<p>A gas turbine engine fueling system (60) includes a number of spray bars (64) having conduits (66, 68) extending through associated vanes (36). A number of fuel injector nozzles (80) are along each conduit (66, 68). Each of the nozzles (80) are positioned to discharge an associated fuel stream from one of the sides (46, 48) of the associated vane (36). A number of wear members (82) are each mounted relative to the associated one of the nozzles (80) for a range of motion relative thereto. The wear members (82) movably cooperate with the associated vane (36) to accommodate operating deflection and/or tolerances of the spray bars (64) and vanes (36).</p>
申请公布号
EP1741983(A2)
申请公布日期
2007.01.10
申请号
EP20060252285
申请日期
2006.04.28
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
MULDOON, MARC J.;SHERWOOD, TOR W.;HARRIS, MEGGAN H.;BROOKS, ROBERT T.