Gas turbine engine
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United States of America Patent
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Oct 8, 2002
Grant Date -
Oct 24, 2002
app pub date -
Sep 25, 1998
filing date -
Sep 25, 1998
priority date (Note) -
Expired
status (Latency Note)
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Abstract
A gas turbine engine has a device for admitting a rotating fluid flow from an annular space of the casing to the inlet portion of a combustor to form a rotating fluid flow in the inlet portion of the combustor. The rotating fluid flow is formed in the annular space of the casing by supplying a fluid from a compressor to the blades of the turbine rotor disk.
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