发明名称 Gas turbine engine structure
摘要 A turbine disk ( 20 ) has a sealing plate ( 28 ) fixed to it by bayonet fixing features ( 36 ) and ( 40 ) formed in sealing plate flange ( 30 ) and disk flange ( 38 ). Abutments ( 42 ) and ( 44 ) are formed on the bayonet fixings, between which a multi part anti relative rotation locking member ( 46 ) is positioned in abutting relationship.
申请公布号 US7318704(B2) 申请公布日期 2008.01.15
申请号 US20050133211 申请日期 2005.05.20
申请人 ROLLS-ROYCE PLC 发明人 WAGNER STEFAN J.
分类号 F01D5/32;F01D5/06;F01D5/30;F01D25/24;F16B5/10;F16B39/10 主分类号 F01D5/32
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