Apparatus for controlling cooling air in gas turbine engine

Power plants – Combustion products used as motive fluid – Combustion products generator

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415115, F02C 712

Patent

active

060677929

ABSTRACT:
In a gas turbine engine, compressor delivery air is fed into air inlets in hollow turbine nozzle guide vanes, and then ejected into the gas stream via holes in the vane walls. Valving is provided so as to provide modulation of the cooling airflow over and above the modulation achieved by compressor output when it changes with engine power setting. Excessive cooling of the gas stream is thus prevented.

REFERENCES:
patent: 4709546 (1987-12-01), Weiler
patent: 4785624 (1988-11-01), Smith et al.
patent: 4807433 (1989-02-01), Maclin et al.
patent: 5157914 (1992-10-01), Schwarz et al.

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