发明名称 A gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger
摘要 <p>Disclosed is a structural frame (38) for a gas turbine (10) engine comprising an integral fluid reservoir (60) and air/fluid heat exchanger (68;168;268). A central hub (56) includes a reservoir (60) for storing a fluid and an outer rim (62) circumscribes the hub (56). A heat exchanger (68;168;268) is fluidly coupled to the reservoir (60) and is in simultaneous communication with the fluid and an air stream.</p>
申请公布号 EP1630358(A2) 申请公布日期 2006.03.01
申请号 EP20050255275 申请日期 2005.08.26
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 WALKER, HERBERT L.;AKERLEY, STEVAN W.
分类号 F01D25/18;F01D9/06;F02C7/06 主分类号 F01D25/18
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