Turbine engine combustor without air film cooling
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United States of America Patent
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Dec 29, 1992
Issued Date -
N/A
app pub date -
Sep 23, 1991
filing date -
Dec 11, 1989
priority date (Note) -
Expired
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Abstract
Difficulties in cooling the shrouds (32, 34) and the nozzle (38) of an air breathing gas turbine are minimized or eliminated through the use of a generally toroidal, annular combustor (44) having an outlet (48) and combustion air inlets (90A, 90B) and otherwise being imperforate or free of any means for the admission of cooling air to the interior of the combustor (44).
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