Description of hydraulic actuator units operating control surfaces of British Aircraft Corp/Sud Aviation Concorde Supersonic transport airliner; control system comprises eight power units for operating elevons and upper and lower rudder sections; three hydraulic relay control units identified as pitch, roll and yaw relays are described; each power control unit is fed from three hydraulic supplies provided by engine driven pump systems operating at 4000 psi.
Concorde power controls
Fluid Power Int
Fluid Power International ; 32 , n 373
1967
3 pages
Article (Journal)
English
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Propulsion controls on concorde
Engineering Index Backfile | 1966
|Engineering Index Backfile | 1966
TIBKAT | 1991
|Online Contents | 2002
|SLUB | 2009
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