发明名称 Hybrid Spinner Support
摘要 A hybrid support ring comprises a suspender and a belt, the suspender defined by a flange and a leg rearwardly extending having a lug, the suspender also extending circumferentially, the suspender formed of a first material, the belt extending circumferentially and disposed in the lug, the belt being formed of a second material.
申请公布号 US2014255203(A1) 申请公布日期 2014.09.11
申请号 US201313763228 申请日期 2013.02.08
申请人 General Electric Company 发明人 Roby Benjamin James;Bishop Michael Jason
分类号 B64C27/54 主分类号 B64C27/54
代理机构 代理人
主权项 1. A hybrid support ring for an aircraft engine, comprising: a suspender and a belt seated in said suspender; a forward flange extending radially and circumferentially; a flow surface having an axial component and extending circumferentially; said flow surface having a first radial location at a first forward end and a second radial location at a second rearward end; said belt extending circumferentially in and engaging a groove of said suspender; said suspender being formed of a first material and said belt being formed of a second distinct material; said flow surface being one of smooth or contoured
地址 US