发明名称 GAS TURBINE ENGINE FRAME HAVING STRUT CONNECTED TO RING WITH MORSE PIN
摘要 PROBLEM TO BE SOLVED: To provide a gas turbine engine frame for use in supporting a bearing that supports a turbine rotor. SOLUTION: At least one inner set of coaxial tapered inner holes extend axially through inner platform flanges and at least one outer set of coaxial tapered outer holes extend axially through outer platform flanges. The inner set of coaxial tapered inner holes define an inner conical surface and the outer set of coaxial tapered outer holes define an outer conical surface. Each of the axial spaced apart platform flanges may be circumferentially continuous or scalloped so as to have protrusions arranged spaced circumferentially apart. A strut has two inner sets of coaxial tapered inner and outer holes extending axially through the inner and outer platform flanges, respectively. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005009479(A) 申请公布日期 2005.01.13
申请号 JP20040030086 申请日期 2004.02.06
申请人 GENERAL ELECTRIC CO 发明人 CZACHOR ROBERT PAUL
分类号 B22D17/00;F01D5/30;F01D9/04;F01D25/16;F01D25/28;F02K3/02;(IPC1-7):F01D9/04 主分类号 B22D17/00
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