发明名称 Annular Cover Delimiting a Turbomachine Lubrication Chamber
摘要 The present application relates to an annular cover for a lubrication chamber of a rotary bearing of a turbomachine. The cover includes a wall that is generally circular and flared with an orifice that is designed to receive a transmission shaft opposite an assembly surface for the cover, and at least one duct communicating with the inside of the wall and extending along the wall as far as the assembly surface. The duct is formed in the thickness of the body of the wall which is made from the same material, and which includes a composite material with a thermoplastic matrix and carbon fibres. The present application also relates to a turbomachine including a compressor linked to a turbine via a transmission shaft, an intermediate fan casing, and a bearing joining the transmission shaft to the intermediate casing. The casing is placed in a lubrication chamber delimited by an annular chamber cover, a chamber casing carrying the bearing and the cover.
申请公布号 US2015139784(A1) 申请公布日期 2015.05.21
申请号 US201414543981 申请日期 2014.11.18
申请人 Techspace Aero S.A. 发明人 Grelin Hervé;Honore Didier
分类号 F01D25/18;F01D25/16 主分类号 F01D25/18
代理机构 代理人
主权项 1. An annular cover for a lubrication chamber of a rotary bearing of a turbomachine, comprising: an annular wall that is generally circular and flared with an orifice at one end intended to receive a transmission shaft and a cover assembly surface at the other end; and at least one duct communicating with the inside of the wall; wherein at least one of the ducts extends along the wall as far as the assembly surface.
地址 Herstal (Milmort) BE
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