专利名称：Turbine engine combustor发明人：Curtis C. Cowan申请号：US11869273申请日：20071009公开号：US08020366B2公开日：20110920
专利附图：
摘要：A gas turbine engine is piloted with a pilot flow of fuel delivered to a combustoras a liquid. A first additional flow of the fuel is also delivered to the combustor as a liquid.A second additional flow of the fuel is vaporized and delivered to the combustor as avapor. A fuel injector may have passageways associated with each of the three flows.
申请人：Curtis C. Cowan
地址：East Hampton CT US
国籍：US
代理机构：Bachman & LaPointe, P.C.
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