-
41.发明公开Yttria-stabilized zirconia coating with a molten silicate resistant outer layer 审中-公开氧化钇的涂层具有稳定的熔融硅酸盐抗性外层的氧化锆
公开(公告)号：EP1811061A2
公开(公告)日：2007-07-25
申请号：EP07250225.5
申请日：2007-01-19
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Freling, Melvin , Schlichting, Kevin W. , Maloney, Michael J. , Litton, David A. , Smeggil, John G. , Snow, David B.
CPC classification number: C23C26/00 , C23C28/042 , C23C28/048 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , F01D5/288 , Y10T428/12806 , Y10T428/12861 , Y10T428/12944 , Y10T428/26 , Y10T428/263 , Y10T428/264 , Y10T428/265
Abstract: A turbine engine component is provided which has a substrate (14), a yttria-stabilized zirconia coating (10) applied over the substrate (14), and a molten silicate resistant outer layer (20). The molten silicate resistant outer layer (20) is formed from gadolinia or gadolinia-stabilized zirconia. A method for forming the coating system of the present invention is described.
Abstract translation: 一种涡轮发动机部件提供一种具有底物（14），施加在基片（14）一氧化钇稳定的氧化锆涂层（10），和熔融硅酸盐抗性外层（20）。 所述熔融硅酸盐抗性外层（20）形成为从氧化钆或氧化钆稳定氧化锆。 描述了一种用于形成本发明的涂层系统的方法。
-
公开(公告)号：EP1647611A3
公开(公告)日：2007-05-09
申请号：EP05255381.5
申请日：2005-09-02
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Burd, Steven W. , Schlichting, Kevin W. , Sonntag, Robert M.
CPC classification number: F01D5/288 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C28/36 , F05D2230/90 , F05D2300/2112 , Y10T428/12535 , Y10T428/31678
Abstract: An article has a metallic substrate having a first emissivity. A thermal barrier coating atop the substrate may have an emissivity that is a substantial fraction of the first emissivity.
-
43.发明公开Single crystal articles having controlled crystallographic orientation 审中-公开Einkristallartikeln mit gesteuerter Kristallorientierung
公开(公告)号：EP1584871A2
公开(公告)日：2005-10-12
申请号：EP05252128.3
申请日：2005-04-05
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Schlichting, Kevin W. , Murray, Stephen D. , Cetel, Alan D. , Marcin, John J. Jr.
CPC classification number: F23R3/002 , C22C19/056 , C22C19/057 , C30B29/52 , F23M5/00 , F23M2900/05004 , F23R2900/00005 , F23R2900/00018 , F23R2900/00019 , Y10T428/12944
Abstract: An article has a characteristic thermal-mechanical stress principal direction. The article has a single crystal substrate having a lowest modulus direction within a target alignment with the principal direction.
Abstract translation: 一个物品具有特征的热机械应力主方向。 该制品具有在与主方向对准的目标对准中具有最低模数方向的单晶衬底。
-
公开(公告)号：EP3276041A1
公开(公告)日：2018-01-31
申请号：EP17182767.8
申请日：2017-07-24
Applicant: United Technologies Corporation
Inventor： Litton, David A. , Gero, Peter F. , Schlichting, Kevin W.
CPC classification number: C23C16/45525 , C23C4/134 , C23C14/083 , C23C14/30 , C23C14/505 , C23C14/568 , C23C16/46 , F01D5/288 , F01D9/02 , F01D11/08 , F02C7/24 , F05D2220/32 , F05D2230/31 , F05D2230/90 , F05D2240/35 , F05D2300/175 , F23R3/002 , F23R3/28
Abstract: An apparatus for depositing a coating on a part comprises: a chamber (42); a source (48) of a coating material, positioned to communicate the coating material to the part in the chamber; a plurality of thermal hoods (162); and means for moving a hood of the plurality of thermal hoods from an operative position and replacing the hood with another hood of the plurality of hoods.
Abstract translation: 一种用于在部件上沉积涂层的设备包括：腔室（42）; 一个涂料材料源（48），该涂料材料的位置使涂料与腔室中的部件连通; 多个热罩（162）; 以及用于使所述多个热罩的罩从工作位置移动并且用所述多个罩中的另一个罩更换罩的装置。
-
公开(公告)号：EP1889949B1
公开(公告)日：2012-05-30
申请号：EP07253182.5
申请日：2007-08-13
Applicant: United Technologies Corporation
Inventor： Schlichting, Kevin W. , Litton, David A. , Maloney, Michael J. , Freling, Melvin , Smeggil, John G. , Snow, David
CPC classification number: C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/42 , C23C30/00
-
Patent Agency Ranking46.发明公开Layered thermal barrier coating with blended transition and method of application 有权GeschichteteWärmesperrenbeschichtungmitMischübergangsowie Anwendungsverfahren
公开(公告)号：EP2388354A1
公开(公告)日：2011-11-23
申请号：EP11250422.0
申请日：2011-04-04
Applicant: United Technologies Corporation
Inventor： Gero, Peter F. , Schlichting, Kevin W. , Neal, James W.
CPC classification number: F01D25/08 , C23C4/11 , C23C14/027 , C23C14/228 , C23C30/00 , F01D5/288 , F05D2230/90 , F05D2260/95 , F05D2300/502 , F05D2300/611 , Y10T428/12021 , Y10T428/12458 , Y10T428/1259 , Y10T428/12618 , Y10T428/12736 , Y10T428/12743 , Y10T428/26 , Y10T428/266
Abstract: A multilayer coating (100) includes a bond coat layer (102) and a first barrier layer (104) applied on the bond coat layer. The first barrier layer (104) has a compositional gradient comprising a majority of a first rare earth stabilized zirconia material proximate the bond coat layer (102) to a majority of a second rare earth stabilized zirconia material away from the bond coat layer. The first and second rare earth stabilized zirconia materials are different.
Abstract translation: 多层涂层（100）包括粘合涂层（102）和施加在粘合涂层上的第一阻挡层（104）。 第一阻挡层（104）具有组成梯度，该组成梯度包括靠近接合涂层（102）的大部分第一稀土稳定的氧化锆材料与远离粘合涂层的大部分第二稀土稳定的氧化锆材料。 第一和第二稀土稳定氧化锆材料是不同的。
-
47.发明公开Thermal barrier coating compositions, processes for applying same and articles coated with same 审中-公开热障涂层组合物，用于施加和涂层组分的方法
公开(公告)号：EP1806431A3
公开(公告)日：2010-11-03
申请号：EP07250089.5
申请日：2007-01-10
Applicant: United Technologies Corporation
Inventor： Litton, David A. , Maloney, Michael J. , Freling, Melvin , Smeggil, John G. , Snow, David B. , Schlichting, Kevin W.
CPC classification number: C04B35/01 , C04B35/486 , C04B2235/75 , C04B2235/76 , C04B2235/762 , C04B2235/764 , C04B2235/767 , C23C26/00 , C23C28/042 , C23C28/048 , C23C28/321 , C23C28/3215 , C23C28/322 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C28/36 , Y02T50/67 , Y10T428/26
Abstract: A process of coating an article includes the steps of (1) applying a ceramic based compound to at least one surface of an article to form a layer of ceramic based compound; (2) applying at least one inert compound upon the ceramic based compound layer to form a protective layer, wherein the at least one inert compound is composed of a first inert compound having a cubic crystalline structure of formula (I) A 3 B 2 X 3 O 12 , or a second inert compound comprising a hexagonal crystalline structure of formula (II) A 4 B 6 X 6 O 26 , or a mixture of the first inert compound and the second inert compound; and (3) heat treating the coated article.
-
公开(公告)号：EP1647611B1
公开(公告)日：2009-12-16
申请号：EP05255381.5
申请日：2005-09-02
Applicant: United Technologies Corporation
Inventor： Burd, Steven W. , Schlichting, Kevin W. , Sonntag, Robert M.
CPC classification number: F01D5/288 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , C23C28/36 , F05D2230/90 , F05D2300/2112 , Y10T428/12535 , Y10T428/31678
-
公开(公告)号：EP1900848A3
公开(公告)日：2009-08-19
申请号：EP07253477.9
申请日：2007-09-03
Applicant: United Technologies Corporation
Inventor： Schlichting, Kevin W. , Litton, David A. , Smeggil, John G. , Maloney, Michael J. , Freling, Melvin , Snow, David B.
CPC classification number: C23C4/02 , C23C28/321 , C23C28/3215 , C23C28/34 , C23C28/345 , C23C28/3455 , C23C28/42 , C23C30/00 , F01D5/288 , F05D2300/501 , F05D2300/506
Abstract: A thermal barrier coating system for use on a turbine engine component which reduces sand related distress is provided. The coating system comprises at least one first layer of a stabilized material selected from the group consisting of zirconia, hafnia, and titania and at least one second layer containing at least one of oxyapatite and garnet. Where the coating system comprises multiple first layers and multiple second layers, the layers are formed or deposited in an alternating manner.
-
50.发明公开Porous protective clothing for turbine engine components 有权PoröseSchutzverkleidungfürTurbinenmotorkomponenten
公开(公告)号：EP2072634A2
公开(公告)日：2009-06-24
申请号：EP08253922.2
申请日：2008-12-09
Applicant: United Technologies Corporation
Inventor： Schlichting, Kevin W. , Freling, Melvin
CPC classification number: C23C24/04 , C23C10/02 , C23C10/60 , C23C28/321 , C23C28/3215 , C23C28/325 , C23C28/345 , C23C28/3455 , Y10T29/49229 , Y10T29/49982 , Y10T428/12479 , Y10T428/12507 , Y10T428/12611 , Y10T428/249953
Abstract: A method for coating a substrate of a turbine engine component comprising cold spray depositing a metal-based material onto a surface of the substrate, and heating the deposited metal-based material to increase the porosity of the deposited metal-based material.
Abstract translation: 一种用于涂覆涡轮发动机部件的基板的方法，包括将基于金属的材料冷喷射沉积到所述基板的表面上，以及加热所沉积的金属基材料以增加沉积的金属基材料的孔隙率。
-
-
-
-
-
-
-
-
-
Search Results
77
records
(took 0.032 seconds)
