Gas turbine engine electromechanical variable inlet guide...

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Reexamination Certificate

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Details

C060S794000, C415S042000, C415S150000

Reexamination Certificate

active

07096657

ABSTRACT:
An electromechanical inlet guide vane actuation system includes one or more electric motor driven actuators that are used to appropriately position the inlet guide vanes in a gas turbine engine. The actuation system includes a control circuit that supplies guide vane actuation control signals in response to guide vane position command signals it receives. The guide vane actuation control signals are supplied to one or more electric motors, which position actuators, and thus the inlet guide vanes, to the commanded position.

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TRW Aeronautical Systems, ITP Rolls-Royce Variable State Vane Digital Mock Up, 2002.
PCT International Search Report PCT/US2004/043268 Feb. 2, 2006.

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