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公开(公告)号:US09816379B2
公开(公告)日:2017-11-14
申请号:US14219726
申请日:2014-03-19
申请人: MTU Aero Engines AG
发明人: Manfred Feldmann , Andreas Holzel , Amelia Frodyma
CPC分类号: F01D5/027 , F01D5/225 , F01D25/28 , F05D2230/60 , F05D2260/15 , F16F15/32 , Y10T29/49245 , Y10T29/4932
摘要: The present invention relates to a balancing body (1) for fastening to a ring (4, 5) of a continuous blade arrangement of a compressor or turbine stage of a gas turbine, wherein the balancing body has a first stop (11) for the form-fitting attachment of the balancing body in one peripheral direction (R) to a first axial shoulder (6; 7) of the ring.
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公开(公告)号:US20140348655A1
公开(公告)日:2014-11-27
申请号:US14219726
申请日:2014-03-19
申请人: MTU Aero Engines AG
发明人: Manfred Feldmann , Andreas Holzel , Amelia Frodyma
CPC分类号: F01D5/027 , F01D5/225 , F01D25/28 , F05D2230/60 , F05D2260/15 , F16F15/32 , Y10T29/49245 , Y10T29/4932
摘要: The present invention relates to a balancing body (1) for fastening to a ring (4, 5) of a continuous blade arrangement of a compressor or turbine stage of a gas turbine, wherein the balancing body has a first stop (11) for the form-fitting attachment of the balancing body in one peripheral direction (R) to a first axial shoulder (6; 7) of the ring.
摘要翻译: 本发明涉及一种用于紧固到燃气轮机的压缩机或涡轮级的连续叶片装置的环(4,5)的平衡体(1),其中平衡体具有用于 平衡体在一个圆周方向(R)与环的第一轴向肩部(6; 7)的形状配合附接。
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