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公开(公告)号：US20090081035A1
公开(公告)日：2009-03-26
申请号：US11858988
申请日：2007-09-21
IPC分类号： F01D25/24
CPC分类号： F01D25/24 , F01D9/041 , F01D9/065 , F05D2240/12 , F05D2240/55
摘要： A compressor case support arrangement for a gas turbine engine includes a fan section having a central axis and a compressor case for housing a compressor. An inlet case guides air to the compressor. The compressor case is positioned axially further from the fan section than the inlet case. A support member extends between the fan section and the compressor case. The support member restricts movement of the compressor case relative to the inlet case. The support member is positioned axially further from the fan section than the plumbing access area.
摘要翻译： 用于燃气涡轮发动机的压缩机壳体支撑装置包括具有中心轴线的风扇部分和用于容纳压缩机的压缩机壳体。 入口箱将空气引导到压缩机。 压缩机壳体比入口箱更远离风扇部分。 支撑构件在风扇部分和压缩机壳体之间延伸。 支撑构件限制压缩机壳体相对于入口壳体的移动。 支撑构件比管道通路区域更远离风扇部分。
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公开(公告)号：US20090056306A1
公开(公告)日：2009-03-05
申请号：US11846095
申请日：2007-08-28
摘要： A turbine engine is disclosed that includes a fan case surrounding a fan. A core is supported relative to the fan case by support structure, such as flow exit guide vanes, which are arranged downstream from the fan. The core includes a core housing having an inlet case arranged to receive airflow from the fan. A compressor case is arranged axially adjacent to the inlet case and surrounds a compressor stage. In one example, the example turbine engine includes a gear train arranged between the fan and a spool. The gear train is axially aligned and supported by the inlet case. An intermediate case is arranged axially adjacent to the compressor case. The support structure is arranged axially forward of the intermediate case. In one example, the support structure is axially aligned with the compressor case.
摘要翻译： 公开了一种涡轮发动机，其包括围绕风扇的风扇壳体。 通过诸如流出口导向叶片的支撑结构相对于风扇壳体支撑芯体，其布置在风扇的下游。 芯部包括具有入口壳体的芯壳体，其布置成接收来自风扇的气流。 压缩机壳体布置成与入口壳体相邻并围绕压缩机台。 在一个示例中，示例性涡轮发动机包括布置在风扇和阀芯之间的齿轮系。 齿轮系轴向对齐并由入口箱支撑。 中间壳体被布置成与压缩机壳体轴向相邻。 支撑结构被布置在中间壳体的轴向前方。 在一个示例中，支撑结构与压缩机壳体轴向对准。
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公开(公告)号：US09957918B2
公开(公告)日：2018-05-01
申请号：US11846095
申请日：2007-08-28
摘要： A turbine engine is disclosed that includes a fan case surrounding a fan. A core is supported relative to the fan case by support structure, such as flow exit guide vanes, which are arranged downstream from the fan. The core includes a core housing having an inlet case arranged to receive airflow from the fan. A compressor case is arranged axially adjacent to the inlet case and surrounds a compressor stage. In one example, the example turbine engine includes a gear train arranged between the fan and a spool. The gear train is axially aligned and supported by the inlet case. An intermediate case is arranged axially adjacent to the compressor case. The support structure is arranged axially forward of the intermediate case. In one example, the support structure is axially aligned with the compressor case.
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公开(公告)号：US09946699B1
公开(公告)日：2018-04-17
申请号：US13598546
申请日：2012-08-29
CPC分类号： G06F17/243 , G06Q30/04 , G06Q40/123 , G10L15/26
摘要： Methods, systems and articles of manufacture for location-based speech recognition for preparation of an electronic tax return.
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公开(公告)号：US09915154B2
公开(公告)日：2018-03-13
申请号：US13116093
申请日：2011-05-26
CPC分类号： F01D5/282 , C04B37/00 , C04B2235/5244 , C04B2237/365 , C04B2237/38 , C04B2237/76 , F01D5/147 , F01D5/284 , F01D9/041 , F01D25/246 , F05D2240/12 , F05D2300/6033 , Y10T29/49321
摘要： A Ceramic Matrix Composite (CMC) airfoil segment for a gas turbine engine includes a box-shape fiber geometry which defines a rectilinear pressure side bond line and a rectilinear suction side bond line.
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86.发明授权Constant-speed pump system for engine thermal management system AOC reduction and environmental control system loss elimination 有权恒速泵系统用于发动机热管理系统AOC减排和环境控制系统损耗消除公开(公告)号：US09151224B2
公开(公告)日：2015-10-06
申请号：US13419695
申请日：2012-03-14
IPC分类号： F02C7/14 , F02C3/09 , F02C9/16 , F02C3/10 , F02C7/32 , F02C7/36 , F02C6/08 , F01D15/08 , F02C6/04
CPC分类号： F02C6/08 , F01D15/08 , F02C7/32 , F02K3/06 , Y02T50/671
摘要： A gas turbine engine has a spool, a towershaft connected to the spool and an impeller pump. An integrated drive pump is connected to the towershaft and to the impeller pump for driving the impeller pump at a constant speed. The integrated drive pump is positioned on an engine core. The gas turbine engine includes a fan and a bypass duct located between a cowl and the engine core. The gas turbine engine includes an intake manifold for the impeller pump, and the intake manifold receives air from the bypass duct.
摘要翻译： 燃气涡轮发动机具有阀芯，连接到阀芯的塔轴和叶轮泵。 集成的驱动泵连接到塔轴和叶轮泵，以恒定的速度驱动叶轮泵。 集成驱动泵位于发动机芯上。 燃气涡轮发动机包括位于罩和发动机芯之间的风扇和旁通管。 燃气涡轮发动机包括用于叶轮泵的进气歧管，并且进气歧管从旁路管道接收空气。
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公开(公告)号：US09121346B2
公开(公告)日：2015-09-01
申请号：US13419649
申请日：2012-03-14
CPC分类号： F02C7/14 , F01D25/12 , F02C7/224 , F02K3/06 , F04D29/5826 , F05D2250/36
摘要： An engine includes a duct containing a flow of cool air and a pump system having an impeller with an inlet for receiving air from the duct and an outlet for discharging air into a discharge manifold. The discharge manifold containing at least one heat exchanger which forms part of a thermal management system.
摘要翻译： 发动机包括含有冷空气流的管道和具有叶轮的泵系统，叶轮具有用于从管道接收空气的入口和用于将空气排放到排放歧管中的出口。 排放歧管包含形成热管理系统的一部分的至少一个热交换器。
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公开(公告)号：US09097186B2
公开(公告)日：2015-08-04
申请号：US13360752
申请日：2012-01-29
申请人： Hung Duong , Gabriel L. Suciu , Christopher M. Dye
发明人： Hung Duong , Gabriel L. Suciu , Christopher M. Dye
CPC分类号： F02C7/32 , F02C7/36 , F05D2260/532
摘要： An accessory box for a gas turbine engine has an input gear to be driven by an input shaft. The input gear is engaged to drive a first driven gear on one radial side of a drive axis of the input gear. The first gear drives at least a second driven gear on one radial side of the drive axis, with at least one accessory driven by one of the first and second driven gears. The second driven gear drives a bevel gear arrangement to drive a third driven gear on an opposed side of the drive axis of the input gear. The third driven gear drives at least a second accessory. The accessories are associated with a gas turbine engine.
摘要翻译： 用于燃气涡轮发动机的附件箱具有由输入轴驱动的输入齿轮。 输入齿轮接合以在输入齿轮的驱动轴的一个径向侧上驱动第一从动齿轮。 第一齿轮在驱动轴的一个径向侧驱动至少第二从动齿轮，至少一个附件由第一和第二从动齿轮中的一个驱动。 第二从动齿轮驱动锥齿轮装置以驱动输入齿轮的驱动轴线的相对侧上的第三从动齿轮。 第三从动齿轮驱动至少一个第二附件。 附件与燃气涡轮发动机有关。
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公开(公告)号：US09097137B2
公开(公告)日：2015-08-04
申请号：US13327722
申请日：2011-12-15
CPC分类号： F01D17/162 , F04D29/563
摘要： An actuator module for a gas turbine engine includes a multiple of actuators mounted within a common actuator housing.
摘要翻译： 用于燃气涡轮发动机的致动器模块包括安装在公共致动器壳体内的多个致动器。
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公开(公告)号：US09068515B2
公开(公告)日：2015-06-30
申请号：US13313433
申请日：2011-12-07
申请人： Hung Duong , Gabriel L. Suciu , Christopher M. Dye
发明人： Hung Duong , Gabriel L. Suciu , Christopher M. Dye
CPC分类号： F02C7/00 , F02C7/32 , F02C7/36 , F05D2230/70 , F05D2250/312 , F16H1/20 , Y10T29/49464
摘要： An accessory system for a gas turbine engine includes an accessory gearbox which defines an accessory gearbox axis and includes first and second sides. A first geartrain includes one or more shafts rotatable about axes perpendicular to the first side of the accessory gearbox and a second geartrain includes one or more shafts rotatable about axes perpendicular to the second side of the accessory gearbox. A driven gear set defines an input axis and drives first geartrain and the second geartrain about corresponding first and second drive axes parallel to the input axis.
摘要翻译： 用于燃气涡轮发动机的附件系统包括限定附件齿轮箱轴线并包括第一和第二侧面的附件齿轮箱。 第一齿轮箱包括可围绕垂直于附件齿轮箱的第一侧的轴线旋转的一个或多个轴，并且第二齿轮箱包括可围绕垂直于附件齿轮箱的第二侧的轴线旋转的一个或多个轴。 从动齿轮组限定输入轴并且驱动第一齿轮和第二齿轮组，绕相应于输入轴平行的第一和第二驱动轴。
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