发明名称 Platform assembly for attaching rotor blades to a rotor disk.
摘要 <p>Nonmetallic airfoil blades (84) are mounted to a rotor disk (38) via a circumferentially spaced array of metal support members (66). Each support member (66) includes a pair or circumferentially spaced arcuate or airfoil shaped dovetail engagement surfaces (90,92). The metal support members (66) are secured to the rotor disk (38) via straight dovetails (68) while the rotor blades (84) are secured to the support members (66) via airfoil shaped dovetails (88). The support members (66) may include hollow portions (78) for channeling cooling air (39) to the airfoil blades (84). &lt;IMAGE&gt;</p>
申请公布号 EP0502660(A1) 申请公布日期 1992.09.09
申请号 EP19920301700 申请日期 1992.02.28
申请人 GENERAL ELECTRIC COMPANY 发明人 CORSMEIER, ROBERT JAMES
分类号 F01D5/18;F01D5/28;F01D5/30;F01D11/00 主分类号 F01D5/18
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