Turbine engine combustor without air film cooling

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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60760, F02C 305

Patent

active

051741083

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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