Speed modification system for gas turbine engine to allow...

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 9/28 (2006.01)

Patent

CA 2336601

The present invention provides a fan speed indication system enabling the operator to control engine rotational speed to match specific thrust performance to flight requirements. The invention accommodates variations in engine thrust performance measured at manufacture or overhaul. In one embodiment, the invention provides an analog speed signal to flight control apparatus. The invention may also be configured to provide a digital speed signal to engine power management control apparatus.

Système d'indication du régime de la soufflante, qui permet à l'opérateur de réguler la vitesse de rotation du moteur de manière à faire correspondre la performance de poussée spécifique aux exigences de vol. La présente invention permet l'adaptation aux variations de la performance de poussée du moteur mesurée lors de la fabrication ou de la révision. Dans un mode de réalisation, ledit système fournit un signal de vitesse analogique à l'appareil de commande de vol. Ledit système peut également être configuré pour fournir un signal de vitesse numérique à l'appareil de commande de gestion de la puissance du moteur.

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