Thermal management system for turbomachinery
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United States of America Patent
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N/A
Issued Date -
Aug 15, 2002
app pub date -
Dec 21, 2001
filing date -
Feb 14, 2001
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
A gas turbine engine thermal management system. In one form an atomized cooling agent is delivered into a non primary gas flow path. A portion of compressor bleed air is passed into the non primary gas flow path. The compressor bleed air and atomized cooling agent function to cool components within the engine.
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