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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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