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公开(公告)号:US09822656B2
公开(公告)日:2017-11-21
申请号:US14728003
申请日:2015-06-02
CPC分类号: F01D11/006 , F01D5/02 , F01D5/30 , F01D5/3007 , F01D5/3015 , F01D5/326 , F01D11/005 , F05D2200/263 , F05D2220/32 , F05D2240/55 , F05D2250/192 , F05D2250/38 , F05D2300/10 , F05D2300/43 , F05D2300/44
摘要: The present invention relates to a rotor assembly for a rotary machine such as a gas turbine. The present solution provides a sealing wire located inside a groove engraved in the rotor body. The sealing wire is responsive to radial centrifugal forces acting during normal operation of the machine, and moves radially in the groove until a sealing configuration is achieved such to prevent damaging hot leakage towards machine components.
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公开(公告)号:US20150267542A1
公开(公告)日:2015-09-24
申请号:US14661220
申请日:2015-03-18
CPC分类号: F01D5/18 , F01D5/02 , F01D5/063 , F01D5/087 , F01D25/12 , F05D2220/31 , F05D2220/32 , F05D2230/10 , F05D2240/60 , F05D2260/232 , F05D2260/941
摘要: The invention relates to a rotor shaft adapted to rotate about a rotor axis thereof. The rotor shaft includes a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft, and a plurality of cooling bores extending radially or quasi-radially outward from the inside to an outside of the rotor shaft. Each cooling bore having a bore inlet location and a distal bore outlet portion, the respective bore inlet location being adapted to abut on the rotor cavity. At least one side or part-side of the cooling bore inlet location is provided with an asymmetric edge fillet in order to maximize the wall thickness between two adjacent cooling bores.
摘要翻译: 本发明涉及适于围绕其转子轴线旋转的转子轴。 转子轴包括与转子轴内的转子轴同心或准同心配置的转子腔,以及从转子轴的内侧向外径向或半径向外延伸的多个冷却孔。 每个冷却孔具有孔入口位置和远端孔出口部分,相应的孔入口位置适于邻接转子腔。 冷却孔入口位置的至少一侧或部分侧设置有不对称边缘,以使两个相邻冷却孔之间的壁厚最大化。
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公开(公告)号:US11105205B2
公开(公告)日:2021-08-31
申请号:US14341189
申请日:2014-07-25
摘要: A rotor shaft adapted to rotate about a rotor axis thereof. The rotor shaft includes a rotor cavity configured concentrically to the rotor axis inside the rotor shaft. The rotor shaft further includes a plurality of cooling bores extending radially outward from the rotor cavity to feed cooling air into an internal cooling system in a blade. Each cooling bore includes a bore inlet portion and a distal bore outlet portion. The respective bore inlet portion ends in a plateau, projecting above the outer circumference contour of the rotor cavity. Thus, cooling bore inlets are shifted to a low stress area and the lifetime of the rotor is improved.
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