Gas turbine engine for controlling stall margin

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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60 395, 415148, F02C 304, F02C 700

Patent

active

053015002

ABSTRACT:
An industrial gas turbine engine includes in serial flow relationship a booster compressor, core engine, power turbine, and flow channel, with the power turbine having a first shaft, joined to the booster compressor, and an output shaft, and the flow channel having an outlet. Means for selectively varying flow area of the channel outlet are provided for controlling stall margin of the booster compressor in an exemplary embodiment of the engine and method of operation. The flow area varying means is effective for providing a minimum area of the channel outlet for controlling booster compressor stall margin at least at a synchronous speed associated with powering an electrical generator. In one embodiment, the flow area varying means effects a minimum horsepower from the output shaft for allowing lock-on and lock-off of the electrical generator at synchronous speed. In another embodiment of the invention, the flow area varying means is effective for braking the electrical generator during a full power stopcock rollback.

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