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公开(公告)号：EP2880195A4
公开(公告)日：2015-07-22
申请号：EP13825631
申请日：2013-07-31
Applicant: UNITED TECHNOLOGIES CORP
Inventor： NEAL JAMES W , LITTON DAVID A , BEERS RUSSELL A , ZIMMERMAN BENJAMIN JOSEPH , MALONEY MICHAEL J
CPC classification number: C23C14/042 , C23C14/044 , C23C14/30 , F05D2230/313
Abstract: A coating system for coating a part (10), such as a turbine blade or vane, has a mask (14) positioned adjacent to a first portion (16) of the part (10) to be coated and a mechanism (30) for moving the mask (14) relative to the part (10). The mechanism (30) may be a gear mechanism or a magnetic mechanism.
Abstract translation: 用于涂覆诸如涡轮叶片或叶片的部分（10）的涂覆系统具有邻近待涂覆的部分（10）的第一部分（16）定位的掩模（14）和用于 使面罩（14）相对于部件（10）移动。 机构（30）可以是齿轮机构或磁性机构。
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公开(公告)号：SG11201404599XA
公开(公告)日：2014-10-30
申请号：SG11201404599X
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：DE60334343D1
公开(公告)日：2010-11-11
申请号：DE60334343
申请日：2003-02-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor： GUPTA DINESH , LAMBERT DAVID L , TRUBELJA MLADEN F , MALONEY MICHAEL J , ULION NICHOLAS E , LITTON DAVID A
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公开(公告)号：SG165150A1
公开(公告)日：2010-10-28
申请号：SG2005084348
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 , C01G25/02 , C01G27/02 , C04B35/488 , C04B35/50 , C09D5/18 , C23C4/10 , F01D5/28 , C23C28/00 , C23C30/00 , F02C7/00 , F23R3/42 , C04B35/01 , C09D1/00 , C23C14/08 , C23C14/22 , C23C16/00
Abstract: A thermal barrier coating comprising from 0.5 to 1.0 mol% of at least one first oxide from the group consisting of CeO2, Pr203, Nd203, Eu2O3, Gd2O3, Dy203, Er2O3, Yb2O3, In2O3, Sc2O3, Y2O3, and mixtures thereof, combined with a second oxide selected from the group consisting of zirconia, hafnia, and ceria.
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公开(公告)号：AT483039T
公开(公告)日：2010-10-15
申请号：AT03250844
申请日：2003-02-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor： GUPTA DINESH , LAMBERT DAVID L , TRUBELJA MLADEN F , MALONEY MICHAEL J , ULION NICHOLAS E , LITTON DAVID A
Abstract: A superalloy article is disclosed having a thermal barrier coating. The article comprises a superalloy substrate (18), an adherent alumina layer (20) on the substrate, and a ceramic, thermally insulating layer (22) on the alumina layer. The ceramic layer has an overall thickness and comprises a relatively strain tolerant, columnar grain ceramic (24) on the alumina layer and relatively more thermally insulating ceramic (26) 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 comprise a material that is 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.
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Patent Agency Ranking
公开(公告)号：DE602005015049D1
公开(公告)日：2009-08-06
申请号：DE602005015049
申请日：2005-03-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor： LITTON DAVID A , ULION NICHOLAS E , TRUBELJA MLADEN F , MALONEY MICHAEL J , WARRIER SUNIL GOVINDA
IPC: F01D5/28 , C01F17/224 , C01G25/02 , C01G27/02 , C04B35/565 , C04B35/584 , C04B41/50 , C04B41/85 , C04B41/87 , C04B41/89 , C09D1/00 , C09D5/18 , C09D7/80 , C23C4/10 , C23C14/00 , C23C14/08 , C23C14/30 , C23C28/00 , C23C28/04 , C23C30/00 , F01D9/02 , F01D25/00 , F01N3/00 , F02C7/00 , F23R3/42
Abstract: A turbine component has a substrate formed from a ceramic material selected from the group consisting of a monolithic ceramic material and a composite ceramic material and a thermal barrier coating bonded to the substrate. In one embodiment, the ceramic material forming the substrate is selected from the group of silicon nitride and self-reinforced silicon nitride. In another embodiment, the ceramic material forming the substrate is selected from the group consisting of a silicon carbide-silicon carbide material and a carbon-carbon material. At least one bond coat layer may be interposed between the substrate and the thermal barrier coating.
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公开(公告)号：SG152050A1
公开(公告)日：2009-05-29
申请号：SG2005084660
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 , C01G25/02 , C01G27/02 , C04B35/488 , C04B35/50 , C09D5/18 , C23C4/10 , F01D5/28 , C23C28/00 , C23C30/00 , F02C7/00 , F23R3/42 , C09D1/00 , C23C16/00 , C04B35/01 , C23C14/08 , C23C14/22
Abstract: A thermal barrier coating comprising at least 15 mol% of at least one lanthanide sesquioxide, each said lanthanide sesquioxide having a formula A2O3 where A is selected from the group consisting of La, Pr, Nd, Sm, Eu, Tb, and mixtures thereof, and the balance comprising a first oxide selected from the group consisting of zirconia, ceria, and hafnia, said first oxide being present in an amount of at least 50 mol%.
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公开(公告)号：SG151094A1
公开(公告)日：2009-04-30
申请号：SG2005084934
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 , C01G25/02 , C01G27/02 , C04B35/488 , F01D5/28 , C04B35/50 , C09D5/18 , C23C4/10 , C23C28/00 , C23C30/00 , F02C7/00 , F23R3/42 , C23C16/00 , C23C14/22 , C23C14/08
Abstract: THERMAL BARRIER COATINGS WITH LOW THERMAL CONDUCTIVITY
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公开(公告)号：SG151093A1
公开(公告)日：2009-04-30
申请号：SG2005084926
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: THERMAL BARRIER COATINGS WITH LOW THERMAL CONDUCTIVITY
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公开(公告)号：SG151091A1
公开(公告)日：2009-04-30
申请号：SG2005084876
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 , C01G25/02 , C01G27/02 , C04B35/488 , C04B35/50 , C09D5/18 , C23C4/10 , F01D5/28 , C23C28/00 , C23C30/00 , F02C7/00 , F23R3/42 , C04B35/01 , C09D1/00 , C23C14/08 , C23C14/22 , C23C16/00
Abstract: THERMAL BARRIER COATINGS WITH LOW THERMAL CONDUCTIVITY
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