Gas turbine engine with compressor bleed valve including at least two open positions
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United States of America Patent
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-
Feb 15, 2022
Grant Date -
Sep 17, 2020
app pub date -
May 2, 2019
filing date -
May 31, 2018
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A gas turbine engine comprising: a compressor; a first turbine; and a first compressor bleed valve in fluid communication with the compressor and configured to release bleed air from the compressor; wherein the first compressor bleed valve is configured to release bleed air to a downstream location in the engine, the downstream location being downstream of the first turbine; wherein the first compressor bleed valve is configured to open wherein the first compressor bleed valve is configured to open to at least two positions, to thereby release a variable amount of bleed air from the compressor.
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