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公开(公告)号:JP2003268569A
公开(公告)日:2003-09-25
申请号:JP2003033955
申请日:2003-02-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor: GUPTA DINESH , LAMBERT DAVID L , TRUBELJA MLADEN F , MALONEY MICHAEL J , ULION NICHOLAS E , LITTON DAVID A
Abstract: PROBLEM TO BE SOLVED: To provide a superalloy article having a thermal barrier coating film. SOLUTION: The article comprises a superalloy substrate, an adherent alumina layer on the substrate, and a ceramic, thermally insulating layer on the alumina layer. The ceramic layer has an overall thickness and comprises relatively strain tolerant columnar grain ceramic on the alumina layer and relatively more thermally insulating ceramic on the columnar grain ceramic. The alumina layer may be formed using an alumina forming layer such as an overlay or aluminide bond coat, or the superalloy may be constituted of a material capable of forming an alumina layer. The ceramic layers may be formed of a stabilized zirconia or other suitable material and may have the same or different compositions. COPYRIGHT: (C)2003,JPO
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公开(公告)号:WO2014126633A3
公开(公告)日:2014-11-13
申请号:PCT/US2013072558
申请日:2013-12-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HAZEL BRIAN T , LITTON DAVID A
CPC classification number: C23C14/30 , C23C4/02 , C23C4/11 , C23C4/134 , C23C14/083 , C23C28/042 , C23C28/321 , C23C28/3215 , C23C28/3455 , F01D5/288
Abstract: In a method for coating a substrate (22), a ceramic first layer (40) is applied by electron beam physical deposition (210). A ceramic second layer (42) is suspension plasma sprayed (220).
Abstract translation: 在用于涂覆基板(22)的方法中,通过电子束物理沉积(210)施加陶瓷第一层(40)。 陶瓷第二层(42)是悬浮等离子体喷涂(220)。
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公开(公告)号:WO2014144189A1
公开(公告)日:2014-09-18
申请号:PCT/US2014028489
申请日:2014-03-14
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HAZEL BRIAN T , MALONEY MICHAEL J , NEAL JAMES W , LITTON DAVID A
IPC: C23C14/22
CPC classification number: C23C14/30 , C23C14/228 , C23C14/243 , C23C14/246 , C23C14/505
Abstract: A deposition apparatus (20) comprising: a chamber (22); a process gas source (62) coupled to the chamber; a vacuum pump (52) coupled to the chamber; at least two electron guns (26); one or more power supplies (30) coupled to the electron guns; a plurality of crucibles (32,33,34) positioned or positionable in an operative position within a field of view of at least one said electron gun; and a part holder (170) having at least one operative position for holding parts spaced above the crucibles by a standoff height H. The standoff height H is adjustable in a range including at least 22 inches.
Abstract translation: 一种沉积设备(20),包括:腔室(22); 耦合到所述室的处理气体源(62); 耦合到所述室的真空泵(52); 至少两个电子枪(26); 耦合到电子枪的一个或多个电源(30); 多个坩埚(32,33,34),其定位或定位在至少一个所述电子枪的视场内的操作位置; 以及具有至少一个操作位置的部件保持器(170),用于将间隔在坩埚上方的部件保持在间隔高度H上。间隔高度H在包括至少22英寸的范围内是可调节的。
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公开(公告)号:WO2014065928A3
公开(公告)日:2014-07-17
申请号:PCT/US2013054088
申请日:2013-08-08
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHROCK CHRISTOPHER W , MALONEY MICHAEL , LITTON DAVID A , ZIMMERMAN BENJAMIN JOSEPH , HAZEL BRIAN T
CPC classification number: C23C4/02 , C23C4/11 , C23C4/134 , C23C28/321 , C23C28/3215 , C23C28/3455 , C23C28/347 , F01D5/288 , F05D2300/13 , F05D2300/514 , Y10T428/249981 , Y10T428/31678
Abstract: A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.
Abstract translation: 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板,沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料,所述环境污染物与外层接触以改变外层的微观结构。
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公开(公告)号:WO2014007901A2
公开(公告)日:2014-01-09
申请号:PCT/US2013034769
申请日:2013-04-01
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HAZEL BRIAN T , LITTON DAVID A , MALONEY MICHAEL J
CPC classification number: C23C28/42 , C23C4/02 , C23C4/11 , C23C4/134 , C23C28/042 , C23C28/044 , C23C28/048 , C23C28/3215 , C23C28/3455 , C23C28/347 , Y10T428/249953 , Y10T428/26 , Y10T428/31678
Abstract: A turbine engine component has a substrate, a thermal barrier layer deposited onto the substrate, and a sealing layer of ceramic material deposited on an outer surface of the thermal barrier layer for limiting molten sand penetration. The thermal barrier layer and sealing layer are formed by suspension plasma spraying. A preferred sealing layer is gadolinium zirconate.
Abstract translation: 涡轮发动机部件具有基板,沉积在基板上的热障层,以及沉积在热障层外表面上的用于限制熔融砂渗透的陶瓷材料密封层。 隔热层和密封层通过悬浮等离子喷涂形成。 优选的密封层是锆酸钆。
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公开(公告)号:SG10201705492UA
公开(公告)日:2017-08-30
申请号:SG10201705492U
申请日:2013-03-05
Applicant: UNITED TECHNOLOGIES CORP
Inventor: LITTON DAVID A , TRYON BRIAN S
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公开(公告)号:SG158734A1
公开(公告)日:2010-02-26
申请号:SG2005084942
申请日:2003-08-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: LITTON DAVID A , ULION NICHOLAS E , TRUBELJA MLADEN F , MALONEY MICHAEL J , WARRIER SUNIL GOVINDA
IPC: C01F17/00 , F01D5/28 , C01G25/02 , C01G27/02 , C04B35/488 , C04B35/50 , C09D5/18 , C23C4/10 , C23C28/00 , C23C30/00 , F02C7/00 , F23R3/42
Abstract: A thermal barrier coating comprising more than 5 to 60 mol% of at least one of La 2 O 3 and Sm 2 O 3 , and from 5 to 60 mol% of at least one oxide having a formula A 2 O 3 where A is selected from the group consisting of Sc, In, Y, Pr, Nd, Eu, Sm, Gd, Dy, Er, Yb, and mixtures thereof; and the balance zirconia. In this coating system, the zirconia is preferably present in an amount greater than 40 mol% and the coating contains less than 10 vol% of phases with a pyrochlore structure. The present invention also broadly relates to an article having a metal substrate and a thermal barrier coating as discussed above.
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公开(公告)号:UA81716C2
公开(公告)日:2008-01-25
申请号:UAA200607046
申请日:2006-06-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PIETRASZKIEWICZ EDWARD F , SCHLICHTING KEVIN W , LITTON DAVID A , TERRY HEATHER A
Abstract: Способнанесениягибридногопокрытия, котороесоздаеттермическийбарьер, включаетмаскированиехотябычастипервойповерхностикомпонентапервыммаскировочнымслоем; нанесениепервогоматериалапокрытиянахотябычастьвторойповерхностикомпонента; извлечениевишеуказаногопервогомаскировочногослоя; необязательноемаскированиехотябычастивторойповерхностикомпонентавторыммаскировочнымслоем; нанесениевторогоматериалапокрытиянахотябычастьпервойповерхностикомпонента; иизвлечениевторогомаскировочногослоя.
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公开(公告)号:SG136042A1
公开(公告)日:2007-10-29
申请号:SG2007013337
申请日:2007-02-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MALONEY MICHAEL J , LITTON DAVID A , SEETHARAMAN VENKATARAMA K
Abstract: A coating suitable for use as a bondcoat for a thermal barrier coating system includes about 5 to about 10 weight percent of aluminum (Al), about 10 to about 18 weight percent of cobalt (Co), about 4 to about 8 weight percent of chromium (Cr), about 0 to about 1 weight percent of hafnium (Hf), about 0 to about 1 weight percent of silicon (Si), about 0 to about 1 percent of yttrium (Y), about 1.5 to about 2.5 weight percent of molybdenum (Mo), about 2 to about 4 weight percent of rhenium (Re), about 5 to about 10 weight percent of tantalum (Ta), about 5 to about 8 weight percent of tungsten (W), about 0 to about 1 weight percent of zirconium (Zr), and a remainder of nickel (Ni).
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公开(公告)号:SG134210A1
公开(公告)日:2007-08-29
申请号:SG2006085989
申请日:2006-12-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor: FRELING MELVIN , SCHLICHTING KEVIN W , MALONEY MICHAEL J , LITTON DAVID A , SMEGGIL JOHN G , SNOW DAVID B
Abstract: A turbine engine component is provided which has a substrate and a thermal barrier coating applied over the substrate. The thermal barrier coating comprises alternating layers of yttria- stabilized zirconia and a molten silicate resistant material. The molten silicate resistant outer layer may be formed from at least one oxide of a material selected from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, scandium, indium, zirconium, hafnium, and titanium or may be formed from a gadolinia-stabilized zirconia. If desired, a metallic bond coat may be present between the substrate and the thermal barrier coating system. A method for forming the thermal barrier coating system of the present invention is described.
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