-
公开(公告)号：US20220010684A1
公开(公告)日：2022-01-13
申请号：US17485732
申请日：2021-09-27
Applicant: General Electric Company
Inventor： Donald Joseph BALDWIN , Joshua Lee MARGOLIES , Jacob John Kittleson
Abstract: A method of protecting a gas turbine component for operation in a high temperature environment that includes the gas turbine component including a substrate having a silicon-containing layer, wherein the gas turbine component has a curved surface; forming a flexible mask configured to cover the curved surface of the gas turbine component, the flexible mask including a plurality of slots disposed in a pattern; disposing the flexible mask in direct contact with the curved surface of the gas turbine component; applying a bondcoat onto the flexible mask and the gas turbine component, such that bondcoat fills the plurality of slots and contacts the curved surface; and removing the flexible mask by heat or chemical reaction, such that, after removing the flexible mask, the curved surface of the gas turbine component comprises a patterned bondcoat layer in the pattern defined by the flexible mask.
-
公开(公告)号：US20180363478A1
公开(公告)日：2018-12-20
申请号：US15623842
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Joshua Lee MARGOLIES , Victor John MORGAN , Matthew Troy HAFNER
CPC classification number: F01D5/288 , F01D9/02 , F01D9/023 , F01D25/005 , F01D25/007 , F01D25/24 , F05D2240/11 , F05D2240/122 , F05D2240/304 , F05D2240/35 , F05D2240/80 , F05D2250/292 , F05D2300/175 , F05D2300/6033 , F05D2300/611 , F23R3/002 , F23R3/007
Abstract: A method for forming a coated turbine component and a coated turbine component is provided. The method includes a step of providing a component having a substrate comprising a trailing edge face. The method further includes a step of applying a thermal barrier coating or environmental barrier coating selectively to the substrate to form a discontinuous transition from a hot gas path surface at the trailing edge face to discourage hot gas flow along the trailing edge face.
-
公开(公告)号：US20180106154A1
公开(公告)日：2018-04-19
申请号：US15292589
申请日：2016-10-13
Applicant: General Electric Company
Inventor： Donald Joseph BALDWIN , Joshua Lee MARGOLIES , Jacob John Kittleson
CPC classification number: F01D5/288 , B05B12/20 , B05D1/322 , B05D3/12 , C04B41/009 , C04B41/52 , C04B41/89 , F05D2220/32 , F05D2300/611 , C04B35/565 , C04B35/806 , C04B35/584 , C04B35/58085 , C04B41/4527 , C04B41/4572 , C04B41/5096 , C04B41/5024
Abstract: A method of forming an article includes forming a plurality of channels and ridges in a silicon-containing layer on a surface of a substrate of the article using a mask placed on the surface of the substrate or the silicon-containing layer.
-
公开(公告)号：US20150354393A1
公开(公告)日：2015-12-10
申请号：US14300666
申请日：2014-06-10
Applicant: GENERAL ELECTRIC COMPANY
CPC classification number: C23C4/01 , C23C4/10 , F01D11/122 , F01D11/125 , F05D2250/121 , F05D2250/184 , F05D2250/24 , F05D2250/283 , F05D2250/294 , F05D2300/514 , F05D2300/522
Abstract: Methods of manufacturing turbine shrouds with an abradable coating that balance the apparently contradictory requirements of high flowpath solidity, low blade tip wear, and good durability in service. The methods include obtaining a shroud substrate. The methods may include obtaining a coating system on the shroud substrate. The methods include forming an abradable coating on a surface of the coating system so as to form a substantially smooth flowpath surface. Forming the abradable coating includes forming a relatively dense scaffold and relatively porous filler regions in-between the relatively dense abradable scaffold. The methods may also include machining the abradable so as to achieve a substantially smooth flowpath surface comprising a relatively porous abradable phase surrounded by a relatively dense, high-durability corrale phase.
Abstract translation: 制造具有可磨损涂层的涡轮罩的方法，其平衡了高流动路径坚固性，低叶尖磨损和良好的耐久性在服务中的明显矛盾的要求。 所述方法包括获得护罩衬底。 所述方法可以包括获得护罩衬底上的涂覆系统。 所述方法包括在涂层系统的表面上形成可磨损涂层，以便形成基本平滑的流路表面。 形成可磨损涂层包括在相对致密的可磨损支架之间形成相对致密的支架和相对多孔的填料区域。 所述方法还可以包括对可磨损进行加工，以便实现基本上平滑的流路表面，该表面包括由相对致密的高耐久性Corrale相包围的相对多孔的可磨损相。
-
5.发明申请COATED ARTICLE, PROCESS OF COATING AN ARTICLE, AND METHOD OF USING A COATED ARTICLE 审中-公开涂层文章，涂料的方法和使用涂层物品的方法公开(公告)号：US20140193760A1
公开(公告)日：2014-07-10
申请号：US13737104
申请日：2013-01-09
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Warren Arthur NELSON , Yuk-Chiu LAU , Tamara Jean RUSSELL , Joshua Lee MARGOLIES
CPC classification number: C23C4/02 , C23C4/11 , C23C4/18 , Y10T428/24942 , Y10T428/249953
Abstract: A coated article, a process of coating an article, and a process of using an article are disclosed. The coated article includes a substrate, a porous coating material, and a thermal barrier coating material. The porous coating material includes a porosity between about 1 percent and about 20 percent, by volume. The thermal barrier coating material has a thermal conductivity that is lower than a thermal conductivity of the substrate. The porous coating material differs in one or both of composition and microstructure from the thermal barrier coating material. Additionally or alternatively, the porous coating material resists at least one of sintering, densification, and phase destabilization for a predetermined period at a predetermined temperature. The process of coating an article includes applying a coating to form the coated article.
Abstract translation: 公开了涂覆制品，涂布物品的方法和使用制品的方法。 涂覆制品包括基底，多孔涂层材料和热障涂层材料。 多孔涂层材料包括约1％至约20％（体积）之间的孔隙率。 热障涂层材料的导热率低于基板的热导率。 多孔涂层材料的组成和微结构中的一种或两者与热障涂层材料不同。 另外或替代地，多孔涂层材料在预定温度下抵抗烧结，致密化和相不稳定中的至少一个预定时间段。 涂覆制品的方法包括施加涂层以形成涂覆制品。
-
Patent Agency Ranking
公开(公告)号：US20140363684A1
公开(公告)日：2014-12-11
申请号：US13910290
申请日：2013-06-05
Applicant: General Electric Company
Inventor： Joshua Lee MARGOLIES , Theodore Robert GROSSMAN
CPC classification number: B05D3/14 , C23C4/02 , C23C4/11 , C23C4/12 , C23C4/134 , C23C4/18 , C23C24/08 , C23C24/085 , C23C24/087 , F01D5/284 , F01D5/288 , F01D25/007 , F05D2230/312 , Y10T428/31678
Abstract: A coating process and coated article are disclosed. The coating process includes positioning an article relative to an inductor, heating the article with the inductor, then applying a coating material over the article to form a crystalline coating. The heating of the article increases a first temperature of a surface of the article to a second temperature favoring crystal formation. Another coating process includes positioning an article, uniformly heating a surface of the article to a second temperature favoring crystal formation, then applying an environmental barrier coating material over the surface of the article to form a crystalline environmental barrier coating. The application of the environmental barrier coating is performed through air plasma spray deposition. The coated article includes an article having a complex geometry, and a crystalline coating applied on a surface of the article. The crystalline coating includes increased resistant to delamination.
Abstract translation: 公开了涂覆工艺和涂覆制品。 涂覆工艺包括相对于电感器定位物品，用电感器加热制品，然后在制品上施加涂层材料以形成结晶涂层。 制品的加热将制品表面的第一温度增加到有利于晶体形成的第二温度。 另一种涂布方法包括定位物品，将制品的表面均匀加热至有利于晶体形成的第二温度，然后在制品的表面上施加环境阻挡涂层材料以形成结晶环境屏障涂层。 环境阻隔涂层的应用通过空气等离子体喷涂沉积来进行。 涂覆制品包括具有复杂几何形状的制品，以及施加在制品表面上的结晶涂层。 结晶涂层包括增加的耐分层性。
-
7.发明申请公开(公告)号：US20140272467A1
公开(公告)日：2014-09-18
申请号：US13801547
申请日：2013-03-13
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Jon Conrad SCHAEFFER , Surinder Singh PABLA , Paul Stephen DIMASCIO , Krishnamurthy ANAND , Joshua Lee MARGOLIES , Padmaja PARAKALA
CPC classification number: F01D25/08 , C23C28/042 , F01D5/288 , F01D25/005
Abstract: A process of forming a calcium-magnesium-aluminosilicate (CMAS) penetration resistant coating, and a CMAS penetration resistant coating are disclosed. The process includes providing a thermal barrier coating having a dopant, and exposing the thermal barrier coating to calcium-magnesium-aluminosilicate and gas turbine operating conditions. The exposing forming a calcium-magnesium-aluminosilicate penetration resistant layer. The coating includes a thermal barrier coating composition comprising a dopant selected from the group consisting of rare earth elements, non-rare earth element solutes, and combinations thereof. Additional or alternatively, the coating includes a thermal barrier coating and an impermeable barrier layer or a washable sacrificial layer positioned on an outer surface of the thermal barrier coating.
Abstract translation: 公开了一种形成钙 - 镁 - 硅铝酸盐（CMAS）渗透性涂层和CMAS渗透涂层的方法。 该方法包括提供具有掺杂剂的热障涂层，并将热障涂层暴露于钙 - 镁 - 硅铝酸盐和燃气轮机的操作条件。 暴露形成钙镁镁硅酸盐防渗层。 该涂层包括一种热障涂层组合物，其包含选自稀土元素，非稀土元素溶质及其组合的掺杂剂。 附加或替代地，涂层包括热障涂层和定位在热障涂层的外表面上的不可渗透阻挡层或可洗涤的牺牲层。
-
8.发明申请公开(公告)号：US20180363477A1
公开(公告)日：2018-12-20
申请号：US15623802
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Matthew Troy HAFNER , Joshua Lee MARGOLIES
Abstract: A coated ceramic matrix composite or metallic component and a gas turbine assembly is provided. The component comprises a substrate comprising a first surface and a hot gas path surface. The hot gas path surface is arranged and disposed to contact a hot gas flow when the component is installed in the gas turbine. The first surface is disposed at an angle to the hot gas path surface and opposes at least one adjacent component when the component is installed in the gas turbine. The component further comprises an angled or rounded feature extending from the first surface to the hot gas path surface. The component further comprises an environmental barrier coating or thermal barrier coating on at least a portion of the hot gas path surface. The angled or rounded feature reduces an incidence angle of the hot gas flow onto the first surface. The gas turbine assembly comprises a plurality of the coated components.
-
9.发明申请公开(公告)号：US20180363476A1
公开(公告)日：2018-12-20
申请号：US15623763
申请日：2017-06-15
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Matthew Troy HAFNER , Joshua Lee MARGOLIES
Abstract: A coated ceramic matrix composite component and a gas turbine assembly are provided. The coated ceramic matrix composite component comprises a substrate comprising an endface surface and a hot gas path surface. The hot gas path surface is arranged and disposed to contact a hot gas path when the component is installed in the gas turbine assembly. The endface surface is disposed at an endface angle to the hot gas path surface and opposing at least one adjacent component when the component is installed in the gas turbine assembly. The coated ceramic matrix composite component further comprises an environmental barrier coating on at least a portion of the endface surface.
-
10.发明申请NOVEL ARCHITECTURES FOR ULTRA LOW THERMAL CONDUCTIVITY THERMAL BARRIER COATINGS WITH IMPROVED EROSION AND IMPACT PROPERTIES 审中-公开具有改进的腐蚀和冲击特性的超低导热性热障涂层的新型结构公开(公告)号：US20150233256A1
公开(公告)日：2015-08-20
申请号：US13741848
申请日：2013-01-15
Applicant: General Electric Company
Inventor： Krishnamurthy ANAND , James Anthony RUUD , Surinder Singh PABLA , Joshua Lee MARGOLIES , Padmaja PARAKALA , Larry Steven ROSENZWEIG
CPC classification number: F01D5/284 , C23C4/02 , C23C4/11 , C23C4/134 , F01D5/28 , F01D5/288 , F05D2300/2118 , Y10T428/12549 , Y10T428/12618
Abstract: A thermal barrier coating system for metal components in a gas turbine engine having an ultra low thermal conductivity and high erosion resistance, comprising an oxidation-resistant bond coat formed from an aluminum rich material such as MCrAlY and a thermal insulating ceramic layer over the bond coat comprising a zirconium or hafnium oxide lattice structure (ZrO2 or HfO2) and an oxide stabilizer compound comprising one or more of the compounds ytterbium oxide (Yb2O3), yttria oxide (Y2O3), hafnium oxide (HfO2), lanthanum Oxide (La2O3), tantalum oxide (Ta2O5) or zirconium oxide (ZrO2). The invention includes a new method of forming the ceramic-based thermal barrier coatings using a liquid-based suspension containing microparticles comprised of at least one of the above compounds ranging in size between about 0.1 and 5 microns. The coatings form a tortuous path of ceramic interfaces that increase the coating toughness while preserving the ultra low thermal conductivity.
Abstract translation: 一种用于具有超低热导率和高耐侵蚀性的燃气轮机中的金属部件的隔热涂层系统，包括由富铝材料如MCrAlY形成的抗氧化粘合涂层和粘结涂层上的绝热陶瓷层 包括锆或铪氧化物晶格结构（ZrO 2或HfO 2）和包含一种或多种化合物氧化镱（Yb 2 O 3），氧化钇（Y 2 O 3），氧化铪（HfO 2），氧化镧（La 2 O 3），钽 氧化物（Ta2O5）或氧化锆（ZrO2）。 本发明包括使用包含由至少一种上述化合物构成的微粒的液体基悬浮液形成陶瓷基热障涂层的新方法，其尺寸范围为约0.1至5微米。 涂层形成陶瓷界面的曲折路径，从而提高涂层韧性，同时保持超低热导率。
-
-
-
-
-
-
-
-
-
Search Results
10
records
(took 0.024 seconds)
