发明名称 Turbomachine blade
摘要 A turbomachine including securing means that extend between the pressure wall and the suction surface and which includes an energy absorbing portion for absorbing energy after impact to the blade by a foreign object. The energy absorbing portion has a catch that provides the blade with an improved resistance to bursting.
申请公布号 US9028219(B2) 申请公布日期 2015.05.12
申请号 US200812105576 申请日期 2008.04.18
申请人 Rolls-Royce PLC 发明人 Clark Daniel;Rongong Jem Athing
分类号 F01D5/14;F04D29/38;F01D21/04;F04D29/32 主分类号 F01D5/14
代理机构 McCormick Paulding & Huber LLP 代理人 McCormick Paulding & Huber LLP
主权项 1. A turbomachine blade comprising a root portion and an aerofoil portion, the aerofoil portion having a leading edge, a trailing edge, a wall for forming a pressure surface extending from the leading edge to the trailing edge and wall for forming a suction wall extending from the leading edge to the trailing edge, wherein the aerofoil portion includes a first extension extending from the suction wall towards the pressure wall and a second extension extending from the pressure wall towards the suction wall, wherein a first catch element is provided on the first extension and a second catch element is provided on the second extension wherein the first catch element is arranged to engage with the second catch element and absorb energy after impact to the blade by the foreign object and the first catch element and the second catch element are separated from each other by a volume containing a viscoelastic damper.
地址 GB