Gas turbine set
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United States of America Patent
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Dec 5, 2006
Issued Date -
N/A
app pub date -
Aug 7, 2003
filing date -
Nov 2, 2001
priority date (Note) -
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Abstract
A gas turbine set, with a cooling air system through which at least one cooling air mass flow flows from a compressor to thermally highly loaded components of the gas turbine set. Pressure increasing ejectors are arranged in a cooling air duct of the cooling air system for increasing the pressure of flowing cooling air. The ejectors are operable with a working fluid. The working fluid mass flow is less than twenty percent of a driven cooling air mass flow.
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