A gas turbine engine augmenter has a gas flowpath. A number of vanes extend into the gas flowpath. A number of augmenter fuel conduits have outlets along at least some of the vanes. At least one burner discharge outlet is along at least one of the vanes for discharging a pilot gas.
申请公布号
US8209987(B2)
申请公布日期
2012.07.03
申请号
US20080323773
申请日期
2008.11.26
申请人
HAUTMAN DONALD J.;COLKET, III MEREDITH B.;LOVETT JEFFERY A.;BROGAN TORENCE P.;UNITED TECHNOLOGIES CORPORATION
发明人
HAUTMAN DONALD J.;COLKET, III MEREDITH B.;LOVETT JEFFERY A.;BROGAN TORENCE P.
