发明名称 TURBINE ENGINE
摘要 <P>PROBLEM TO BE SOLVED: To improve technology for an engine and a bearing system of the engine. <P>SOLUTION: Effective length L<SB>2</SB>between two bearings 60 and 70 exceeds actual length L to separate unbalance further in a rotary structure such as a gas turbine engine 20. This can be achieved through a bearing supporting body 72 having one or a plurality of tapers related to at least one bearing 70. A meltable link is provided in a force path between the first bearing 60 and a support column hub 32 to specify a predetermined destruction position for unbalance force exceeding a threshold value. The meltable link is provided in the visinity of a connection part 160 between a rear side flange of a front side member 128 and a front side flange of a rear side member 130. <P>COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2005325837(A) 申请公布日期 2005.11.24
申请号 JP20050139206 申请日期 2005.05.12
申请人 UNITED TECHNOL CORP <UTC> 发明人 VAN DUYN KEVEN G
分类号 F01D21/04;F01D25/16;F02C7/00;F02C7/06;F02K3/06;F16C27/04;F16C35/07 主分类号 F01D21/04
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