发明名称 THERMALLY TUNABLE SYSTEMS
摘要 One embodiment of the present disclosure is a unique system. Another embodiment is a unique fastener system. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines, fastener systems and other systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
申请公布号 US2014186095(A1) 申请公布日期 2014.07.03
申请号 US201314137437 申请日期 2013.12.20
申请人 Rolls-Royce Corporation 发明人 Peters Joshua M.;Muskat James C.
分类号 F04D29/02 主分类号 F04D29/02
代理机构 代理人
主权项 1. A system for securing a first attachment location to a second attachment location, comprising: a first member having a first coefficient of thermal expansion, a first attachment feature, and a first interface feature, wherein the first attachment feature is configured for attaching the first member to the first attachment location; a second member having a second coefficient of thermal expansion that is higher than the first coefficient of thermal expansion; and having a second interface feature and a third interface feature, wherein the first interface feature and the second interface feature are configured for engagement with each other, and are configured to transmit an axial load between the first member and the second member; and a third member having a third coefficient of thermal expansion that is lower than the second coefficient of thermal expansion; and having a second attachment feature and a fourth interface feature, wherein the second attachment feature is configured to attach the third member to the second attachment location; and wherein the fourth interface feature and the third interface feature are configured for engagement with each other, and are configured to transmit an axial load between the second member and the third member.
地址 Indianapolis IN US