公开(公告)号：US10422234B2

公开(公告)日：2019-09-24

申请号：US15106608

申请日：2014-08-14

Applicant: United Technologies Corporation

Inventor： James T. Roach ,  Benjamin T. Fisk ,  Grant O. Cook, III

IPC: F01D5/14 ,  F01D5/30 ,  F01D5/28 ,  C09J5/00 ,  F01D11/08 ,  F01D25/24 ,  C23C14/22 ,  C23C16/44 ,  C23C18/16 ,  C23C24/04 ,  F01D9/04 ,  F01D25/00

Abstract: A compliant attachment for an organic matrix composite component that is configured to interface with a mating component is disclosed. The compliant attachment may comprise an inner surface configured to bond to an interfacing surface of a body portion of the organic matrix component, and an outer surface configured to interface with the mating component. The compliant attachment may have a coefficient of thermal expansion intermediate between a coefficient of thermal expansion of the body portion of the organic matrix composite component and a coefficient of thermal expansion of the mating component.

公开(公告)号：US20160368238A1

公开(公告)日：2016-12-22

申请号：US14903880

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： William Bogue ,  Grant O. Cook, III ,  Gary M. Lomasney ,  Joseph Parkos ,  Colin J. Kling ,  Charles R. Watson

IPC: B32B3/26 ,  B32B15/20 ,  C25D5/56 ,  C23C16/06 ,  C25D11/20 ,  C25D9/04 ,  B32B15/08 ,  C23C14/20

CPC classification number: C25D5/56 ,  B05D5/00 ,  B05D7/02 ,  B22C7/023 ,  B22C9/043 ,  B22C9/10 ,  B28B1/24 ,  B28B7/342 ,  B28B11/04 ,  B28B11/243 ,  B32B3/263 ,  B32B7/12 ,  B32B15/04 ,  B32B15/08 ,  B32B15/20 ,  B32B37/12 ,  B32B37/1284 ,  B32B37/14 ,  B32B2255/10 ,  B32B2307/202 ,  B32B2307/554 ,  B32B2603/00 ,  B33Y10/00 ,  B33Y80/00 ,  B62D35/00 ,  C04B35/76 ,  C04B35/806 ,  C09D5/26 ,  C23C14/20 ,  C23C16/06 ,  C23C18/1633 ,  C23C18/165 ,  C23C18/2013 ,  C23C18/22 ,  C23C18/31 ,  C23C26/00 ,  C23C28/02 ,  C25D3/02 ,  C25D3/38 ,  C25D3/46 ,  C25D5/48 ,  C25D9/04 ,  C25D11/20 ,  F01D5/00 ,  F01D5/147 ,  F01D5/187 ,  F01D5/284 ,  F01D5/288 ,  F01D9/02 ,  F01D9/041 ,  F01D11/08 ,  F01D25/005 ,  F04D29/023 ,  F04D29/324 ,  F04D29/542 ,  F05D2220/32 ,  F05D2230/10 ,  F05D2230/22 ,  F05D2230/30 ,  F05D2230/312 ,  F05D2230/314 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2300/10 ,  F05D2300/11 ,  F05D2300/121 ,  F05D2300/132 ,  F05D2300/133 ,  F05D2300/1616 ,  F05D2300/171 ,  F05D2300/177 ,  F05D2300/20 ,  F05D2300/30 ,  F05D2300/44 ,  F05D2300/501 ,  F05D2300/603 ,  F05D2300/611 ,  F05D2300/614 ,  F42B10/02

Abstract: A composite component and a plated polymer component are disclosed. The composite component may comprise a body portion formed from an organic matrix composite, a first metal coating applied to a surface of the body portion, and an outer metal layer on the first metal coating that is erosion-resistant. The plated polymer component may comprise a polymer substrate, a metal plating layer applied to a surface of the polymer substrate, and at least one selectively thickened region in the metal plating layer. The at least one selectively thickened region may assist in protecting the plated polymer component against wear and/or erosion.

Abstract translation: 公开了复合组分和镀覆聚合物组分。 复合部件可以包括由有机基质复合材料形成的主体部分，施加到主体部分的表面上的第一金属涂层以及耐腐蚀的第一金属涂层上的外部金属层。 镀覆的聚合物组分可以包括聚合物基材，施加到聚合物基材的表面的金属镀层，以及金属镀层中的至少一个选择性增稠区域。 所述至少一个选择性增稠的区域可有助于保护镀覆的聚合物组分免受磨损和/或侵蚀。

公开(公告)号：US20160326892A1

公开(公告)日：2016-11-10

申请号：US15108613

申请日：2015-01-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Grant O. Cook, III ,  Wendell V. Twelves

IPC: F01D5/28

CPC classification number: F01D5/288 ,  F01D5/147 ,  F01D5/282 ,  F01D5/284 ,  F04D19/00 ,  F05D2220/32 ,  F05D2240/30 ,  F05D2300/10 ,  F05D2300/20 ,  F05D2300/502 ,  F05D2300/611 ,  F05D2300/615 ,  Y02T50/672

Abstract: A component for a gas turbine engine comprises an underlying substrate. A plurality of ceramic panels have intermediate thermal expansion joints bonded by a bond layer to the underlying substrate. The thermal expansion joints are formed of a material having a greater coefficient of expansion than a material forming the ceramic panels. The ceramic panels and the thermal expansion joints are positioned to define an outer surface for the component. A gas turbine engine and a component for a gas turbine engine are also disclosed.

Abstract translation: 用于燃气涡轮发动机的部件包括下面的基板。 多个陶瓷板具有通过接合层与下面的基底结合的中间热膨胀接头。 热膨胀接头由比形成陶瓷板的材料膨胀系数大的材料形成。 陶瓷板和热膨胀接头被定位以限定用于部件的外表面。 还公开了一种燃气涡轮发动机和用于燃气涡轮发动机的部件。

公开(公告)号：US20160238248A1

公开(公告)日：2016-08-18

申请号：US15025012

申请日：2014-10-07

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Gary D. Roberge ,  Grant O. Cook, III

IPC: F23R3/00 ,  F02C7/18 ,  F23R3/06

CPC classification number: F23R3/002 ,  F02C7/18 ,  F23R3/005 ,  F23R3/007 ,  F23R3/06 ,  F23R2900/00017 ,  F23R2900/00018 ,  F23R2900/03042 ,  F23R2900/03044

Abstract: A combustor wall is provided for a turbine engine. The combustor wall includes a shell, a heat shield and a combustion chamber. The heat shield is connected to the shell by a bonded connection, and defines a portion of the combustion chamber. A cooling cavity is defined between the shell and the heat shield.

Abstract translation: 为涡轮发动机提供燃烧器壁。 燃烧器壁包括壳体，隔热罩和燃烧室。 隔热罩通过粘合连接连接到壳体，并且限定燃烧室的一部分。 在外壳和隔热罩之间限定一个冷却腔。

公开(公告)号：US20160169783A1

公开(公告)日：2016-06-16

申请号：US14903935

申请日：2014-07-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Glenn Levasseur ,  James T. Roach ,  Grant O. Cook, III ,  Raymond K. Kersey

IPC: G01N3/08

CPC classification number: G06K19/07749 ,  B29C37/0025 ,  B29C64/106 ,  B29C64/124 ,  B29C64/153 ,  B29C70/42 ,  B29C70/54 ,  B29K2079/08 ,  B29K2105/0058 ,  B29K2105/12 ,  B29K2105/251 ,  B29K2105/253 ,  B29K2307/04 ,  B29K2309/08 ,  B29L2009/008 ,  B29L2031/082 ,  B32B27/08 ,  B32B27/281 ,  B32B2250/02 ,  B32B2255/10 ,  B32B2255/205 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2603/00 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C23C18/1641 ,  C23C18/1653 ,  C23C18/1657 ,  C23C18/166 ,  C23C18/22 ,  C23C18/30 ,  C23C18/32 ,  C23C28/021 ,  C23C28/023 ,  C25D1/003 ,  C25D1/02 ,  C25D1/20 ,  C25D3/02 ,  C25D5/06 ,  C25D5/54 ,  C25D5/56 ,  C25D7/00 ,  C25D7/04 ,  C25D9/02 ,  C25D17/12 ,  G01B7/16 ,  G01D5/12 ,  G01N3/08 ,  G01N2203/026 ,  G01N2203/0268 ,  G01N2203/0298

Abstract: A plated polymer test specimen for measuring strain imparted to the plated polymer test specimen includes a polymeric substrate including a top, a bottom, a pair of opposing edges and a pair of opposing end edges, the top and bottom being plated with top and bottom metal layers respectively, the side edges and the end edges being at least substantially free of plating. The substrate includes two spaced-apart holes that extend through the top metal layer, substrate and the bottom metal layer. Alternatively, the substrate may comprise a composite layup structure. A method for testing the strain imparted to a plated polymer test specimen is also disclosed.

Abstract translation: 用于测量赋予镀覆聚合物测试样品的应变的镀覆聚合物测试样品包括聚合物基材，其包括顶部，底部，一对相对的边缘和一对相对的端部边缘，顶部和底部镀有顶部和底部金属 层边缘和端边缘至少基本上没有电镀。 衬底包括延伸穿过顶部金属层，衬底和底部金属层的两个间隔开的孔。 或者，衬底可以包括复合叠层结构。 还公开了一种用于测试赋予镀覆聚合物试样的应变的方法。

公开(公告)号：US20160083303A1

公开(公告)日：2016-03-24

申请号：US14786919

申请日：2014-04-22

Applicant: United Technologies Corporation

Inventor： Sergey Mironets ,  Grant O. Cook, III

IPC: C04B35/65 ,  C04B35/44 ,  C04B35/48 ,  C04B35/565

CPC classification number: C04B35/65 ,  B33Y10/00 ,  B33Y70/00 ,  C04B35/117 ,  C04B35/44 ,  C04B35/46 ,  C04B35/48 ,  C04B35/486 ,  C04B35/565 ,  C04B35/584 ,  C04B35/6303 ,  C04B35/6316 ,  C04B2235/3217 ,  C04B2235/3225 ,  C04B2235/3244 ,  C04B2235/3281 ,  C04B2235/3298 ,  C04B2235/3409 ,  C04B2235/3418 ,  C04B2235/386 ,  C04B2235/3865 ,  C04B2235/40 ,  C04B2235/402 ,  C04B2235/6026 ,  C04B2235/665 ,  C04B2235/764 ,  C04B2235/9653

Abstract: A ceramic turbine component is formed by a process including mixing a ceramic powder with an inorganic binder powder. The powder mixture is then formed into a turbine component that is subsequently densified by transient liquid phase sintering. In an embodiment, the turbine component may be formed by an additive manufacturing process such as selective laser sintering.

Abstract translation: 通过包括将陶瓷粉末与无机粘合剂粉末混合的方法形成陶瓷涡轮机部件。 然后将粉末混合物形成涡轮机部件，随后通过瞬态液相烧结致密化。 在一个实施例中，涡轮机部件可以通过诸如选择性激光烧结的添加剂制造工艺来形成。

公开(公告)号：US20160010658A1

公开(公告)日：2016-01-14

申请号：US14866194

申请日：2015-09-25

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James T. Roach ,  Grant O. Cook, III

IPC: F04D29/38 ,  B23P15/04 ,  F04D29/34

CPC classification number: F04D29/388 ,  B23P15/04 ,  F01D5/147 ,  F01D5/282 ,  F01D5/30 ,  F04D29/322 ,  F04D29/324 ,  F04D29/34 ,  F05D2220/36 ,  F05D2230/232 ,  F05D2240/303

Abstract: The present disclosure relates to composite airfoils bonded to a metallic root. A composite body (510) may be formed with a metallic co-molded detail (520). The co-molded detail (520) may be transient liquid phase (TLP) bonded to an attachment feature (530). The attachment feature (530) may allow the composite body (510) to be attached to a rotor (200). The airfoil (500) may also have a metallic edge (550) which is TLP bonded to the composite body (510) via a co-molded edge (540).

Abstract translation: 本公开涉及结合到金属根的复合翼型件。 复合体（510）可以形成有金属共模塑细节（520）。 共模塑细节（520）可以是结合到附着特征（530）的瞬态液相（TLP）。 附接特征（530）可以允许复合体（510）附接到转子（200）。 翼型件（500）也可以具有金属边缘（550），其通过共模制边缘（540）与TLP结合到复合体（510）上。

公开(公告)号：US20140202170A1

公开(公告)日：2014-07-24

申请号：US13682048

申请日：2012-11-20

Applicant: United Technologies Corporation

Inventor： Grant O. Cook, III

IPC: F02C7/04

CPC classification number: F02C7/04 ,  B32B15/08 ,  B32B27/281 ,  B32B27/288 ,  B32B2255/06 ,  B32B2255/26 ,  B32B2307/306 ,  B32B2307/54 ,  B32B2307/558 ,  B32B2307/714 ,  C23C18/1605 ,  C23C18/1616 ,  C23C18/165 ,  C25D1/02 ,  C25D5/022 ,  C25D5/56 ,  C25D7/04 ,  F02C7/14 ,  F05D2230/90 ,  F16L9/12 ,  Y10T428/24967 ,  Y10T428/26

Abstract: An article has a polymeric substrate and a coating system. The coating system includes a metallic plating and a polymeric coating atop the metallic plating. The metallic plating has a thickness of at least 0.05 mm.

Abstract translation: 制品具有聚合物基材和涂料体系。 涂层系统包括金属镀层和金属镀层顶部的聚合物涂层。 金属镀层的厚度至少为0.05mm。

公开(公告)号：US11267576B2

公开(公告)日：2022-03-08

申请号：US14903987

申请日：2014-07-09

Applicant: United Technologies Corporation

Inventor： James T. Roach ,  Colin J. Kling ,  Grant O. Cook, III ,  James J. McPhail ,  Shari L. Bugaj ,  James F. O'Brien ,  Majidullah Dehlavi ,  Scott A. Smith ,  Matthew R. Rader ,  Matthew A. Turner ,  JinQuan Xu

IPC: B64D29/00 ,  B29D22/00 ,  F02K3/04 ,  F01D5/02 ,  F01D25/28

Abstract: Plated polymeric gas turbine engine parts and methods for fabricating lightweight plated polymeric gas turbine engine parts are disclosed. The parts include a polymeric substrate plated with one or more metal layers. The polymeric material of the polymeric substrate may be structurally reinforced with materials that may include carbon, metal, or glass. The polymeric substrate may also include a plurality of layers to form a composite layup structure.

公开(公告)号：US10933489B2

公开(公告)日：2021-03-02

申请号：US14903844

申请日：2014-07-09

Applicant: United Technologies Corporation

Inventor： Grant O. Cook, III

IPC: B23K35/00 ,  B23K20/16 ,  B23K20/02 ,  B23K35/36 ,  B32B15/01 ,  B23K20/233 ,  B23K103/16 ,  B23K101/00 ,  B23K103/00 ,  B23K101/34 ,  B23K103/18

Abstract: A method for bonding components is disclosed. The method may comprise positioning an interlayer between a metallic component and a metal-plated non-metallic component at a bond region, heating the bond region to a bonding temperature to produce a liquid at the bond region, and maintaining the bond region at the bonding temperature until the liquid has solidified to form a bond between the metallic component and the metal-plated non-metallic component at the bond region. A method for providing a part having a customized coating is also disclosed. The method may comprise applying a metallic coating on a surface of a metallic substrate, and bonding the metallic coating to the metallic substrate by a transient liquid phase bonding process to provide the part having the customized coating.