公开(公告)号：US20250145541A1

公开(公告)日：2025-05-08

申请号：US18504894

申请日：2023-11-08

Applicant: Honeywell International Inc.

Inventor： Mehrad Mehr ,  Bahram Jadidian ,  Kevin Blinn

IPC: C04B41/50 ,  C04B35/591 ,  C04B35/65 ,  C04B41/45 ,  C04B41/87

Abstract: In some examples, a method for making a refractory component includes depositing carbon on a surface of a refractory substrate. The carbon fills surface voids on the surface of the refractory substrate. A melting point of the refractory substrate is greater than or equal to about 1500 degrees Celsius (° C.). The method includes applying a metal slurry to a surface of the refractory substrate following the deposition of the carbon and reacting a metal of the metal slurry with the carbon to form a metal carbide phase within the surface voids of the refractory substrate.

公开(公告)号：US12297778B2

公开(公告)日：2025-05-13

申请号：US18181159

申请日：2023-03-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Bahram Jadidian ,  Kevin Blinn ,  Mehrad Mehr

IPC: F02C7/24 ,  B64D27/10 ,  F02C6/20

Abstract: 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.

公开(公告)号：US20240300860A1

公开(公告)日：2024-09-12

申请号：US18181345

申请日：2023-03-09

Applicant: Honeywell International Inc.

Inventor： Kevin Blinn ,  Mehrad Mehr ,  Bahram Jadidian

IPC: C04B35/571 ,  C04B35/626 ,  C04B35/645

CPC classification number: C04B35/571 ,  C04B35/6263 ,  C04B35/645 ,  B22D41/02 ,  C04B2235/3206 ,  C04B2235/3208 ,  C04B2235/3217 ,  C04B2235/3232 ,  C04B2235/3244 ,  C04B2235/3272 ,  C04B2235/3418 ,  C04B2235/3427 ,  C04B2235/349 ,  C04B2235/3826 ,  C04B2235/483 ,  C04B2235/656 ,  C04B2235/9676

Abstract: A method for forming a refractory component of foundry system includes forming a preform from a refractory mixture. The refractory mixture includes a silicon carbide preceramic polymer and at least one of a refractory powder or refractory aggregate. The method further includes heating the preform to pyrolyze the silicon carbide preceramic polymer and form a refractory material defining the refractory component. The resulting refractory material includes at least one of the refractory powder or the refractory aggregate in a silicon carbide matrix. The refractory component defines an oxidation-resistant surface configured to contact molten metal.

公开(公告)号：US12228051B1

公开(公告)日：2025-02-18

申请号：US18359480

申请日：2023-07-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Bahram Jadidian ,  Kevin Blinn ,  Mehrad Mehr

IPC: F01D5/28 ,  C04B35/16 ,  C04B35/584 ,  C04B41/52 ,  C04B41/87 ,  C04B41/91

Abstract: Components having coating systems that include mud cracks, methods for forming the coating systems, and vehicles including the components are provided. The components include a substrate having silicon nitride and a coating system on a surface of the substrate. The coating system includes a first layer of a first coating material on the substrate, wherein the first coating material includes a rare earth silicate and has a first thickness measured in a direction perpendicular to the surface of the substrate, and a second layer of a second coating material on the first layer, wherein the second coating material includes a rare earth silicate and has a second thickness that is greater than the first thickness. The second layer includes mud cracks that extend from an exterior surface thereof toward the substrate, and the mud cracks have widths in a range of about 50 to 200 micrometers.

公开(公告)号：US20250035001A1

公开(公告)日：2025-01-30

申请号：US18359480

申请日：2023-07-26

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Bahram Jadidian ,  Kevin Blinn ,  Mehrad Mehr

IPC: F01D5/28 ,  C04B35/16 ,  C04B35/584 ,  C04B41/52 ,  C04B41/87 ,  C04B41/91

Abstract: Components having coating systems that include mud cracks, methods for forming the coating systems, and vehicles including the components are provided. The components include a substrate having silicon nitride and a coating system on a surface of the substrate. The coating system includes a first layer of a first coating material on the substrate, wherein the first coating material includes a rare earth silicate and has a first thickness measured in a direction perpendicular to the surface of the substrate, and a second layer of a second coating material on the first layer, wherein the second coating material includes a rare earth silicate and has a second thickness that is greater than the first thickness. The second layer includes mud cracks that extend from an exterior surface thereof toward the substrate, and the mud cracks have widths in a range of about 50 to 200 micrometers.

公开(公告)号：US20240301832A1

公开(公告)日：2024-09-12

申请号：US18181159

申请日：2023-03-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Bahram Jadidian ,  Kevin Blinn ,  Mehrad Mehr

IPC: F02C7/24 ,  B64D27/10 ,  F02C6/20

CPC classification number: F02C7/24 ,  B64D27/10 ,  F02C6/20

Abstract: 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.