发明名称 Thrust bearing housing for a gas turbine engine
摘要 A thrust bearing housing (20) comprises two opposite annular end members (36,38) and a cone member (34) extending between the two end members. The cone member is connected to each end member at a circular junction (42,44), each circular junction having a medial line which borders a respective end of a virtual conical surface (50). At least a major portion of the cone member (34) is provided inside the virtual conical surface (50).
申请公布号 EP1900910(B1) 申请公布日期 2015.01.28
申请号 EP20070253526 申请日期 2007.09.06
申请人 PRATT & WHITNEY CANADA CORP. 发明人 GILLESPIE, CHRISTOPHER
分类号 F01D25/16;F16C19/10 主分类号 F01D25/16
代理机构 代理人
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