发明名称 Thermal gradient tolerant turbomachine coupling member
摘要 An exemplary turbomachine securing apparatus includes a coupling member (70) that couples a first component (50) to a second component (60) within a turbomachine. The first component (50) and the second component (60) are both non-rotating components during operation of the turbomachine. The coupling member (70) limits relative circumferential movement between the first component (50) and the second component (60), and permits relative radial movement. It may comprise a Hirth coupling.
申请公布号 EP2597272(A3) 申请公布日期 2016.09.14
申请号 EP20120192539 申请日期 2012.11.14
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 HUDSON, ERIC A.
分类号 F01D25/16;F02C7/36 主分类号 F01D25/16
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