公开(公告)号：US20170058686A1

公开(公告)日：2017-03-02

申请号：US14834866

申请日：2015-08-25

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Stephen Francis BANCHERI ,  Venkat Subramaniam VENKATARAMANI ,  Glen Harold KIRBY ,  Neelesh Nandkumar SARAWATE ,  Nicholas Edward ANTOLINO ,  Edip SEVINCER ,  Anthony Christopher MARIN

IPC: F01D11/00 ,  F01D25/00

CPC classification number: F01D11/003 ,  B05D1/005 ,  F01D9/041 ,  F01D11/005 ,  F01D25/005 ,  F05D2230/90 ,  F05D2240/11 ,  F05D2240/80 ,  F16J15/0887 ,  Y02T50/672

Abstract: A coated seal slot system for turbomachinery includes a first turbine component comprising a first groove having at least one first coating attached to at least a portion of the first groove of the first turbine component, a second turbine component comprising a second groove having at least one second coating attached to at least a portion of the second groove of the second turbine component. The first and the second turbine components are disposable adjacent to each other with the first groove having the first coating and the second groove having the second coating together forming a coated seal slot extending across a gap between the first turbine component and the second turbine component. A seal is disposable in the coated seal slot and extendable across the gap between the first and the second turbine components and engageable with the first coating and the second coating to inhibit leakage of gas through the gap.

Abstract translation: 一种用于涡轮机械的涂覆密封槽系统包括第一涡轮机部件，该第一涡轮机部件包括第一凹槽，该第一凹槽具有连接到第一涡轮机部件的第一凹槽的至少一部分的至少一个第一涂层，第二涡轮部件，其包括具有至少一个 第二涂层附着到第二涡轮机部件的第二凹槽的至少一部分。 第一和第二涡轮机部件是彼此相邻的，第一凹槽具有第一涂层，第二凹槽具有第二涂层，一起形成延伸穿过第一涡轮机部件和第二涡轮机部件之间的间隙的涂覆的密封槽。 密封件在涂覆的密封槽中是一次性的，并且可以跨越第一和第二涡轮机部件之间的间隙延伸并且可与第一涂层和第二涂层接合以抑制气体通过间隙的泄漏。

公开(公告)号：US20160194476A1

公开(公告)日：2016-07-07

申请号：US14589021

申请日：2015-01-05

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Don Mark LIPKIN ,  Nicholas Edward ANTOLINO ,  David POERSCHKE ,  Kevin Paul MCEVOY

IPC: C08K3/34 ,  C08K3/36

CPC classification number: C08K3/34 ,  B29C73/02 ,  B29K2083/00 ,  C08K3/36 ,  C08K2003/221 ,  C08K2003/2213 ,  C09D183/04 ,  C08K3/0083 ,  C08K3/105

Abstract: There is set forth herein a silicon-based patch formulation comprising about 25 to 66 percent by volume of a solvent; about 4 to 10 percent by volume of a silicon-comprising binding material; and about 30 to 65 percent by volume of a patching material, the patching material comprising particles having one or more non-actinide Group IIIA elements, wherein a molar ratio of the one or more non-actinide Group IIIA elements to silicon within the patch formulation is about 0.95 to 1.25.

Abstract translation: 本文提出了含有约25至66％（体积）溶剂的硅基贴片制剂; 约4至10体积％的含硅粘合材料; 和约30至65体积％的修补材料，所述修补材料包含具有一种或多种非锕系IIIA族元素的颗粒，其中所述一种或多种非锕系IIIA族元素与所述贴剂配方中的硅的摩尔比 为约0.95至1.25。

公开(公告)号：US20170247787A1

公开(公告)日：2017-08-31

申请号：US15431805

申请日：2017-02-14

Applicant: General Electric Company

Inventor： Atanu SAHA ,  Nicholas Edward ANTOLINO ,  Don Mark LIPKIN

IPC: C23C8/62 ,  C23C12/00 ,  C04B35/505

Abstract: Methods of forming an environmental barrier coating are disclosed. A method includes disposing a powder-based coating on a substrate, heat-treating the powder-based coating at a temperature greater than 800° C. and less than 1200° C. to form a porous coating that includes surface-connected pores, infiltrating at least some of the surface-connected pores of the porous coating with an infiltrant material to form an infiltrated coating, and sintering the infiltrated coating at a temperature greater than 1200° C. and less than 1500° C. to form the environmental barrier coating on the substrate.

公开(公告)号：US20170275747A1

公开(公告)日：2017-09-28

申请号：US15076825

申请日：2016-03-22

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Nicholas Edward ANTOLINO ,  Glen Harold KIRBY

IPC: C23C4/134 ,  C23C4/02 ,  C23C4/10

CPC classification number: C23C4/134 ,  C23C4/02 ,  C23C4/10 ,  C23C4/11

Abstract: A stacked up structure can include a first environmental barrier coating (EBC) layer and a second EBC layer. A first process can be used to form the first layer and a second process can be used to form the second layer. In one embodiment interfacial material can be formed for improved bonding of the second layer to the first layer. The interfacial material can define a continuous or discontinuous layer of nonuniform thickness.

公开(公告)号：US20160108510A1

公开(公告)日：2016-04-21

申请号：US14204367

申请日：2014-03-11

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Glen Harold KIRBY ,  Nicholas Edward ANTOLINO ,  Luc Stephane LEBLANC

IPC: C23C4/12 ,  C23C4/04

CPC classification number: C04B41/5045 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  C23C4/02 ,  C23C4/04 ,  C23C4/11 ,  C23C4/12 ,  C23C4/129 ,  C23C4/134 ,  C23C4/18 ,  F01D5/288 ,  F05D2300/15 ,  F05D2300/211 ,  C04B35/565 ,  C04B35/806 ,  C04B41/5096 ,  C04B41/4527 ,  C04B41/5024 ,  C04B2103/0021 ,  C04B41/526

Abstract: A rare earth silicate-based hermetic layer includes a thermal sprayed coating including a rare earth silicate having a hermetic microstructure. An environmental barrier coating includes a bond coat layer including silicon; and at least one rare earth silicate-based hermetic layer deposited on the bond coat layer by thermal spraying. The rare earth silicate-based hermetic layer includes a thermal sprayed coating including a rare earth silicate having a hermetic microstructure. An article for service in extreme environments may be provided with such an environmental barrier coating. A thermal spray feedstock for producing a rare earth silicate-based hermetic layer.

Abstract translation: 稀土硅酸盐系密封层包括具有密闭微结构的稀土硅酸盐的热喷涂层。 环境保护涂层包括包含硅的粘合涂层; 和通过热喷涂沉积在粘合涂层上的至少一种稀土硅酸盐基密封层。 稀土硅酸盐系密封层包括具有密闭微结构的稀土硅酸盐的热喷涂层。 在极端环境中用于服务的物品可以设置有这种环境屏障涂层。 用于生产稀土硅酸盐基密封层的热喷涂原料。

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

Inventor： Don Mark LIPKIN ,  Luc Stephane LEBLANC ,  Joshua Lee MARGOLIES ,  Nicholas Edward ANTOLINO

IPC: F01D11/12 ,  C23C4/00

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。