-
公开(公告)号:US20210139381A1
公开(公告)日:2021-05-13
申请号:US16678852
申请日:2019-11-08
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson , Ying She , Gajawalli V. Srinivasan
Abstract: Disclosed is a coated ceramic fiber including a silicon carbide coating layer adjacent to the ceramic fiber and a silicon dioxide coating layer adjacent to the silicon carbide coating layer, wherein the silicon dioxide coating layer forms micro cracks after a crystal structure transformation. The coated ceramic fiber may be included in a composite material having a ceramic matrix.
-
公开(公告)号:US20210070666A1
公开(公告)日:2021-03-11
申请号:US16562103
申请日:2019-09-05
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson , Xia Tang , Paul Sheedy
Abstract: A gas turbine engine article includes a substrate and a silicate-resistant barrier coating disposed on the substrate. The silicate-resistant barrier coating is composed of a refractory matrix and a calcium aluminosilicate additive (CAS additive) dispersed in the refractory matrix.
-
公开(公告)号:US20190284099A1
公开(公告)日:2019-09-19
申请号:US16422223
申请日:2019-05-24
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson , Kathryn S. Read , Jeremy R. Hart , Andrew J. Lazur
IPC: C04B35/80 , C04B35/571 , C04B35/628
Abstract: A method of producing an enhanced ceramic matrix composite includes applying a tackifier compound to a fiber preform. The tackifier compound includes inorganic filler particles. The method further includes modifying the tackifier compound such that the inorganic filler particles remain interspersed throughout the fiber preform, and occupy pores of fiber preform.
-
公开(公告)号:US11697622B2
公开(公告)日:2023-07-11
申请号:US16562103
申请日:2019-09-05
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson , Xia Tang , Paul Sheedy
CPC classification number: C04B41/5024 , C04B41/009 , C04B41/4523 , C04B41/52 , F01D5/288 , C04B2235/3208 , C04B2235/3217 , C04B2235/3418 , C04B2235/3481 , C04B2235/5244 , C04B2235/5436 , C04B2235/96 , F05D2220/32 , F05D2300/6033
Abstract: A gas turbine engine article includes a substrate and a silicate-resistant barrier coating disposed on the substrate. The silicate-resistant barrier coating is composed of a refractory matrix and a calcium aluminosilicate additive (CAS additive) dispersed in the refractory matrix.
-
公开(公告)号:US11466589B2
公开(公告)日:2022-10-11
申请号:US16722050
申请日:2019-12-20
Applicant: United Technologies Corporation
Inventor: Michael R. Kracum , Xia Tang , Richard Wesley Jackson , Zhongfen Ding , James T. Beals
Abstract: A gas turbine engine article includes a substrate and an environmental barrier coating (EBC) system disposed on the substrate. The EBC system includes, from the substrate, a dense bond coat layer, a porous bond coat layer, and a topcoat layer in contact with the porous bond coat layer at an interface. The porous bond coat layer includes a matrix, oxygen-scavenging gas-evolution particles dispersed through the matrix, and engineered buffer pores. The oxygen-scavenging gas-evolution particles react with oxygen and generate a gaseous byproduct that diffuses through the interface to escape the EBC system. The engineered buffer pores buffer diffusion of gaseous byproduct to the interface by retaining at least a portion of the gaseous byproduct.
-
公开(公告)号:US20210246082A1
公开(公告)日:2021-08-12
申请号:US16785085
申请日:2020-02-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Richard Wesley Jackson , Michael R. Kracum , Xia Tang , James T. Beals
Abstract: An article includes a ceramic-based substrate and a barrier layer on the ceramic-based substrate. The barrier layer includes a matrix phase and gettering particles in the matrix phase. The gettering particles with an aspect ratio greater than one are aligned such that a maximum dimension of the gettering particles extends along an axis that is generally parallel to the substrate. The barrier layer includes a dispersion of diffusive particles in the matrix phase. A composite material and a method of applying a barrier layer to a substrate are also disclosed.
-
公开(公告)号:US20210189904A1
公开(公告)日:2021-06-24
申请号:US16722050
申请日:2019-12-20
Applicant: United Technologies Corporation
Inventor: Michael R. Kracum , Xia Tang , Richard Wesley Jackson , Zhongfen Ding , James T. Beals
Abstract: A gas turbine engine article includes a substrate and an environmental barrier coating (EBC) system disposed on the substrate. The EBC system includes, from the substrate, a dense bond coat layer, a porous bond coat layer, and a topcoat layer in contact with the porous bond coat layer at an interface. The porous bond coat layer includes a matrix, oxygen-scavenging gas-evolution particles dispersed through the matrix, and engineered buffer pores. The oxygen-scavenging gas-evolution particles react with oxygen and generate a gaseous byproduct that diffuses through the interface to escape the EBC system. The engineered buffer pores buffer diffusion of gaseous byproduct to the interface by retaining at least a portion of the gaseous byproduct.
-
28.
公开(公告)号:US20200216365A1
公开(公告)日:2020-07-09
申请号:US16240062
申请日:2019-01-04
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson
IPC: C04B35/80
Abstract: A ceramic matrix composite (CMC) material component is provided that includes a CMC material and an environmental barrier coating (EBC). The CMC material includes first fibers, a matrix, and at least one coefficient of thermal expansion (CTE) increasing additive. The first fibers include a first material having a first CTE value. The matrix includes a second material having a second CTE value. The at least one CTE increasing additive has a third CTE value. The EBC is disposed on at least one exposed surface of the CMC material and has a fourth CTE value. The third CTE value is greater than the first CTE value and the second CTE value, and the at least one CTE increasing additive is present within the CMC material in an amount that elevates a CTE value of the CMC material above the first CTE value or the second CTE value.
-
公开(公告)号:US20200024974A1
公开(公告)日:2020-01-23
申请号:US16038723
申请日:2018-07-18
Applicant: United Technologies Corporation
Inventor: Richard Wesley Jackson
Abstract: Disclosed is a multi-phase abradable coating including a ceramic matrix and a dislocator phase.
-
-
-
-
-
-
-
-