发明名称 Gas turbine engine fan stand with hinged rotating frame
摘要 A gas turbine engine fan stand (40) comprising a base frame (42) and a fan case frame (44) coupled together at one edge by a hinge (46). The fan case frame (44) is arranged to: rotate about the hinge (46) between abutting the base frame (42) and substantially perpendicular thereto; and tilt about a yaw axis (52) perpendicular to the hinge (46) and in the plane of the fan case frame (44). The fan case frame (44) further comprising a coupling arrangement (56) arranged to rotate about a roll axis (60) and to couple a fan case (36) to the fan case frame (44). A gas turbine engine stand assembly (68) comprising a fan stand (40) and a core stand (38). A method of splitting a gas turbine engine (10) and a method of reassembling a gas turbine engine (10).
申请公布号 EP2873903(B1) 申请公布日期 2016.01.20
申请号 EP20140190642 申请日期 2014.10.28
申请人 ROLLS-ROYCE PLC 发明人 HALLAM, CHRISTOPHER RICHARD;TAYLOR, JONATHAN PAUL
分类号 F16M11/42;B23P19/04;B64F5/00;F01D25/28;F02C7/20 主分类号 F16M11/42
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