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1.发明授权公开(公告)号：US11407688B2
公开(公告)日：2022-08-09
申请号：US16098368
申请日：2017-04-11
IPC分类号： C04B35/16 , C04B41/89 , F01D25/00 , F01D25/24 , F23R3/42 , F02C7/00 , F01D5/18 , C04B41/45 , C04B41/50 , F01D5/14
摘要： Provided are a coating structure, a turbine part having the same, and a method for manufacturing the coating structure. The coating structure is provided on a surface of a base portion including a ceramic matrix composite. The coating structure is layered on the surface of the base portion, and includes a bond coat layer formed of a rare-earth silicate and a top coat layer layered on the bond coat layer. The residual stress present in the bond coat layer is compressive residual stress. The oxygen permeability coefficient of the bond coat layer is no greater than 10−9 kg·m−1·s−1 at a temperature of not lower than 1200° C. and a higher oxygen partial pressure of not less than 0.02 MPa. The bond coat layer may contain carbonitride particles or carbonitride whiskers.
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公开(公告)号：US11371353B2
公开(公告)日：2022-06-28
申请号：US16647060
申请日：2018-06-22
IPC分类号： F01D5/14 , F01D25/12 , F01D9/04 , B22F5/04 , B22F7/06 , B22F10/40 , B23K26/21 , B23K26/24 , B23K26/342 , B23P15/04 , B33Y10/00 , B33Y80/00
摘要： A method of manufacturing a turbine blade includes forming a blade body divided body constituting a blade body of the turbine blade by a three-dimensional lamination method; individually forming a plurality of shroud divided bodies constituting a shroud of the turbine blade for each of the shroud divided bodies by a three-dimensional lamination method; joining the shroud divided bodies together; and joining the blade body divided body and the shroud divided bodies.
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公开(公告)号：US11148169B2
公开(公告)日：2021-10-19
申请号：US15515677
申请日：2015-12-03
发明人： Taiji Torigoe , Masahiko Mega , Yoshifumi Okajima , Shuji Tanigawa , Masamitsu Kuwabara , Naotoshi Okaya
IPC分类号： C23C4/02 , C23C4/18 , F01D5/28 , F01D5/18 , B05D1/32 , B05D1/02 , B05D3/06 , B05D7/14 , C23C26/00 , F01D9/04 , F23R3/00
摘要： A method of forming a sprayed coating includes preparing a spray target member having a surface on which openings of first ends of holes are formed, preparing a plurality of masking pins each of which comprises metal, and inserting each of the masking pins into a corresponding one of the holes so that each of the masking pins partially protrudes from the surface. The method also includes applying an adhesive agent for fixing the masking pins to the respective holes, to at least one of the holes or the masking pins, forming a ceramic layer by spraying on the surface of the spraying target member, the ceramic layer comprising a ceramic material, while the masking pins are fixed to the respective holes via the adhesive agent, and removing the masking pins from the holes after the spraying step.
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公开(公告)号：US09989450B2
公开(公告)日：2018-06-05
申请号：US14933373
申请日：2015-11-05
发明人： Daisuke Kudo , Taiji Torigoe , Junichiro Masada , Koji Takahashi , Yoshitaka Uemura , Yoshifumi Okajima , Naotoshi Okaya , Eisaku Ito , Masahiko Mega , Shigenari Horie , Shuji Tanigawa , Yasuhiko Tsuru , Keizo Tsukagoshi , Masamitsu Kuwabara
摘要： An erosion test apparatus includes a combustor configured to obtain a combustion gas by mixing and combusting compressed air and a fuel, and an erodent supply unit configured to supply an erodent to the combustion gas. The erosion test apparatus further includes an accommodation support unit configured to accommodate and support a test piece having a front surface coated through thermal barrier coating, and an accelerator configured to accelerate the combustion gas including the erodent to collide with the test piece.
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