A fuel system for a gas turbine engine comprises an injector disposed to inject fuel and air into a combustor of the gas turbine engine. In a first embodiment, the fuel system further comprises an air separation module configured to supply oxygen-enriched air into the combustor via the injector for combustion. In a second embodiment, the fuel system further comprises a barbotage system and a heating element. The barbotage system is configured to feed hydrogen to the injector, and the heating element is configured to pre-heat the fuel.
申请公布号
WO2015050601(A3)
申请公布日期
2015.06.11
申请号
WO2014US43868
申请日期
2014.06.24
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
RIBAROV, LUBOMIR, A.;LISCINSKY, DAVID, S.;COLKET, MEREDITH, B. III