Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
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United States of America Patent
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Jan 30, 2018
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N/A
app pub date -
Dec 31, 2012
filing date -
Sep 27, 2012
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Abstract
A gas turbine engine has a compressor section received within an inner housing. An is an outer housing is spaced radially outwardly of the inner core housing. A nacelle has an anti-icing system which taps compressed air from the compressor section through an anti-ice valve and to the nacelle. The anti-ice valve is opened at startup of the gas turbine engine to assist compressor stability.
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