control Link System Parts & Components

The All-in-One Coaxial Helicopter Flight Control Link System is Patent Pending. 

ALL RIGHTS RESERVED.

Diagram 1

Diagram 2

 

Diagram 3

 

 

 

祐祥直升飛機股份有限公司 / 台中市中部科學園區科園一路5 

E-Mail: clin@mail.com / ezycopter@yoshine.com  

Tel: (04) 2462-7889  Fax: (04) 2463- 9165

  Copyright © 2007/2008. All rights reserved.

Last Modified :12.23.2007