中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

40 records (took 0.044 seconds)

    11.
    发明专利
    未知

    公开(公告)号：DE69903595T2

    公开(公告)日：2003-06-18

    申请号：DE69903595

    申请日：1999-06-11

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： BOSE SUDHANGSU ,  GUPTA DINESH K ,  MARCIN JEANINE T ,  ULION NICHOLAS E

    IPC: F01D5/28 ,  C23C4/00 ,  C23C4/08 ,  C23C28/00 ,  F01D5/18 ,  F02C7/00 ,  C23C4/02

    Abstract: A thermal barrier coating system for a superalloy substrate is disclosed. The superalloy is preferably of the type that is capable of forming an adherent alumina layer. A bond coat is applied to a local area of the substrate (24), so that a portion of the substrate remains exposed. The localized area is defined to be the area(s) at which a TBC typically fails first, e.g., the leading (30) and trailing edges (32) of an airfoil (20), or other area. An alumina layer (26) is formed on the remaining portion of the substrate, and also on the bond coat. A ceramic layer (28) is then applied on the alumina layer. Even if the ceramic material is removed, the localized bond coat remains, and reduces the rate at which the underlying substrate oxidizes. A coated article is also disclosed, as is a system that utilizes a conventional superalloy and aluminide coating with the localized bond coat.

    Thermal barrier coating system utilizing lcalized bond coat and article having the same
    12.
    发明专利
    Thermal barrier coating system utilizing lcalized bond coat and article having the same 未知

    公开(公告)号：SG75960A1

    公开(公告)日：2000-10-24

    申请号：SG1999002587

    申请日：1999-05-26

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： BOSE SUDHANGSHU ,  GUPTA DINESH K ,  MARCIN JEANINE T ,  ULION NICHOLAS E

    IPC: F01D5/28 ,  C23C4/00 ,  C23C4/08 ,  C23C28/00 ,  F01D5/18 ,  F02C7/00

    Abstract: A thermal barrier coating system for a superalloy substrate is disclosed. The superalloy is preferably of the type that is capable of forming an adherent alumina layer. A bond coat is applied to a local area of the substrate (24), so that a portion of the substrate remains exposed. The localized area is defined to be the area(s) at which a TBC typically fails first, e.g., the leading (30) and trailing edges (32) of an airfoil (20), or other area. An alumina layer (26) is formed on the remaining portion of the substrate, and also on the bond coat. A ceramic layer (28) is then applied on the alumina layer. Even if the ceramic material is removed, the localized bond coat remains, and reduces the rate at which the underlying substrate oxidizes. A coated article is also disclosed, as is a system that utilizes a conventional superalloy and aluminide coating with the localized bond coat.

    16.
    发明专利
    未知

    公开(公告)号：ES2181365T3

    公开(公告)日：2003-02-16

    申请号：ES99304588

    申请日：1999-06-11

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： BOSE SUDHANGSU ,  GUPTA DINESH K ,  MARCIN JEANINE T ,  ULION NICHOLAS E

    IPC: F01D5/28 ,  C23C4/00 ,  C23C4/08 ,  C23C28/00 ,  F01D5/18 ,  F02C7/00 ,  C23C4/02

    Abstract: A thermal barrier coating system for a superalloy substrate is disclosed. The superalloy is preferably of the type that is capable of forming an adherent alumina layer. A bond coat is applied to a local area of the substrate (24), so that a portion of the substrate remains exposed. The localized area is defined to be the area(s) at which a TBC typically fails first, e.g., the leading (30) and trailing edges (32) of an airfoil (20), or other area. An alumina layer (26) is formed on the remaining portion of the substrate, and also on the bond coat. A ceramic layer (28) is then applied on the alumina layer. Even if the ceramic material is removed, the localized bond coat remains, and reduces the rate at which the underlying substrate oxidizes. A coated article is also disclosed, as is a system that utilizes a conventional superalloy and aluminide coating with the localized bond coat.

    THERMAL BARRIER COATING SYSTEM UTILIZING LOCALIZED BOND COATAND ARTICLE HAVING THE SAME
    17.
    发明专利
    THERMAL BARRIER COATING SYSTEM UTILIZING LOCALIZED BOND COATAND ARTICLE HAVING THE SAME 未知

    公开(公告)号：CA2274412A1

    公开(公告)日：1999-12-12

    申请号：CA2274412

    申请日：1999-06-11

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： BOSE SUDHANGSHU ,  MARCIN JEANINE T ,  GUPTA DINESH K ,  ULION NICHOLAS E

    IPC: F01D5/28 ,  C23C4/00 ,  C23C4/08 ,  C23C28/00 ,  F01D5/18 ,  F02C7/00 ,  C23C4/10

    Abstract: A thermal barrier coating system for a superalloy substrate is disclosed. The superalloy is preferably of the type that is capable of forming an adherent alumina layer. A bond coat is applied to a local area of the substrate, so that a portion of the substrate remains exposed. The localized area is defined to be the areas) at which a TBC typically fails first, e.g., the leading and trailing edges of an airfoil, or other area. An alumina layer is formed on the remaining portion of the substrate, and also on the bond coat. A ceramic layer is then applied on the alumina layer. Even if the ceramic material is removed, the localized bond coat remains, and reduces the rate at which the underlying substrate oxidizes. A coated article is also disclosed, as is a system that utilizes a conventional superalloy and aluminide coating with the localized bond coat.

    18.
    发明专利
    未知

    公开(公告)号：DE3415282A1

    公开(公告)日：1984-12-06

    申请号：DE3415282

    申请日：1984-04-24

    Applicant: UNITED TECHNOLOGIES CORP

    Inventor： FIELD THOMAS T ,  CHEN OTIS Y ,  GEARY ARTHUR R ,  SALKELD RICHARD W ,  ULION NICHOLAS E

    IPC: C30B21/02 ,  C22C19/05 ,  C22F1/00 ,  C22F1/10 ,  C30B29/52 ,  C30B33/00

    Abstract: Concepts relating to the heat treatment of single crystal superalloy articles are disclosed. A first concept is the use of a heat treatment sequence which includes incipient melting of the article being heat treated followed by one or more steps which essentially heal the incipient melting damage. A second concept relates to the treatment of previously heat treated single crystal articles which have incipient melting. Methods are disclosed for healing this damage and for recovering the mechanical properties of such articles. A third concept disclosed is a particular cycle which permits effective heat treatment of a specific single crystal alloy composition.

Patent Agency Ranking