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公开(公告)号：US20140290268A1
公开(公告)日：2014-10-02
申请号：US14306402
申请日：2014-06-17
Applicant: United Technologies Corporation
Inventor： James B. Coffin , Alessio Pescosolido
IPC: F02C7/20
CPC classification number: F02C7/20 , B64D27/26 , B64D2027/266 , F01D21/045 , F01D25/16 , F02C7/36 , F05D2220/36 , F05D2260/40311 , Y10T29/49318
Abstract: A gas turbine engine includes a fan, an engine static structure, a geared architecture to drive the fan and supported relative to the static structure, a fan drive turbine to drive the geared architecture, a first member secured to the geared architecture, and a second member secured to the engine static structure and configured to cooperate with the first member to limit movement of the geared architecture relative to the static structure. A fan drive gear system and method are also disclosed.
Abstract translation: 燃气涡轮发动机包括风扇，发动机静态结构，用于驱动风扇并相对于静态结构支撑的齿轮架构，驱动齿轮架构的风扇驱动涡轮机，固定到齿轮架构的第一构件，以及第二 固定到发动机静态结构并被构造成与第一构件协作以限制齿轮架构相对于静态结构的运动的构件。 还公开了一种风扇驱动齿轮系统和方法。
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公开(公告)号：US08827633B2
公开(公告)日：2014-09-09
申请号：US14036927
申请日：2013-09-25
Applicant: United Technologies Corporation
Inventor： James B. Coffin , John R. Otto
CPC classification number: F01D15/12 , F01D25/04 , F02C7/36 , F02K3/06 , F05D2260/40311 , F05D2260/96 , Y10T74/19642
Abstract: A gas turbine engine includes a fan section. A turbine section is coupled to the fan section via a geared architecture. The geared architecture includes a torque frame and a flex support spaced apart from one another at a location. A gear train is supported by the torque frame. A viscous damper is provided between the torque frame and the flex support at the location.
Abstract translation: 燃气涡轮发动机包括风扇部分。 涡轮机部分通过齿轮架构耦合到风扇部分。 齿轮架构包括在一个位置处彼此间隔开的扭矩框架和柔性支撑件。 齿轮系由转矩架支撑。 在位置处的扭矩框架和柔性支撑件之间设置粘性阻尼器。
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公开(公告)号：US10436116B2
公开(公告)日：2019-10-08
申请号：US15497590
申请日：2017-04-26
Applicant: United Technologies Corporation
Inventor： James B. Coffin , Alessio Pescosolido
Abstract: A gas turbine engine includes a fan, an engine static structure, a geared architecture to drive the fan and supported relative to the static structure, a fan drive turbine to drive the geared architecture, a first member secured to the geared architecture, and a second member secured to the engine static structure and configured to cooperate with the first member to limit movement of the geared architecture relative to the static structure. A fan drive gear system and method are also disclosed.
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公开(公告)号：US10267406B2
公开(公告)日：2019-04-23
申请号：US14902018
申请日：2014-07-03
Applicant: United Technologies Corporation
Inventor： John R. Otto , Stephanie M. Baker , James B. Coffin
IPC: F02C7/06 , F02K3/06 , F01D25/18 , F16H57/04 , F04D29/063
Abstract: A lubricant manifold for gear system of a turbofan engine includes a base plate defining an inlet, an outlet and a plurality of open channels. The open channels define a portion of a corresponding plurality of lubricant passages. A cover plate is attached to the base plate to complete the formation of the plurality of lubricant passages. An interlocking interface between the base plate and the cover plate secures the cover plate to the base plate.
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公开(公告)号：US09976443B2
公开(公告)日：2018-05-22
申请号：US14774029
申请日：2014-03-14
Applicant: United Technologies Corporation
Inventor： James B. Coffin , Alessio Pescosolido
CPC classification number: F01D25/162 , B64D29/06 , F01D25/28 , F05D2220/36 , F05D2230/60 , F05D2260/40311
Abstract: A method for assembling a turbofan engine (20) comprises coupling a bearing assembly (176) and a shaft (420) as a unit to a bearing support (453). A transmission (46) and the fan shaft (132) are installed to a front frame assembly (172). The bearing assembly and shaft are installed as a unit so that the shaft engages a central gear (52) of the transmission and the bearing support engages the front frame assembly.
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Patent Agency Ranking
公开(公告)号：US09790855B2
公开(公告)日：2017-10-17
申请号：US13955385
申请日：2013-07-31
Applicant: United Technologies Corporation
Inventor： Enzo DiBenedetto , James B. Coffin , Todd A. Davis
CPC classification number: F02C7/06 , F01D25/164 , F01D25/20 , F05D2260/96
Abstract: A method for distributing liquid in a gas turbine engine is disclosed. The method includes rotating a fan shaft coupled to a spool via a fan drive gear system. The spool drives rotation of the fan shaft through the fan drive gear system during operation of the gas turbine engine. A pump is driven via the fan shaft. Liquid is supplied from a sump to the pump under a first operating condition. Liquid is supplied from an auxiliary reservoir to the pump under a second operating condition. Liquid is pumped to a damper.
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27.发明授权Forward compartment service system for a geared architecture gas turbine engine 有权用于齿轮架构燃气涡轮发动机的前车厢服务系统公开(公告)号：US09410447B2
公开(公告)日：2016-08-09
申请号：US13693733
申请日：2012-12-04
Applicant: United Technologies Corporation
Inventor： James B. Coffin , Todd A. Davis , Enzo DiBenedetto
CPC classification number: F01D25/16 , F01D9/065 , F01D25/162 , F01D25/18
Abstract: A gas turbine engine includes a jumper tube that extends through a first passage and a second passage.
Abstract translation: 燃气涡轮发动机包括延伸穿过第一通道和第二通道的跳线管。
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28.发明申请公开(公告)号：US20160195096A1
公开(公告)日：2016-07-07
申请号：US14912105
申请日：2014-08-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： John R. Otto , James B. Coffin , Jason Husband
CPC classification number: F04D25/045 , F01D5/02 , F01D15/12 , F02C3/107 , F02C7/36 , F02K3/06 , F04D25/028 , F04D27/004 , F04D29/321 , F05D2220/32 , F05D2260/40311 , F05D2270/02
Abstract: A turbofan engine is disclosed that includes a fan rotatable about an axis, a compressor section including a high pressure compressor, a medium pressure compressor and a low pressure compressor and a turbine section including a high pressure turbine, an intermediate turbine and a fan drive turbine. A fan drive gear system is driven by the fan drive turbine for driving the fan. A compressor drive gear system is driven by the intermediate turbine for driving the low pressure compressor. A gear controller controls rotation of at least one of the fan drive gear system and the compressor drive gear system relative to a static structure to vary an effective speed reduction ratio of one of the fan drive gear system and the compressor drive gear system.
Abstract translation: 公开了一种涡轮风扇发动机，其包括可围绕轴线旋转的风扇，包括高压压缩机，中压压缩机和低压压缩机的压缩机部分和包括高压涡轮机，中间涡轮机和风扇驱动涡轮机 。 风扇驱动齿轮系由风扇驱动涡轮驱动，用于驱动风扇。 压缩机驱动齿轮系由驱动低压压缩机的中间涡轮驱动。 齿轮控制器相对于静态结构控制风扇驱动齿轮系统和压缩机驱动齿轮系统中的至少一个的旋转，以改变风扇驱动齿轮系统和压缩机驱动齿轮系统之一的有效减速比。
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公开(公告)号：US20160138422A1
公开(公告)日：2016-05-19
申请号：US15007296
申请日：2016-01-27
Applicant: United Technologies Corporation
Inventor： James B. Coffin , Michael E. McCune , William G. Sheridan
IPC: F01D25/18 , F16H57/025
CPC classification number: F16H57/0467 , F01D25/18 , F02C7/36 , F05D2220/32 , F05D2260/30 , F05D2260/31 , F05D2260/40311 , F05D2260/98 , F16H57/025 , F16H57/0479
Abstract: An exemplary method of lubricating a turbomachine interface includes, among other things, securing a carrier relative to a torque frame using a flexure pin, and lubricating an interface of the flexure pin using a lubricant that has moved through a lubricant passage in the carrier and a lubricant passage in the flexure pin.
Abstract translation: 润滑涡轮机接口的示例性方法包括：使用弯曲销固定载体相对于扭矩框架的载体;以及使用已经移动通过载体中的润滑剂通道的润滑剂润滑挠曲销的界面，以及 柔性销中的润滑剂通道。
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公开(公告)号：US09033653B2
公开(公告)日：2015-05-19
申请号：US14247706
申请日：2014-04-08
Applicant: United Technologies Corporation
Inventor： James B. Coffin , John R. Otto
CPC classification number: F01D15/12 , F01D25/04 , F02C7/36 , F02K3/06 , F05D2260/40311 , F05D2260/96 , Y10T74/19642
Abstract: A gas turbine engine includes a fan section, a turbine section coupled to the fan section through a geared architecture, a first member supporting the geared architecture, and a second member supporting the first member relative to an engine static structure. The first member and the second members are spaced apart from one another at a location. A damper includes opposing ends and extending between the first member and the second member at the location for limiting relative movement between the first member and the second member. A fan drive gear system and a method are also disclosed.
Abstract translation: 燃气涡轮发动机包括风扇部分，通过齿轮架构联接到风扇部分的涡轮机部分，支撑齿轮架构的第一部件和相对于发动机静态结构支撑第一部件的第二部件。 第一构件和第二构件在一个位置处彼此间隔开。 阻尼器包括相对的端部并且在所述位置处在第一构件和第二构件之间延伸以限制第一构件和第二构件之间的相对运动。 还公开了一种风扇驱动齿轮系统和方法。
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