Methods and apparatus for operating gas turbine engines

Power plants – Reaction motor – Method of operation

Reexamination Certificate

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C060S224000, C060S226100

Reexamination Certificate

active

06968674

ABSTRACT:
A method facilitates operating a gas turbine engine assembly including a propelling engine and an auxiliary power engine. The method comprises channeling a portion of airflow entering an inlet to the propelling gas turbine engine through a fan assembly and a bypass duct such that the air bypasses the core engine, and channeling a portion of airflow from the bypass duct towards the auxiliary power engine.

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patent: 6415597 (2002-07-01), Futamura et al.
patent: 6457305 (2002-10-01), Schierbaum
patent: 6634596 (2003-10-01), Albero et al.

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