Flameholder for gas turbine engine afterburner

Claim 2

A flameholder for reducing screech in gas turbine engines comprising: an elongated V-shaped member having a pair of opposing elongated walls joined at one end and diverging to respective trailing edges, the apex of said elongated V-shaped member facing upstream; and a plurality of vortex creating members extending from each of the trailing edges in a downstream direction, each vortex creating member extending from one trailing edge aligned between vortex creating members on the opposing trailing edge so that opposing spanwise vortices originating at opposing elongated walls originate at different distances downstream from the apex of the V-shaped member and each vortex creating member can provide streamwise vortices between the spanwise vortices.

Claim 3

The flameholder of claim 1 wherein said plurality of vortex creating members comprises generally rectangular spaced apart projections on each trailing edge, with the generally rectangular projections on one trailing edge staggered relative to the generally rectangular projections on the opposing trailing edge.

Claim 4

The flameholder of claim 2 wherein said generally rectangular projections are uniformly spaced apart.

Claim 5

The flameholder of claim 3 wherein the ratio of the depth of the rectangular projection to the width of the rectangular projection is approximately 1 to 2.

Claim 6

An afterburner flameholder for a gas turbine engine, said engine including a central diffuser cone, an outer shell and fuel injection means between the shell and the cone defining an afterburner region, said flameholder comprising: a V-shaped annular member adapted to be secured to the engine in the afterburner region between the shell and cone, said V-shaped annular member having a pair of opposing annular walls joined at one end and diverging to respective trailing edges, the apex of the V-shaped annular member facing upstream toward the fuel injection means; and a plurality of spaced apart generally rectangular projections extending from each of the trailing edges, each generally rectangular projection extending from one trailing edge aligned between rectangular projections on the opposing trailing edge so that opposing spanwise vortices originating at opposing annular walls originate at different distances downstream from the apex of the V-shaped member and each generally rectangular projection can provide streamwise vortices between the spanwise vortices.

Claim 7

An afterburner flameholder for a gas turbine engine, said engine including a central diffuser cone, an outer shell and fuel injection means between the shell and the cone defining an afterburner region, said flameholder comprising: a V-shaped annular member adapted to be secured to the engine in the afterburner region between the shell and cone, said V-shaped annular member having a pair of opposing annular walls joined at one end and diverging to respective trailing edges, the apex of the V-shaped annular member facing upstream toward the fuel injection means; and a plurality of spaced apart generally rectangular projections extending from each of the trailing edges, each generally rectangular projection extending from one trailing edge aligned between rectangular projections on the opposing trailing edge so that opposing spanwise vortices originating at opposing annular walls originate at different distances downstream from the apex of the V-shaped member and each generally rectangular projection can provide streamwise vortices between the spanwise vortices.

Claim 8

The flameholder of claim 5 wherein said generally rectangular projections are uniformly spaced apart.

Claim 9

The flameholder of claim 6 wherein the ratio of the depth of the rectangular projection to the width of the rectangular projection is approximately 1 to 2.