Engine power extraction control system

Details Engine power extraction control system Engine power extraction control system

B - Operations, Transporting

64

D

B64D 41/00 (2006.01) B64D 31/00 (2006.01)

Patent

CA 2516884

An engine power extraction control system controls the main propulsion engines and the electrical machines that are coupled thereto to supply an appropriate amount of aircraft thrust and electrical energy to the aircraft. The engines and electrical machines are also controlled so that the propulsion thrust that is generated is split between the various turbines in the main propulsion engines to maintain an adequate surge margin and to minimize residual thrust generation.

Un système de gestion d'extraction de puissance de moteurs commande les principaux moteurs de propulsion et les machines électriques accouplés pour fournir une quantité appropriée de poussée à un aéronef et l'énergie électrique à l'aéronef. Les moteurs et les machines électriques sont aussi gérés de sorte que la poussée propulsive produite est divisée entre les diverses turbines dans les principaux moteurs de propulsion pour maintenir une marge de pompage appropriée et pour minimiser la production de poussée résiduelle.

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