公开(公告)号：US10577950B2

公开(公告)日：2020-03-03

申请号：US15873406

申请日：2018-01-17

Applicant: Rolls-Royce Corporation

Inventor： Sean E. Landwehr ,  Michael Cybulsky ,  Kang N. Lee

IPC: C04B41/52 ,  F01D5/28 ,  C04B41/89 ,  C04B41/00 ,  C23C24/08 ,  C04B35/628 ,  F23R3/00 ,  C04B41/50

Abstract: An article having a substrate that includes a ceramic or a ceramic matrix composite, a bond layer on the substrate that includes silicon metal and a boria stabilizing agent, and at least one additional layer on the bond layer.

公开(公告)号：US10047614B2

公开(公告)日：2018-08-14

申请号：US14879931

申请日：2015-10-09

Applicant: Rolls-Royce Corporation

Inventor： Sungbo Shim ,  Sean E. Landwehr

IPC: F01D5/28 ,  C04B41/50 ,  C04B41/85 ,  C04B41/89 ,  F01D5/30 ,  C23C16/50 ,  C23C16/34 ,  C23C16/40 ,  C04B41/52

Abstract: In some examples, an article may include a substrate and a coating on the substrate. The substrate may include a superalloy, a ceramic, or a ceramic matrix composite. The coating may include a first set of layers and a second set of layers. At least one layer of the first set of layers is between two layers of the second set of layers. The at least one layer of the first set of layers comprises one of amorphous silica or silicon nitride, and the at least two layers of the second set of layers comprises the other of amorphous silica or silicon nitride.

公开(公告)号：US09803486B2

公开(公告)日：2017-10-31

申请号：US14144939

申请日：2013-12-31

Applicant: Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

Inventor： Ted J. Freeman ,  Robert F. Proctor ,  Sean E. Landwehr ,  Adam L. Chamberlain

IPC: F01D5/28 ,  F01D9/02 ,  F01D5/18 ,  F01D9/04 ,  C04B37/00

CPC classification number: F01D9/02 ,  C04B37/005 ,  C04B2237/083 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/61 ,  C04B2237/76 ,  C04B2237/84 ,  F01D5/189 ,  F01D5/284 ,  F01D5/288 ,  F01D9/041 ,  F01D9/044 ,  F05D2260/20 ,  F05D2300/211 ,  F05D2300/6033 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676

Abstract: One aspect of the present disclosure includes a turbine vane assembly comprising a vane made from ceramic matrix composite material having an outer wall extending between a leading edge and a trailing edge and between a first end and an opposing second end; an endwall made at least partially from a ceramic matrix composite material configured to engage the first end of the vane; and a retaining region including corresponding bi-cast grooves formed adjacent the first end of the vane and a receiving aperture formed in the endwall; wherein a bond is formed in the retaining region to join the vane and endwall together.

公开(公告)号：US09630885B2

公开(公告)日：2017-04-25

申请号：US14864082

申请日：2015-09-24

Applicant: Rolls-Royce High Temperature Composites, Inc. ,  Rolls-Royce Corporation

Inventor： Anthony Martin Goetz ,  Robert Shinavski ,  Stephen Isaiah Harris ,  Sean E. Landwehr

IPC: B32B9/00 ,  C04B41/45 ,  C04B41/87 ,  C04B41/85 ,  C04B41/53 ,  C04B41/52 ,  C04B41/50 ,  C04B35/565 ,  C04B35/573 ,  C04B35/626 ,  C04B35/628 ,  C04B35/634 ,  C04B35/636

CPC classification number: C04B35/806 ,  C04B35/565 ,  C04B35/573 ,  C04B35/62281 ,  C04B35/624 ,  C04B35/6261 ,  C04B35/6263 ,  C04B35/6264 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62865 ,  C04B35/62868 ,  C04B35/62873 ,  C04B35/634 ,  C04B35/636 ,  C04B35/6365 ,  C04B35/65 ,  C04B35/657 ,  C04B41/4584 ,  C04B41/5059 ,  C04B41/5096 ,  C04B41/52 ,  C04B41/53 ,  C04B41/85 ,  C04B41/87 ,  C04B2235/3826 ,  C04B2235/428 ,  C04B2235/48 ,  C04B2235/5224 ,  C04B2235/5228 ,  C04B2235/5232 ,  C04B2235/5236 ,  C04B2235/524 ,  C04B2235/5244 ,  C04B2235/5248 ,  C04B2235/5436 ,  C04B2235/5481 ,  C04B2235/6023 ,  C04B2235/616 ,  C04B2235/656 ,  C04B2235/6581

Abstract: A method of forming a composite article includes impregnating an inorganic fiber preform with a slurry composition. The slurry composition includes a particulate, a solvent, and a pre-gellant material. Gelling of the pre-gellant material in the slurry composition is initiated to immobilize the particulate and yield a gelled article, and substantially all solvent is removed from the gelled article to form a green composite article. The green composite article is then infiltrated with a molten infiltrant to form the composite article.

公开(公告)号：US20170044070A1

公开(公告)日：2017-02-16

申请号：US15229786

申请日：2016-08-05

Applicant: Rolls-Royce High Temperature Composites Inc. ,  Rolls-Royce Corporation

Inventor： Stephen I. Harris ,  Robert J. Shinavski ,  Sungbo Shim ,  Sean E. Landwehr

IPC: C04B35/80 ,  C04B37/00 ,  C23C16/04

CPC classification number: C04B35/806 ,  C04B35/565 ,  C04B35/62857 ,  C04B35/6286 ,  C04B35/62863 ,  C04B35/62876 ,  C04B35/62884 ,  C04B35/62894 ,  C04B35/62897 ,  C04B37/005 ,  C04B37/006 ,  C04B2235/3826 ,  C04B2235/428 ,  C04B2235/5244 ,  C04B2235/614 ,  C04B2235/616 ,  C04B2237/08 ,  C04B2237/083 ,  C04B2237/122 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/708 ,  C04B2237/72 ,  C23C16/045

Abstract: A ceramic matrix composite component and methods of making are described herein. The ceramic matrix composite may include a silicon containing matrix and refractory fibers embedded within the silicon containing matrix. The ceramic matrix composite component may further include a silicide layer sandwiched between the silicon containing matrix and the refractory fibers. A method of forming a ceramic matrix composite may include infiltrating a fluid that includes a refractory metal element containing compound into a fiber preform that includes fibers. The method may further include depositing the refractory metal element from the refractory metal element containing compound onto the fibers and forming, from the refractory metal element deposited onto the fibers, a refractory metal silicide.

Abstract translation: 本文描述了陶瓷基复合材料组件及其制造方法。 陶瓷基复合材料可以包括含硅基体和嵌入含硅基体内的难熔纤维。 陶瓷基复合材料组件还可以包括夹在含硅基质和耐火纤维之间的硅化物层。 形成陶瓷基质复合材料的方法可以包括将含有难熔金属元素的化合物的流体渗透到包括纤维的纤维预制棒中。 该方法还可以包括将难熔金属元素从含难熔金属元素的化合物沉积到纤维上，并从沉积在纤维上的耐火金属元素形成难熔金属硅化物。

公开(公告)号：US20160368827A1

公开(公告)日：2016-12-22

申请号：US15188159

申请日：2016-06-21

Applicant: Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce High Temperature Composites, Inc.

Inventor： Sean E. Landwehr ,  Daniel K. Vetters ,  Ted J. Freeman ,  Robert J. Shinavski

IPC: C04B35/80 ,  C04B35/565 ,  C04B41/87

CPC classification number: C04B35/806 ,  B32B18/00 ,  C04B35/565 ,  C04B35/573 ,  C04B37/001 ,  C04B41/87 ,  C04B2235/3826 ,  C04B2235/422 ,  C04B2235/5244 ,  C04B2235/612 ,  C04B2235/614 ,  C04B2235/616 ,  C04B2235/77 ,  C04B2237/365 ,  C04B2237/38 ,  C04B2237/60 ,  C04B2237/61 ,  C04B2237/84 ,  F05D2240/11 ,  F05D2240/15 ,  F05D2300/20 ,  F05D2300/6033 ,  F23M2900/05004 ,  F23R3/002 ,  F23R3/007

Abstract: Integrated ceramic matrix composite components for use in gas turbine engines are disclosed along with methods for making the same. The methods include coinfiltrating a greenbody assembly with ceramic matrix to produce an integrated component.

Abstract translation: 公开了用于燃气涡轮发动机的集成陶瓷基复合材料组件及其制造方法。 所述方法包括将具有陶瓷基质的生物体组合体渗透以产生集成的组分。

公开(公告)号：US20160356499A1

公开(公告)日：2016-12-08

申请号：US15172975

申请日：2016-06-03

Applicant: Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce Corporation

Inventor： Ted J. Freeman ,  Thomas D. Nixon ,  Sean E. Landwehr ,  Aaron D. Sippel ,  Donald W. Reinhart

IPC: F23R3/00 ,  C23C16/04 ,  F01D5/28 ,  C23C16/44 ,  F02C3/04 ,  F01D9/02

CPC classification number: F23R3/007 ,  F01D5/284 ,  F01D25/246 ,  F05D2230/314 ,  F05D2240/11 ,  F05D2240/12 ,  F05D2300/2261 ,  F05D2300/6033 ,  F05D2300/611

Abstract: An assembly comprising a ceramic matrix composite component, a ceramic insert, and a ply and a method for producing the same. The ceramic matrix composite component may comprise silicon carbide fibers in a silicon carbide matrix. The ceramic inset may be adjacent to the ceramic matrix composite component. The ply may at least partially cover the ceramic insert such that the ceramic insert may be sandwiched between the ply and the ceramic matrix composite component, and the ply may extend beyond the ceramic insert in at least one direction so that the ply is joined to the ceramic matrix composite. The ply may comprise at least one layer of silicon carbide fibers or carbon fibers in a silicon carbide matrix.

Abstract translation: 一种组件，其包括陶瓷基复合材料组件，陶瓷嵌件和层及其制造方法。 陶瓷基复合材料组分可包括碳化硅基体中的碳化硅纤维。 陶瓷插图可以与陶瓷基复合元件相邻。 帘布层可以至少部分地覆盖陶瓷插入件，使得陶瓷插入件可以夹在层和陶瓷基复合构件之间，并且层可以在至少一个方向上延伸超过陶瓷插入件，使得层与 陶瓷基复合材料。 层可以包括碳化硅基体中的至少一层碳化硅纤维或碳纤维。

公开(公告)号：US20160356497A1

公开(公告)日：2016-12-08

申请号：US15172985

申请日：2016-06-03

Applicant: Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce Corporation

Inventor： Ted J. Freeman ,  Thomas D. Nixon ,  Sean E. Landwehr ,  Aaron D. Sippel ,  Donald W. Reinhart

IPC: F23R3/00 ,  B32B38/04 ,  B32B37/16 ,  B32B38/08 ,  F02C3/04 ,  F01D9/04

CPC classification number: F23R3/002 ,  B32B37/18 ,  B32B38/08 ,  B32B2038/042 ,  B32B2262/105 ,  B32B2315/02 ,  B32B2603/00 ,  F01D5/284 ,  F01D25/246 ,  F05D2240/11 ,  F05D2240/12 ,  F05D2300/2261 ,  F05D2300/6033 ,  F05D2300/611 ,  F05D2300/614

Abstract: An assembly comprising a structural component and a sacrificial layer, and method for producing the same. The structural component may comprise silicon carbide fibers within a silicon carbide matrix. The sacrificial layer may be joined to the structural component and may comprising unarranged ceramic fibers, wherein the sacrificial layer may comprise a volume fiber fraction lower than a volume fiber fraction of the structural component.

Abstract translation: 包括结构部件和牺牲层的组件及其制造方法。 结构部件可以包括碳化硅基体内的碳化硅纤维。 牺牲层可以结合到结构部件上并且可以包括未经修整的陶瓷纤维，其中牺牲层可以包括低于结构部件的体积纤维部分的体积纤维部分。

公开(公告)号：US20140271144A1

公开(公告)日：2014-09-18

申请号：US14095714

申请日：2013-12-03

Applicant: Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce Corporation

Inventor： Sean E. Landwehr ,  William Westphal ,  Ted J. Freeman ,  Adam L. Chamberlain

IPC: F01D11/08 ,  B23P15/04

CPC classification number: F01D11/08 ,  B23P15/04 ,  F01D9/04 ,  F01D25/246 ,  F05D2230/64 ,  F05D2300/6033 ,  Y02T50/672 ,  Y10T29/49321

Abstract: A turbine shroud for a gas turbine engine includes an annular metallic carrier, a blade track, and a cross-key connection formed between the annular metallic carrier and the ceramic blade track. The cross-key connection is formed between the annular metallic carrier and inserts included in the blade track. The inserts are bonded to an annular runner also included in the blade track by a braze layer.

Abstract translation: 用于燃气涡轮发动机的涡轮罩包括环形金属载体，叶片轨道和形成在环形金属载体和陶瓷叶片轨道之间的交叉键连接。 交叉键连接形成在环形金属托架和包括在刀片轨道中的刀片之间。 刀片通过钎焊层结合到也包括在刀片轨道中的环形转轮上。

公开(公告)号：US11827986B2

公开(公告)日：2023-11-28

申请号：US16355056

申请日：2019-03-15

Applicant: Rolls-Royce Corporation ,  Rolls-Royce plc ,  Rolls-Royce North American Technologies, Inc.

Inventor： Sean E. Landwehr ,  Ngunjoh Lawrence Ndamka ,  Matthew R. Gold ,  Michael Cybulsky ,  Li Li ,  Robert Golden

IPC: C23C4/04 ,  C04B41/50 ,  C23C28/00 ,  C23C4/134 ,  C23C14/06 ,  C23C14/30 ,  C23C28/04 ,  C04B41/45

CPC classification number: C23C28/345 ,  C04B41/459 ,  C04B41/5024 ,  C23C4/04 ,  C23C4/134 ,  C23C14/06 ,  C23C14/30 ,  C23C28/042 ,  C23C28/044 ,  C23C28/321 ,  C23C28/322 ,  C23C28/3215 ,  C23C28/34 ,  C23C28/347 ,  C23C28/3455 ,  Y10T428/249953

Abstract: In some examples, an article may include a substrate and a coating system on the substrate. The coating system may include a layer comprising a plurality of voids, wherein respective voids of the plurality of voids define respective void volumes; and a nucleating agent within at least some of the respective void volumes of the layer, wherein the nucleating agent is configured to induce crystallization of the molten CMAS. The coating system may include an environmental barrier coating, thermal barrier coating, and/or abradable coating.