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公开(公告)号：US20160201607A1
公开(公告)日：2016-07-14
申请号：US14695373
申请日：2015-04-24
Applicant: United Technologies Corporation
Inventor： Edward J. Gallagher , Byron R. Monzon , Shari L. Bugaj
CPC classification number: F02C7/36 , F01D5/147 , F01D5/282 , F01D15/12 , F02K1/06 , F02K3/06 , F04D29/023 , F04D29/053 , F04D29/325 , F04D29/388 , F04D29/526 , F04D29/563 , F05D2220/32 , F05D2220/327 , F05D2220/36 , F05D2260/4031 , F05D2300/603 , Y02T50/672
Abstract: A gas turbine engine includes a core flow passage, a bypass flow passage, and a propulsor arranged at an inlet of the bypass flow passage and the core flow passage. The propulsor includes a row of propulsor blades. The row includes no more than 20 of the propulsor blades. The propulsor has a pressure ratio between about 1.2 and about 1.7 across the propulsor blades.
Abstract translation: 燃气涡轮发动机包括芯流路，旁通流路和布置在旁通流路和芯流路的入口的推进器。 推进器包括一排推进刀片。 该行包括不超过20个推进刀片。 推进器在推进刀片上的压力比介于约1.2和约1.7之间。
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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：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
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.
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公开(公告)号：US09663867B2
公开(公告)日：2017-05-30
申请号：US14331771
申请日：2014-07-15
Applicant: United Technologies Corporation
Inventor： Shari L. Bugaj , Wendell V. Twelves, Jr. , Grant O. Cook, III
CPC classification number: C25D5/48 , C23C18/1605 , C23C18/1608 , C23C18/1653 , C23C18/30 , C25D5/02 , C25D5/022 , C25D5/10 , C25D7/00 , G01D5/2086
Abstract: A component comprises a non-metallic core having an outer surface, a first catalyst deposited onto at least a first portion of the outer surface of the non-metallic core, a second catalyst deposited onto at least a second portion of the outer surface of the non-metallic core, an electrical interface, and a metallic coating. The electrical interface is plated onto the first catalyst, and includes a first interface layer electroless plated onto the first catalyst. The metallic coating is plated onto the second catalyst.
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公开(公告)号：US20160369703A1
公开(公告)日：2016-12-22
申请号：US15233142
申请日：2016-08-10
Applicant: United Technologies Corporation
Inventor： Edward J. Gallagher , Byron R. Monzon , Shari L. Bugaj
IPC: F02C7/36 , F04D29/02 , F04D29/053 , F02K3/06 , F04D29/38 , F04D29/56 , F04D29/52 , F01D15/12 , F04D29/32
CPC classification number: F02C7/36 , F01D5/147 , F01D5/282 , F01D15/12 , F02K1/06 , F02K3/06 , F04D29/023 , F04D29/053 , F04D29/325 , F04D29/388 , F04D29/526 , F04D29/563 , F05D2220/32 , F05D2220/327 , F05D2220/36 , F05D2260/4031 , F05D2300/603 , Y02T50/672
Abstract: A gas turbine engine includes a gear assembly and a bypass flow passage that includes an inlet and an outlet that define a design pressure ratio between 1.3 and 1.55. A fan is arranged at the inlet. A first turbine is coupled with a first shaft such that rotation of the first turbine will drive the fan, through the first shaft and the gear assembly, at a lower speed than the first shaft. The fan includes a row of fan blades. The row includes 12-16 (N) fan blades, a solidity value (R) that is from 1.0 to 1.3, and a ratio of N/R that is from 10.0 to 16.
Abstract translation: 燃气涡轮发动机包括齿轮组件和旁通流动通道，其包括限定1.3至1.55之间的设计压力比的入口和出口。 入口处设有风扇。 第一涡轮与第一轴联接，使得第一涡轮的旋转将以比第一轴更低的速度通过第一轴和齿轮组件驱动风扇。 风扇包括一排风扇叶片。 该行包括12-16（N）个风扇叶片，固体值（R）为1.0至1.3，N / R的比例为10.0至16。
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Patent Agency Ranking
公开(公告)号：US20150315922A1
公开(公告)日：2015-11-05
申请号：US14592942
申请日：2015-01-09
Applicant: United Technologies Corporation
Inventor： James T. Roach , Grant O. Cook, III , Colin J. Kling , James F. O'Brien , Shari L. Bugaj
CPC classification number: F01D9/02 , B64C11/14 , F01D5/02 , F01D5/12 , F02C7/04 , F05D2220/32 , F05D2300/10 , F05D2300/603 , F05D2300/6034 , Y02T50/672
Abstract: A spinner for a gas turbine engine comprises an outer shell for defining an airflow path when mounted in a gas turbine engine. An inner surface is provided with a plurality of webs. A gas turbine engine and a fan section for a gas turbine engine are also disclosed.
Abstract translation: 用于燃气涡轮发动机的旋转器包括用于在安装在燃气涡轮发动机中时限定气流路径的外壳。 内表面设置有多个腹板。 还公开了一种燃气涡轮发动机和用于燃气涡轮发动机的风扇部分。
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公开(公告)号：US20180328372A1
公开(公告)日：2018-11-15
申请号：US15709567
申请日：2017-09-20
Applicant: United Technologies Corporation
Inventor： Edward J. Gallagher , Byron R. Monzon , Shari L. Bugaj
CPC classification number: F04D29/023 , F01D5/147 , F01D5/282 , F01D15/12 , F02C3/06 , F02C7/36 , F02K1/06 , F02K3/06 , F04D29/053 , F04D29/325 , F04D29/388 , F04D29/526 , F04D29/563 , F05D2220/32 , F05D2220/323 , F05D2220/327 , F05D2220/36 , F05D2260/4031 , F05D2300/603 , Y02T50/672
Abstract: A gas turbine engine includes a gear assembly and a bypass flow passage that has an inlet. A fan is arranged within the bypass flow passage. A first turbine is coupled with a first shaft, which is coupled with the fan. A second turbine is coupled with a second shaft. The fan includes a hub and a row of fan blades that extend from the hub. The row includes 12 to 14 (N) of the fan blades, a solidity value (R) at tips of the fan blades that is greater than 0.85 and less than 1.1, and a ratio of N/R that is from 9 to 20.
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公开(公告)号：US09909505B2
公开(公告)日：2018-03-06
申请号：US14695373
申请日：2015-04-24
Applicant: United Technologies Corporation
Inventor： Edward J. Gallagher , Byron R. Monzon , Shari L. Bugaj
IPC: F02C7/36 , F02K1/06 , F02K3/06 , F01D5/28 , F01D5/14 , F01D15/12 , F04D29/02 , F04D29/053 , F04D29/32 , F04D29/38 , F04D29/52 , F04D29/56
CPC classification number: F02C7/36 , F01D5/147 , F01D5/282 , F01D15/12 , F02K1/06 , F02K3/06 , F04D29/023 , F04D29/053 , F04D29/325 , F04D29/388 , F04D29/526 , F04D29/563 , F05D2220/32 , F05D2220/327 , F05D2220/36 , F05D2260/4031 , F05D2300/603 , Y02T50/672
Abstract: A gas turbine engine includes a core flow passage, a bypass flow passage, and a propulsor arranged at an inlet of the bypass flow passage and the core flow passage. The propulsor includes a row of propulsor blades. The row includes no more than 20 of the propulsor blades. The propulsor has a pressure ratio between about 1.2 and about 1.7 across the propulsor blades.
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公开(公告)号：US20170030205A1
公开(公告)日：2017-02-02
申请号：US15039880
申请日：2014-11-07
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Charles W. Brown , Andrew G. Alarcon , Shari L. Bugaj , Charles R. Watson
Abstract: In a featured embodiment, a fan rotor comprises a platform. Clevises extend radially inwardly of the platform. Each clevis has an aperture. A hub has hub lugs positioned intermediate spaced ends of the clevises, and apertures. A pin extends through the apertures in the hub and the clevises to connect the platform to the hub. The apertures in the clevises are formed to have an inner surface for supporting the pin. A method of forming a fan blade platform is also disclosed.
Abstract translation: 在特征实施例中，风扇转子包括平台。 夹具在平台的径向内侧延伸。 每个U形夹具有一个孔。 轮毂具有定位在U形夹的中间间隔的端部处的毂凸耳和孔。 销延伸穿过轮毂中的孔和套筒将平台连接到轮毂。 夹头中的孔形成为具有用于支撑销的内表面。 还公开了一种形成风扇叶片平台的方法。
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公开(公告)号：US20160169012A1
公开(公告)日：2016-06-16
申请号：US14904007
申请日：2014-07-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Nelson DaCunha , Barry Barnett , Gary M. Lomasney , Joseph Parkos , James T. Roach , Glenn Levasseur , Charles R. Watson , Jinquan Xu , Grant O. Cook , Raymond K. Kersey , Wendell V. Twelves , Shari L. Bugaj
CPC classification number: F01D5/3092 , C23C18/1641 , C23C18/1651 , C23C18/1657 , C23C18/31 , C25D1/00 , C25D5/022 , C25D5/10 , C25D7/00 , C25D7/04 , C25D7/0607 , F02C7/04 , F02K1/54 , F05D2230/90 , F05D2260/96 , F05D2300/43 , Y02T50/672 , Y02T50/673
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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