发明名称 Gas turbine engines
摘要 A mounting arrangement for the fan rotor of a ducted fan engine includes a first drive which supports and rotates the fan under normal operating conditions but which includes a frangible connection which breaks when an excessive out-of-balance force is applied to the fan rotor for example after loss of one or more blades. A second supporting and driving structure is provided which has built-in transverse flexibility but which can transmit torque. This structure is redundant during normal operation of the engine but comes into use when the frangible connection is broken and allows the fan rotor to rotate eccentrically around a new axis in an inverted condition.
申请公布号 US4193741(A) 申请公布日期 1980.03.18
申请号 US19780893817 申请日期 1978.04.05
申请人 ROLLS ROYCE LTD 发明人 BRIGGS, HENRY R
分类号 F01D21/04;F01D25/16;F02C7/04;(IPC1-7):F01D5/10 主分类号 F01D21/04
代理机构 代理人
主权项
地址