Gas turbine prechamber and fuel manifold structure

Claim 2

In a gas turbine engine having a pressurized air plenum, a combustor in said plenum, a source of fuel, a fuel control means remote from said combustor and connected to said fuel source, said fuel control means having a metering mode for metering fuel flow for combustion and a dump mode for purging fuel upon engine shut down to minimize fuel coking, and a generally cylindrical prechamber housing in said plenum defining a prechamber having an inlet exposed to said plenum and an outlet exposed to said combustor and a cylindrical surface therebetween, the improvement comprising, a plurality of delivery heads disposed on said prechamber housing with symmetrical spacing around said cylindrical surface and projecting therethrough into said prechamber, a plurality of identical fuel conduits in said plenum each having a first end and a second end and corresponding in number to the number of said delivery heads, means connecting said fuel conduit first ends to corresponding ones of said delivery heads, each of said fuel conduits wrapping around said prechamber housing and uniting with the others to form a bundle wherein said fuel conduit second ends terminate at successively greater distances from the end of said bundle, a fuel supply pipe having one end connected to said fuel control means and another end enveloping said fuel conduit bundle such that each of said fuel conduit second ends is disposed within said supply pipe, and means in said supply pipe defining a wall around said fuel conduit bundle downstream of the most distant of said fuel conduit second ends relative to the end of said fuel conduit bundle operative to prevent passage of fuel thereacross so that in said fuel control means metering mode equal fuel flow is induced in each of said fuel conduits and so that in said fuel control means dump mode fuel purge in each of said fuel conduits is rapid and complete.

Claim 3

The improvement recited in claim 1 wherein each of said fuel conduits has an internal diameter of between about 0.007 and 0.020 inches and wherein said fuel supply pipe has an internal diameter on the order of about 0.125 inches.

Claim 4

In a gas turbine engine having a pressurized air plenum, a combustor in said plenum, a source of fuel, a fuel control means remote from said combustor and connected to said fuel source, said fuel control means having a metering mode for metering fuel flow for combustion and a dump mode for purging fuel upon engine shut down to minimize fuel coking, a generally cylindrical prechamber housing in said plenum having a cylindrical wall disposed on a longitudinal axis of said combustor, and a center body projecting into said prechamber housing and cooperating with said cylindrical wall in defining an annular prechamber having an inlet exposed to said plenum and an outlet exposed to said combustor, the improvement comprising, a plurality of identical delivery heads disposed on said prechamber housing with symmetrical spacing around said cylindrical wall and projecting therethrough into said prechamber, each of said delivery heads having a flow port operative to direct a flow stream generally tangent to said cylindrical wall, a plurality of identical fuel conduits corresponding in number to the number of said delivery heads each having an internal diameter of between 0.007 and 0.020 inches and a first end and a second end, means connecting said fuel conduit first ends to corresponding ones of said delivery heads, each of said fuel conduits wrapping around said prechamber housing and uniting with the others to form a bundle wherein said fuel conduit second ends terminate at successively greater distances from the end of said bundle, a fuel supply pipe having an internal diameter of about 0.125 inches and one end connected to said fuel control means and another end enveloping said fuel conduit bundle such that each of said fuel conduit second ends is disposed within said supply pipe, and means in said supply pipe defining a wall around said fuel conduit bundle downstream of the most distant of said fuel conduit second ends relative to the end of said fuel conduit bundle operative to prevent passage of fuel thereacross so that in said fuel control means metering mode equal fuel flow is induced in each of said fuel conduits and so that in said fuel control means dump mode fuel purge in each of said fuel conduits is rapid and complete.

Claim 5

In a gas turbine engine having a pressurized air plenum, a combustor in said plenum, a source of fuel, a fuel control means remote from said combustor and connected to said fuel source, said fuel control means having a metering mode for metering fuel flow for combustion and a dump mode for purging fuel upon engine shut down to minimize fuel coking, a generally cylindrical prechamber housing in said plenum having a cylindrical wall disposed on a longitudinal axis of said combustor, and a center body projecting into said prechamber housing and cooperating with said cylindrical wall in defining an annular prechamber having an inlet exposed to said plenum and an outlet exposed to said combustor, the improvement comprising, a plurality of identical delivery heads disposed on said prechamber housing with symmetrical spacing around said cylindrical wall and projecting therethrough into said prechamber, each of said delivery heads having a flow port operative to direct a flow stream generally tangent to said cylindrical wall, a plurality of identical fuel conduits corresponding in number to the number of said delivery heads each having an internal diameter of between 0.007 and 0.020 inches and a first end and a second end, means connecting said fuel conduit first ends to corresponding ones of said delivery heads, each of said fuel conduits wrapping around said prechamber housing and uniting with the others to form a bundle wherein said fuel conduit second ends terminate at successively greater distances from the end of said bundle, a fuel supply pipe having an internal diameter of about 0.125 inches and one end connected to said fuel control means and another end enveloping said fuel conduit bundle such that each of said fuel conduit second ends is disposed within said supply pipe, and means in said supply pipe defining a wall around said fuel conduit bundle downstream of the most distant of said fuel conduit second ends relative to the end of said fuel conduit bundle operative to prevent passage of fuel thereacross so that in said fuel control means metering mode equal fuel flow is induced in each of said fuel conduits and so that in said fuel control means dump mode fuel purge in each of said fuel conduits is rapid and complete.