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公开(公告)号：US10208667B2
公开(公告)日：2019-02-19
申请号：US15026692
申请日：2014-05-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Colin J. Kling , Steven Clarkson
Abstract: A nose cone may have a spinner including a main portion and an axially extending stepped portion. The nose cone may also have an annular aft support ring radially secured to the axially extending stepped portion. The nose cone may further include a fairing, which may be secured to the stepped portion.
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公开(公告)号：US10094282B2
公开(公告)日：2018-10-09
申请号：US14693488
申请日：2015-04-22
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Colin J. Kling , Darin S. Lussier
Abstract: A spinner for a fan assembly of a gas turbine engine, a method of fabricating a spinner for a fan assembly of a gas turbine engine, and a gas turbine engine are disclosed. The fan section may include a nosecap. The spinner may include a forward end, an aft end, and a return flange associated with the forward end. The return flange may include a forward flange extending forward towards the nosecap and an aft flange extending aft towards the aft end.
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公开(公告)号：US20170349265A1
公开(公告)日：2017-12-07
申请号：US15171926
申请日：2016-06-02
Applicant: United Technologies Corporation
Inventor： James J. McPhail , Colin J. Kling
CPC classification number: B64C11/14 , F02C7/04 , F02K3/06 , F05D2220/32 , F05D2250/71 , F05D2300/603
Abstract: A spinner for a gas turbine engine may include a substantially-flat inner surface having frustoconical geometry. A flange having semi-torroidal geometry may extend from the spinner with an inner curved surface of the flange being tangential to the inner surface. A mating portion may extend substantially tangentially from the inner curved surface of the flange and configured for fastening to a fan hub.
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Patent Agency Ranking
公开(公告)号：US20160369812A1
公开(公告)日：2016-12-22
申请号：US15185573
申请日：2016-06-17
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Darin S. Lussier , James F. O'Brien
CPC classification number: F04D29/526 , B29C70/86 , B29C70/885 , F01D21/045 , F04D29/023 , F04D29/664 , F05D2300/224 , F05D2300/433 , F05D2300/603 , Y02T50/672
Abstract: A method of fabricating a fan case for a gas turbine engine defines a metallic ring including an outer surface and an inner surface. A first composite material is assembled about the outer surface of the metallic ring. A second composite material is assembled about the first composite material. The first composite material and the second material are cured about the metallic ring within a tool to form a first subassembly. The first subassembly is removed from the tool. A fan case assembly for a gas turbine engine and a gas turbine engine are also disclosed.
Abstract translation: 制造用于燃气涡轮发动机的风扇壳体的方法限定了包括外表面和内表面的金属环。 围绕金属环的外表面组装第一复合材料。 围绕第一复合材料组装第二复合材料。 第一复合材料和第二材料围绕工具中的金属环固化以形成第一子组件。 第一个子组件从工具中移除。 还公开了一种用于燃气涡轮发动机和燃气涡轮发动机的风扇壳体组件。
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公开(公告)号：US20160281737A1
公开(公告)日：2016-09-29
申请号：US14850438
申请日：2015-09-10
Applicant: United Technologies Corporation
Inventor： Matthew A. Turner , Colin J. Kling , David A. Topol
CPC classification number: F04D29/526 , F01D5/02 , F01D21/045 , F02C3/04 , F02C7/045 , F04D29/321 , F04D29/325 , F05D2220/32 , F05D2220/36 , F05D2230/23 , F05D2230/30 , F05D2240/35 , F05D2300/17 , F05D2300/43 , Y02T50/671
Abstract: A gas turbine engine impact liner is disclosed. The impact liner may include a base sheet, a plurality of stanchions extending from the base sheet, and a plurality of supports, each being operatively associated with one of the plurality of stanchions.
Abstract translation: 公开了一种燃气涡轮发动机冲击衬垫。 冲击衬垫可以包括基片，从基片延伸的多个支柱，以及多个支撑件，每个支撑件与多个支柱中的一个可操作地相关联。
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公开(公告)号：US20160237897A1
公开(公告)日：2016-08-18
申请号：US15026692
申请日：2014-05-23
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Colin J. Kling , Steven Clarkson
CPC classification number: F02C7/04 , B64C11/14 , F01D5/066 , F02C3/04 , F05D2220/32 , F05D2260/31 , F05D2260/37
Abstract: A nose cone may have a spinner including a main portion and an axially extending stepped portion. The nose cone may also have an annular aft support ring radially secured to the axially extending stepped portion. The nose cone may further include a fairing, which may be secured to the stepped portion.
Abstract translation: 鼻锥可以具有包括主要部分和轴向延伸的阶梯部分的旋转器。 鼻锥体还可以具有径向固定到轴向延伸的阶梯部分的环形后支撑环。 鼻锥可以进一步包括可以固定到阶梯部分的整流罩。
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公开(公告)号：US20160168716A1
公开(公告)日：2016-06-16
申请号：US14903942
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Colin J. Kling , James T. Roach , Shari L. Bugaj
IPC: C23C18/16 , C25D5/54 , C25D7/00 , C23C28/02 , B29C37/00 , C23C18/22 , C23C18/30 , B29C70/42 , B29C70/54 , B32B27/08 , C23C18/32
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: Plated polymeric articles having a composite layup structure and method of making the same are disclosed. A plated polymeric article comprises a composite layup having first and second polymer layers. The plated polymeric article further comprises a first metal plated onto the polymer. Additionally, methods for fabricating a plated polymeric article are disclosed. A composite layup is provided and compression molded into a desired shape having an outer surface. The outer surface of the article is prepared to receive a catalyst and then is activated with the catalyst. A first metallic layer is then plated onto the outer surface.
Abstract translation: 公开了具有复合叠层结构的电镀聚合物及其制备方法。 镀覆的聚合物制品包括具有第一和第二聚合物层的复合叠层。 镀覆的聚合物制品还包括镀在聚合物上的第一金属。 另外，公开了制造镀覆聚合物的方法。 提供复合叠层并压缩成具有外表面的所需形状。 制品的外表面准备接收催化剂，然后用催化剂活化。 然后将第一金属层电镀到外表面上。
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公开(公告)号：US20150218966A1
公开(公告)日：2015-08-06
申请号：US14426252
申请日：2013-09-17
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Charles W. Brown , Christopher M. Quinn , Shelton O. Duelm , Peter V. Tomeo , Corey L. Hubbert
CPC classification number: F01D25/28 , F01D11/008 , F01D25/24 , F02C3/10 , Y02T50/671 , Y10T29/4932
Abstract: A fan hub assembly for a gas turbine engine includes a fan hub that is configured to rotate about an axis. The fan hub has an axially extending aperture and a platform. A fastener is received in the aperture in a slip fit relationship to secure the platform to the fan hub.
Abstract translation: 一种用于燃气涡轮发动机的风扇轮毂组件，其包括被配置为围绕轴线旋转的风扇轮毂。 风扇毂具有轴向延伸的孔和平台。 紧固件以滑动配合关系容纳在孔中，以将平台固定到风扇毂。
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