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公开(公告)号:EP4140968B1
公开(公告)日:2024-06-05
申请号:EP22188486.9
申请日:2022-08-03
IPC分类号: C04B35/83 , B32B18/00 , C04B35/645 , F16D65/12 , D04H1/4242
CPC分类号: C04B35/83 , C04B35/645 , C04B2235/524820130101 , C04B2235/526820130101 , C04B2235/525620130101 , C04B2235/61420130101 , C04B2235/656720130101 , C04B2235/65820130101 , C04B2235/7720130101 , C04B2237/6220130101 , C04B2237/38520130101 , B32B18/00 , C04B2235/602820130101 , D04H1/4242 , F16D65/127 , F16D69/023 , F16D2200/005220130101 , F16D2200/006520130101 , D04H1/593 , D04H1/645
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公开(公告)号:EP4414345A1
公开(公告)日:2024-08-14
申请号:EP24154222.4
申请日:2024-01-26
IPC分类号: C04B37/00
CPC分类号: C04B37/005 , C04B2237/3820130101 , C04B2237/6120130101 , C04B2237/6220130101 , C04B2237/08620130101 , C04B2237/08320130101 , C04B2237/0920130101 , F02C7/045 , C04B2235/602620130101 , C04B2235/61420130101 , C04B2235/61620130101 , C04B35/6263
摘要: A method (200) of assembling a composite panel (100) includes disposing a pliable matrix material (190) between a first side (141) of a ceramic core structure (120) and a ceramic matrix composite face sheet (110), wherein the ceramic core structure (120) comprises a plurality of hollow cells (130) defined by a plurality of walls (132) extending from the first side (141) of the ceramic core structure (120) to a second side (143) of the ceramic core structure (120) opposite the first side (141); and densifying the pliable matrix material (190) to bond the pliable matrix material (190) with the ceramic core structure (120) and the ceramic matrix composite face sheet (110). The pliable matrix material (190) may comprise a liquid carrier, a powder, and a polymeric binder.
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公开(公告)号:EP4355576A1
公开(公告)日:2024-04-24
申请号:EP22741919.9
申请日:2022-06-17
申请人: RTX Corporation
发明人: READ, Kathryn Sarah , LENZ, Brendan Michael , ROACH, James T. , CLARKE, Steven R. , TOMICH, Aaron
CPC分类号: C04B35/80 , B32B18/00 , C04B2237/3820130101 , C04B2237/58620130101 , C04B2237/6220130101 , C04B2235/524420130101 , B32B5/12 , B32B5/26 , C04B2235/525220130101 , C04B2235/525620130101 , C04B2235/524820130101 , C04B2235/522420130101 , C04B2235/522820130101 , C04B2235/61420130101 , C04B35/565 , C04B35/117 , C04B35/583 , C04B35/563 , C04B35/584 , C04B35/58092 , C04B35/14 , C04B35/5603 , B32B5/024 , B32B2262/10520130101
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公开(公告)号:EP4428113A1
公开(公告)日:2024-09-11
申请号:EP23217250.2
申请日:2023-12-15
发明人: JADIDIAN, Bahram , BLINN, Kevin , MEHR, Mehrad
IPC分类号: C04B37/00 , C04B35/645 , F23R3/00
CPC分类号: C04B37/005 , C04B2237/34120130101 , C04B2237/36520130101 , C04B2237/36820130101 , C04B2237/3820130101 , C04B2237/3420130101 , C04B2237/06220130101 , C04B2237/6220130101 , C04B2237/8620130101 , F23R3/007 , C04B2235/544520130101 , C04B2235/543620130101 , C04B2235/65820130101 , C04B35/6455
摘要: Components of gas turbine engines, aircraft comprising the components, and methods of producing the components are provided. The component includes a surface, and a set of tiles secured to the surface at interfaces between the set of tiles and the surface and between each of the set of tiles. The set of tiles conform to the surface and in combination define a coating system on the surface that includes an environmental barrier coating and/or a thermal barrier coating.
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公开(公告)号:EP4408815A1
公开(公告)日:2024-08-07
申请号:EP21790101.6
申请日:2021-09-29
IPC分类号: C04B35/528 , C04B35/56 , C04B35/563 , C04B35/565 , C04B35/58 , C04B35/581 , C04B35/584 , C04B37/00 , C04B38/00
CPC分类号: C04B37/003 , C04B2237/3620130101 , C04B2237/36520130101 , C04B2237/36620130101 , C04B2237/36820130101 , C04B2237/6120130101 , C04B2237/6220130101 , C04B35/565 , C04B35/563 , C04B35/528 , C04B35/58092 , C04B35/584 , C04B35/581 , C04B35/5611 , C04B35/5622 , C04B35/5626 , C04B2235/42720130101 , C04B2235/42820130101 , C04B2235/42120130101 , C04B2235/40220130101 , C04B2235/40720130101 , C04B2235/61620130101 , C04B2235/61420130101 , C04B2235/543620130101 , C04B38/0003 , C04B2111/0084420130101
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