发明名称 GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To limit deviation of a rotor shaft to minimize a torque load applied to a fun case from the rotor shaft when a fun blade is lost. SOLUTION: A hardening fun case liner 42 is provided inside a fun storing case assembly 30 for a gas turbine engine. A fun blade top part gets rotatable along a circumferential direction in the periphery of a fun case 48 by the fun case liner 42 at the time of generation of a fun blade lost condition. By this manner, the liner 42 reduces a cut and fracture of the fun case 48, reduces damage of the fun case 48 to the minimum, and reduces a torque load applied to the fun case 48 due to rotor deviation.
申请公布号 JPH11200813(A) 申请公布日期 1999.07.27
申请号 JP19980299285 申请日期 1998.10.21
申请人 UNITED TECHNOL CORP <UTC> 发明人 DUYN KEVEN G VAN
分类号 F01D11/08;F01D25/24;(IPC1-7):F01D25/24 主分类号 F01D11/08
代理机构 代理人
主权项
地址