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公开(公告)号：US20140140832A1
公开(公告)日：2014-05-22
申请号：US13652962
申请日：2012-10-16
Applicant: GENERAL ELECTRIC COMPANY
Inventor： William Howard Hasting , Courtney James Tudor
IPC: F01D25/24
CPC classification number: F01D25/246 , F01D9/04 , F01D9/042 , F05D2240/12 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: A quick engine change assembly, comprises a first circular frame member, a plurality of doublet supports spaced about the first circular frame member, the doublet supports being contoured along the axial direction, a flow surface defined between the plurality of doublet supports and, a plurality of cradles, each of the cradles including the doublet supports, the doublet supports from a lower portion of the cradle to the flow surface.
Abstract translation: 一种快速发动机更换组件，包括第一圆形框架构件，围绕第一圆形框架构件间隔开的多个双重支撑件，沿着轴向方向成轮廓的双重支撑件，限定在所述多个双重支撑件之间的流动表面，以及多个 的支架，每个支架包括双重支撑件，双头支撑件从支架的下部到流动表面。
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公开(公告)号：US09303520B2
公开(公告)日：2016-04-05
申请号：US13652955
申请日：2012-10-16
Applicant: General Electric Company
Inventor： William Howard Hasting , Courtney James Tudor
CPC classification number: F01D9/02 , F01D9/042 , F01D25/246 , F05D2240/12 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: The assembly has a first guide vane having a first end, a second end opposed to the first end, and a second guide vane having a first end, a second end opposed to its first end. A first end structure spans between the first guide vane first end and the second guide vane first end. A second end structure spans between the first guide vane second end and the second guide vane second end. The first guide vane, the second guide vane, the first end structure, and the second end structure are integrally formed together to form a double vane with a continuous outer surface, and a continuous inner surface.
Abstract translation: 组件具有第一导叶，其具有第一端，与第一端相对的第二端和具有第一端的第二导叶，与第一端相对的第二端。 第一端结构跨越第一导叶第一端和第二导叶第一端。 第二端部结构跨越第一导叶第二端和第二导叶第二端。 第一导向叶片，第二导向叶片，第一端部结构和第二端部结构一体地形成在一起，形成具有连续外表面的双叶片和连续的内表面。
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Patent Agency Ranking
公开(公告)号：US20130149127A1
公开(公告)日：2013-06-13
申请号：US13652970
申请日：2012-10-16
Applicant: General Electric Company
Inventor： William Howard Hasting , Courtney James Tudor
CPC classification number: F01D9/042 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: A structural platform comprises a first end, a second end, a first side wall and a second side wall, a platform body extending between the first end and the second end and further between the first side wall and the second side wall, a first fillet joining the first side wall and the platform body, a second fillet joining the second side wall and the platform body, the sidewalls being curved.
Abstract translation: 结构平台包括第一端，第二端，第一侧壁和第二侧壁，在第一端和第二端之间以及在第一侧壁和第二侧壁之间延伸的平台体，第一圆角 连接第一侧壁和平台体，连接第二侧壁和平台体的第二圆角，所述侧壁是弯曲的。
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公开(公告)号：US20170101878A1
公开(公告)日：2017-04-13
申请号：US15213504
申请日：2016-07-19
Applicant: General Electric Company
Inventor： Mingchao Wang , Gerald Alexander Pauley , Courtney James Tudor , Elzbieta Kryj-Kos , Weizeng Kong
CPC classification number: F01D9/041 , F01D5/3007 , F01D11/008 , F01D25/005 , F05D2220/32 , F05D2230/30 , F05D2230/40 , F05D2230/50 , F05D2240/12 , F05D2240/30 , F05D2240/80 , F05D2300/43 , F05D2300/44 , F05D2300/501 , F05D2300/522 , F05D2300/601 , F05D2300/603 , F05D2300/612 , Y02T50/672 , Y02T50/673
Abstract: A gas turbine engine including a component having a first and a second component that are attached or integrally formed with each other. The first and the second component define an enclosed void. An insert is positioned within the enclosed void which is formed of a material having a relatively low Young's modulus. The insert may prevent resin from filling the enclosed void during assembly/manufacture of the component, while also reducing a weight of the component and an amount of stress on the component. The component may be a fan platform positioned between a plurality of fan blades, an outlet guide vane, or another component of the gas turbine engine.
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公开(公告)号：US09303531B2
公开(公告)日：2016-04-05
申请号：US13652962
申请日：2012-10-16
Applicant: General Electric Company
Inventor： William Howard Hasting , Courtney James Tudor
CPC classification number: F01D25/246 , F01D9/04 , F01D9/042 , F05D2240/12 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: A quick engine change assembly, comprises a first circular frame member, a plurality of doublet supports spaced about the first circular frame member, the doublet supports being contoured along the axial direction, a flow surface defined between the plurality of doublet supports and, a plurality of cradles, each of the cradles including the doublet supports, the doublet supports from a lower portion of the cradle to the flow surface.
Abstract translation: 一种快速发动机更换组件，包括第一圆形框架构件，围绕第一圆形框架构件间隔开的多个双重支撑件，沿着轴向方向成轮廓的双重支撑件，限定在所述多个双重支撑件之间的流动表面，以及多个 的支架，每个支架包括双重支撑件，双头支撑件从支架的下部到流动表面。
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公开(公告)号：US20140133975A1
公开(公告)日：2014-05-15
申请号：US13652955
申请日：2012-10-16
Applicant: GENERAL ELECTRIC COMPANY
Inventor： William Howard Hasting , Courtney James Tudor
IPC: F01D9/02
CPC classification number: F01D9/02 , F01D9/042 , F01D25/246 , F05D2240/12 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: The assembly has a first guide vane having a first end, a second end opposed to the first end, and a second guide vane having a first end, a second end opposed to its first end. A first end structure spans between the first guide vane first end and the second guide vane first end. A second end structure spans between the first guide vane second end and the second guide vane second end. The first guide vane, the second guide vane, the first end structure, and the second end structure are integrally formed together to form a double vane with a continuous outer surface, and a continuous inner surface.
Abstract translation: 组件具有第一导叶，其具有第一端，与第一端相对的第二端和具有第一端的第二导叶，与第一端相对的第二端。 第一端结构跨越第一导叶第一端和第二导叶第一端。 第二端部结构跨越第一导叶第二端和第二导叶第二端。 第一导向叶片，第二导向叶片，第一端部结构和第二端部结构一体地形成在一起，形成具有连续外表面的双叶片和连续的内表面。
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公开(公告)号：US20130149130A1
公开(公告)日：2013-06-13
申请号：US13652949
申请日：2012-10-16
Applicant: General Electric Company
Inventor： William Howard Hasting , Courtney James Tudor
IPC: F01D25/00
CPC classification number: F01D9/042 , F05D2300/6033 , Y02T50/672 , Y02T50/673
Abstract: A fan hub frame comprises a circular hub having an opening extending axially wherein an engine core is capable of being positioned, the circular hub having a radially outer surface, the radial outer surface having a plurality of cradles, each of the cradles having a lower surface and fillets disposed between the lower surface and upwardly extending sidewalls, the cradles capable of receiving a double outlet guide vane.
Abstract translation: 风扇轮毂框架包括圆形毂，其具有轴向延伸的开口，其中发动机芯能够定位，所述圆形轮毂具有径向外表面，所述径向外表面具有多个托架，每个所述托架具有下表面 以及设置在下表面和向上延伸的侧壁之间的圆角，该支架能够容纳双出口导向叶片。
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