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公开(公告)号:EP4048870B1
公开(公告)日:2024-05-08
申请号:EP20767666.9
申请日:2020-08-21
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公开(公告)号:EP3865680B1
公开(公告)日:2024-05-08
申请号:EP21156971.0
申请日:2021-02-12
CPC分类号: F01D25/12 , F01D25/183 , F01D11/003 , F16J15/3404 , F05D2240/5520130101 , F05D2260/2020130101 , F05D2260/20120130101 , F05D2260/221220130101 , F04D29/122 , Y02T50/60
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公开(公告)号:EP4353948A1
公开(公告)日:2024-04-17
申请号:EP23197045.0
申请日:2023-09-13
申请人: Rolls-Royce plc
CPC分类号: F01D5/187 , F01D9/065 , F05D2240/12620130101 , F05D2260/20120130101 , F05D2260/20220130101 , F05D2260/221420130101
摘要: Disclosed is an aerofoil (100) for a gas turbine engine comprising: a first conduit (1129 formed in the aerofoil; a second conduit (114) formed in the aerofoil; and a dividing wall (116) separating the first and second conduits, the dividing wall comprising a transfer port (118) configured to permit fluid flow between the first and second conduits; wherein the dividing wall (116) further comprises a reinforcing boss (120) at least partially encircling the transfer port (118). Also disclosed is a gas turbine engine comprising the aerofoil and an aircraft comprising the gas turbine engine.
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公开(公告)号:EP3098386B1
公开(公告)日:2024-09-18
申请号:EP16169984.8
申请日:2016-05-17
IPC分类号: F01D5/18
CPC分类号: F01D5/189 , F05D2260/20120130101
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公开(公告)号:EP4189215B1
公开(公告)日:2024-05-29
申请号:EP21786728.2
申请日:2021-09-02
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公开(公告)号:EP3971391B1
公开(公告)日:2024-05-01
申请号:EP21197522.2
申请日:2021-09-17
CPC分类号: F01D5/284 , F05D2300/603320130101 , F05D2260/20120130101 , F05D2240/12120130101 , F01D9/041 , F01D5/188 , F01D5/189 , F01D9/065
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公开(公告)号:EP3385504B1
公开(公告)日:2024-05-01
申请号:EP18160507.2
申请日:2018-03-07
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公开(公告)号:EP2890880B1
公开(公告)日:2024-09-25
申请号:EP13832115.3
申请日:2013-08-26
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公开(公告)号:EP3816407B1
公开(公告)日:2024-07-17
申请号:EP20205461.5
申请日:2020-11-03
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公开(公告)号:EP3865682B1
公开(公告)日:2024-05-29
申请号:EP21156078.4
申请日:2021-02-09
IPC分类号: F01D25/24
CPC分类号: F01D25/246 , F05D2240/1120130101 , F05D2260/20120130101 , Y02T50/60
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