发明授权
- 专利标题: Duct wall for a fan of a gas turbine engine
- 专利标题(中): 燃气涡轮发动机风机的管壁
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申请号: US12768041申请日: 2010-04-27
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公开(公告)号: US08506234B2公开(公告)日: 2013-08-13
- 发明人: Richard V Brooks , Kenneth F Udall , Richard G Stretton
- 申请人: Richard V Brooks , Kenneth F Udall , Richard G Stretton
- 申请人地址: GB London
- 专利权人: Rolls-Royce PLC
- 当前专利权人: Rolls-Royce PLC
- 当前专利权人地址: GB London
- 代理机构: Oliff & Berridge, PLC
- 优先权: GB0907580.5 20090505
- 主分类号: F01D21/00
- IPC分类号: F01D21/00
摘要:
A duct wall of a fan casing of a gas turbine engine comprises an intake section and a containment casing, which are interconnected by bolts at flanges. An acoustic flutter damper is provided between the flanges to reduce or eliminate flutter arising in blades of the fan at certain important operating conditions. The damper provides flexibility at the connection between the intake section and the containment casing so that, in the event of detachment of a blade or a bladed fragment, the resulting deflection wave in the containment casing can be accommodated by displacement and/or deformation of the acoustic flutter damper, reducing the risk that the bolts will shear to allow the intake section and the containment casing to become detached from each other. The acoustic flutter damper may comprise a circumferential array of separate segments.
公开/授权文献
- US20100284788A1 DUCT WALL FOR A FAN OF A GAS TURBINE ENGINE 公开/授权日:2010-11-11
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