发明名称 Guide vane assembly
摘要 <p>A vane assembly (60) for a gas turbine engine includes at least one vane that includes a first body (62), a second body (64), and a passageway (94). The first body includes a first sidewall (66) and a second sidewall (68) that are connected at a leading edge (70) and a trailing edge (72). The passageway extends between the second body and the first body leading edge. <IMAGE></p>
申请公布号 EP1298286(A2) 申请公布日期 2003.04.02
申请号 EP20020256477 申请日期 2002.09.18
申请人 GENERAL ELECTRIC COMPANY 发明人 KOSHOFFER, JOHN MICHAEL;DRAKE, KEVIN ROBERT
分类号 F01D25/30;F01D5/14;F01D9/04;F02C7/00;F02K3/10;(IPC1-7):F01D9/04;B64C3/00 主分类号 F01D25/30
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