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公开(公告)号:US20240318567A1
公开(公告)日:2024-09-26
申请号:US18357322
申请日:2023-07-24
发明人: Ravindra Shankar Ganiger , Chandrashekhar Kandukuri , David Raju Yamarthi , Rajesh Kumar , Tajinder Singh
CPC分类号: F01D11/001 , F01D11/025 , F05D2240/55 , F05D2260/38
摘要: A turbine engine is provided. The gas turbine engine includes: a rotor; a stator comprising a carrier; a seal assembly disposed between the rotor and the stator, the seal assembly comprising a plurality of seal segments supported at least in part by the carrier, the plurality of seal segments having a first seal segment and a second seal segment, the first and second seal segments each having a seal face forming a fluid bearing with the rotor; and a seal support assembly comprising a tangential spring extension extending between the first seal segment and the second seal segment for biasing the first seal segment away from the second seal segment in the circumferential direction.