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公开(公告)号：US10119423B2
公开(公告)日：2018-11-06
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
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.
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公开(公告)号：US20160159488A1
公开(公告)日：2016-06-09
申请号：US14903987
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： James T. Roach , Colin J. Kling , Grant O. Cook , James J. McPhail , Shari L. Bugaj , James F. O'Brien , Majidullah Dehlavi , Scott A. Smith , Matthew R. Rader , Matthew A. Turner , JinQuan Xu
CPC classification number: B64D29/00 , B29D22/00 , F01D5/02 , F01D25/28 , F02K3/04 , F05D2220/32 , F05D2230/30 , F05D2230/90 , F05D2300/10 , F05D2300/43 , F05D2300/603 , Y02T50/672
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.
Abstract translation: 公开了用于制造轻质电镀聚合物燃气涡轮发动机部件的电镀聚合物燃气涡轮发动机部件和方法。 这些部件包括镀有一个或多个金属层的聚合物基材。 聚合物基材的聚合材料可以用可以包括碳，金属或玻璃的材料在结构上加强。 聚合物基底还可以包括多个层以形成复合铺层结构。
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公开(公告)号：US20160152320A1
公开(公告)日：2016-06-02
申请号：US14930760
申请日：2015-11-03
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Shari L. Bugaj , James T. Roach
CPC classification number: B64C11/14 , B29C70/14 , B29C70/46 , B29K2101/10 , B29K2105/128 , B29K2307/04 , B29L2031/7504 , B29L2031/7724 , F02C7/04 , F05D2300/603 , Y02T50/672
Abstract: A spinner for a gas turbine engine is disclosed. The spinner may include a body extending between a first and second end comprised of a cured chopped unidirectional fiber pre-impregnated material. The body may have a generally conical shape and may further be plated with a metal or metal alloy.
Abstract translation: 公开了一种用于燃气涡轮发动机的旋转器。 旋转器可以包括在由固化的切断的单向纤维预浸渍材料组成的第一和第二端之间延伸的主体。 主体可以具有大致圆锥形的形状，并且还可以镀金属或金属合金。
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公开(公告)号：US09279531B2
公开(公告)日：2016-03-08
申请号：US13716487
申请日：2012-12-17
Applicant: United Technologies Corporation
Inventor： Michael J. Parkin , Colin J. Kling
IPC: F16L9/00 , F16L55/00 , F16L23/032 , F16L43/00
CPC classification number: F16L55/00 , F01D9/02 , F01D25/005 , F02C7/14 , F05D2300/224 , F05D2300/606 , F05D2300/614 , F16L23/032 , F16L43/008 , F16L47/145 , Y10T29/49286 , Y10T29/49826
Abstract: A duct has: a first non-metallic member extending between a first end and a second end, at least at the first end having an outwardly-projecting flange portion; a metallic flange member having a sleeve extending between a first end and a second end and a flange extending outward from the sleeve and having a first face and a second face; and a second non-metallic member extending between a first end and a second end having an outwardly-projecting flange portion, the first non-metallic member flange portion mounted to the flange first face and the second non-metallic member flange portion mounted to the flange second face.
Abstract translation: 管道具有：在第一端和第二端之间延伸的第一非金属构件，至少在第一端具有向外突出的凸缘部分; 金属凸缘构件，其具有在第一端和第二端之间延伸的套筒和从套筒向外延伸并具有第一面和第二面的凸缘; 以及第二非金属构件，其在具有向外突出的凸缘部分的第一端和第二端之间延伸，所述第一非金属构件凸缘部分安装到所述凸缘第一面，所述第二非金属构件凸缘部分安装到 法兰第二面。
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公开(公告)号：US20140166144A1
公开(公告)日：2014-06-19
申请号：US13716487
申请日：2012-12-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Michael J. Parkin , Colin J. Kling
CPC classification number: F16L55/00 , F01D9/02 , F01D25/005 , F02C7/14 , F05D2300/224 , F05D2300/606 , F05D2300/614 , F16L23/032 , F16L43/008 , F16L47/145 , Y10T29/49286 , Y10T29/49826
Abstract: A duct has: a first non-metallic member extending between a first end and a second end, at least at the first end having an outwardly-projecting flange portion; a metallic flange member having a sleeve extending between a first end and a second end and a flange extending outward from the sleeve and having a first face and a second face; and a second non-metallic member extending between a first end and a second end having an outwardly-projecting flange portion, the first non-metallic member flange portion mounted to the flange first face and the second non-metallic member flange portion mounted to the flange second face.
Abstract translation: 管道具有：在第一端和第二端之间延伸的第一非金属构件，至少在第一端具有向外突出的凸缘部分; 金属法兰构件，其具有在第一端和第二端之间延伸的套筒和从套筒向外延伸并具有第一面和第二面的凸缘; 以及第二非金属构件，其在具有向外突出的凸缘部的第一端和第二端之间延伸，所述第一非金属构件凸缘部安装到所述凸缘第一面，并且所述第二非金属构件凸缘部安装到 法兰第二面。
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Patent Agency Ranking
公开(公告)号：US11236765B2
公开(公告)日：2022-02-01
申请号：US16663479
申请日：2019-10-25
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Darin S. Lussier , James F. O'Brien
IPC: F01D21/04 , F04D29/52 , F04D29/66 , F04D29/02 , B29C70/88 , F01D5/28 , B29C70/02 , B29C70/72 , F01D25/24 , B29C70/86
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.
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公开(公告)号：US20200056626A1
公开(公告)日：2020-02-20
申请号：US16663479
申请日：2019-10-25
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Darin S. Lussier , James F. O'Brien
IPC: F04D29/52 , F04D29/02 , F04D29/66 , B29C70/86 , F01D25/24 , F01D21/04 , B29C70/72 , B29C70/02 , F01D5/28 , B29C70/88
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.
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公开(公告)号：US10458433B2
公开(公告)日：2019-10-29
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
IPC: F04D29/52 , F04D29/66 , F04D29/02 , B29C70/72 , B29C70/02 , F01D21/04 , F01D5/28 , F01D25/24 , B29C70/86 , B29C70/88
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.
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公开(公告)号：US20190323520A1
公开(公告)日：2019-10-24
申请号：US15957432
申请日：2018-04-19
Applicant: United Technologies Corporation
Inventor： David R. Lyders , Colin J. Kling
Abstract: A gas turbine engine fan case may comprise a plurality of wound layers that form a laminate and have a nominal radial fan case thickness, where the laminate includes a plurality of discrete fan case radial locations comprising a plurality of radially stacked composite plies that form a radial integral build up in comparison to the nominal radial fan case thickness.
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公开(公告)号：US20190162119A1
公开(公告)日：2019-05-30
申请号：US15823229
申请日：2017-11-27
Applicant: United Technologies Corporation
Inventor： Colin J. Kling , Darin S. Lussier , David R. Lyders
Abstract: A reinforced component in accordance with various embodiments includes a metal lug configured to be attached to a secondary component. The reinforced component further includes a composite material integrally formed around the metal lug and configured to be retained in place relative to the secondary component via an attachment between the metal lug and the secondary component.
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