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A combustor assembly for an automotive gas turbine engine includes a continuously ignited, pilot flame tube supported on a combustor dome immediately downstream of an inlet fuel nozzle and air swirler assembly. The pilot flame tube has an air swirler and fuel nozzle supported on an interior bulkhead

A combustor assembly for an automotive gas turbine engine includes a continuously ignited, pilot flame tube supported on a combustor dome immediately downstream of an inlet fuel nozzle and air swirler assembly. The pilot flame tube has an air swirler and fuel nozzle supported on an interior bulkhead and air is supplied upstream of the bulkhead and through a double-walled porous tube assembly for cooling wall portions of the flame tube exposed to the flame front within the combustor and wall portions thereof exposed to a pilot flame formed within the flame tube.

대표청구항 ▼

In an automotive gas turbine engine having fuel flow to a prechamber liner of a combustor for a prevaporization upstream of a combustor wall surrounded by a compressed air source and with the wall defining a primary combustion zone the improvement comprising: a continuously operated pilot flame tube

In an automotive gas turbine engine having fuel flow to a prechamber liner of a combustor for a prevaporization upstream of a combustor wall surrounded by a compressed air source and with the wall defining a primary combustion zone the improvement comprising: a continuously operated pilot flame tube assembly supported on the combustor wall to maintain a continuous ignition flame within the primary combustion zone during engine deceleration, said assembly including a dome located exteriorly of the wall and having an interior bulkhead defining an upstream air space therebetween in communication with said air chamber, a pilot air swirler on said bulkhead including a pilot nozzle for continuously directing fuel and air downstream of said bulkhead for ignition as a continuously burning pilot flame located within said combustor wall for continuously igniting air fuel mixtures within said primary combustion zone, a double-walled open end flame tube surrounding said pilot ignition flame, said flame tube located within said combustor wall and having an outer tubular member of porous material with holes therein and an inner tubular member of porous material with holes therein, said inner tubular member being telescoped within and located in spaced relationship to said outer tubular membeR to form an air passage therebetween upstream of holes in both said tubular members, said inner and outer tubular members having one end thereof sealed together at the open end of said flame tube to prevent air flow axially therefrom into said primary combustion zone, cooling air entrance means to direct compressed air from said air source to the surfaces of said inner and outer tubular members which define said air passage therebetween, said inner tubular member holes receiving air from said air passage for redistributing air as a sheath radially inwardly of said inner tubular member to continuously shield it from said pilot flame, said outer tubular member holes receiving air from said air passage for redistributing air as a sheath radially outwardly through said outer tubular member to shield it against a flame within said combustor primary combustion zone thereby to maintain a continuous pilot flame within said primary combustion zone to prevent flameout therein during engine decelerations wherein air and fuel flows are reduced to the primary combustion zone.