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公开(公告)号：US20150247460A1
公开(公告)日：2015-09-03
申请号：US14427396
申请日：2013-02-10
发明人： Marc R. Sauerhoefer , Ryan K. Snyder , James D. Marshall , Kari L. Kisselbrack , Thomas Livingston
摘要： An adapter for a gas turbine engine has a first portion with a control module mount interface. A second portion with a sensor mount interface defines a sensor mount position relative to a control module. A connecting body connects the first and second portions such that the second portion provides a re-orientated sensor mount position relative to the control module. A lubrication system for a gas turbine engine is also disclosed.
摘要翻译： 用于燃气涡轮发动机的适配器具有带有控制模块安装接口的第一部分。 具有传感器安装接口的第二部分定义相对于控制模块的传感器安装位置。 连接体连接第一和第二部分，使得第二部分相对于控制模块提供重新定向的传感器安装位置。 还公开了一种用于燃气涡轮发动机的润滑系统。
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公开(公告)号：US20140334916A1
公开(公告)日：2014-11-13
申请号：US14273111
申请日：2014-05-08
发明人： Ryan K. Snyder , Michael Dreher
IPC分类号： F01D25/28
CPC分类号： F01D25/285 , F01D21/003 , G02B23/2492
摘要： A borescope inspection (BSI) port fitting is provided for a gas turbine engine. The borescope inspection (BSI) port fitting includes a housing with a borescope inspection port.
摘要翻译： 为燃气涡轮发动机提供管道检查（BSI）端口接头。 管道检查（BSI）端口接头包括一个带孔镜检查口的外壳。
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公开(公告)号：US20140231437A1
公开(公告)日：2014-08-21
申请号：US14186435
申请日：2014-02-21
IPC分类号： B60K15/04
CPC分类号： F01D25/18 , F01D25/00 , F01M11/0458 , F01M2011/0491 , F05D2260/98 , F16N19/00 , F16N31/00
摘要： A cap assembly includes a plunger mounted to a retainer pin and a latch operable to retract the retainer pin.
摘要翻译： 帽组件包括安装到保持销的柱塞和可操作以缩回保持销的闩锁。
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公开(公告)号：US20190341965A1
公开(公告)日：2019-11-07
申请号：US16516393
申请日：2019-07-19
发明人： Ryan K. Snyder , Eric J. Heims
摘要： A wave guide assembly for a control and diagnostic system for a machine, the wave guide assembly includes a housing defining an exterior surface and an internal cavity extending between distal ends. A wave guide is defined within the internal cavity. At least one open conduit is defined within the internal cavity providing a space for routing conductors through the housing. A fluid passage is defined within the internal cavity separate from the wave guide. A control and diagnostic system for a machine and a gas turbine engine are also disclosed.
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公开(公告)号：US20180289359A1
公开(公告)日：2018-10-11
申请号：US15480757
申请日：2017-04-06
发明人： Eric J. Heims , Ryan K. Snyder , Kurt J. Sobanski
CPC分类号： A61B8/485 , A61B8/13 , A61B8/14 , A61B8/4483 , A61B8/5207 , F01D21/003 , F05D2260/80 , F23N2023/38 , F23N2900/05004 , F23N2900/05005 , H01P1/042
摘要： A wave guide assembly for a control and diagnostic system for a machine includes a housing defining an exterior surface and an internal cavity extending between distal ends. At least one wave guide within the internal cavity defines a wave propagation passage for at least one wave form signal. At least one conductor within the internal cavity is separate from the wave guide. A control and diagnostic system for a machine and a gas turbine engine are also disclosed.
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公开(公告)号：US09988943B2
公开(公告)日：2018-06-05
申请号：US14696615
申请日：2015-04-27
发明人： James P. Chasse, Jr. , Ryan K. Snyder , William K. Ackermann , Pellegrino J. Pisacreta , Judith F. Brooks , Stephanie Ernst
CPC分类号： F01D25/28 , F01D25/12 , F01D25/14 , F02C7/18 , Y02T50/675
摘要： A fitting according to an exemplary aspect of the present disclosure includes, among other things, a main body portion having a first axial end and a second axial end opposite the first axial end, an inlet provided at the first axial end, and an outlet adjacent the second axial end. The outlet includes a plurality of circumferentially spaced-apart slots formed through the main body portion, and each slot has an area within a range of 0.52 and 0.59 square inches.
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公开(公告)号：US09982601B2
公开(公告)日：2018-05-29
申请号：US14726993
申请日：2015-06-01
CPC分类号： F02C7/06 , F01D25/18 , F01D25/20 , F01M1/02 , F01M1/16 , F01M5/002 , F01M11/02 , F05D2220/32 , F05D2260/98
摘要： An oil lubrication system is provided. The oil lubrication system may comprise an oil pump, a conduit fluidly coupled to the oil pump, and a damper fluidly coupled to the conduit. The damper may further comprise a volume configured to receive oil in response to a pulse event. A heat exchanger may also be fluidly coupled to the conduit. In various embodiments, the damper may comprise a spherical volume. The damper may be fluidly coupled to the conduit between the oil pump and the heat exchanger. An adapter may be mechanically coupled between the conduit and the damper. The adapter may comprise a passage in fluid communication with the conduit and the damper. The damper may further comprise a membrane. A gas or compressible fluid may be disposed in the damper on a first side of the membrane. The membrane may be configured to separate the gas from the oil.
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公开(公告)号：US20160333791A1
公开(公告)日：2016-11-17
申请号：US15111572
申请日：2015-02-04
发明人： Ryan K. Snyder , Eric J. Heims , Mark W. Colebrook
IPC分类号： F02C7/32 , F02C3/04 , F02C7/14 , B64D29/08 , F01D25/20 , F01D25/26 , F01D25/28 , B64D27/10 , F02K3/06 , H02K7/18
CPC分类号： F02C7/32 , B64C7/02 , B64D27/10 , B64D29/06 , B64D29/08 , F01D25/20 , F01D25/265 , F01D25/28 , F02C3/04 , F02C7/14 , F02K3/06 , F05D2220/327 , F05D2230/72 , F05D2250/30 , F05D2250/411 , H02K7/1823 , Y02T50/671
摘要： A gas turbine engine comprises a compressor, a combustor and a turbine. A housing for the gas turbine engine includes a mount member to define a vertically upper location. Sides of the engine are defined on opposed sides of the mount, with a fuel filter, a fuel pump and a fuel flow meter being positioned on a first side and an oil pump, an oil filter and an oil tank positioned on a second of the sides.
摘要翻译： 燃气涡轮发动机包括压缩机，燃烧器和涡轮机。 用于燃气涡轮发动机的壳体包括用于限定垂直上方位置的安装构件。 发动机的侧面限定在安装座的相对侧上，燃料过滤器，燃料泵和燃料流量计位于第一侧，油泵，油过滤器和油箱位于第二侧 边。
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19.发明申请公开(公告)号：US20160177828A1
公开(公告)日：2016-06-23
申请号：US14606076
申请日：2015-01-27
发明人： Ryan K. Snyder , Michael R. Thomas
CPC分类号： F02C6/08 , F02C7/185 , F02K3/075 , F02K3/077 , F02K3/115 , F05D2260/213 , Y02T50/675
摘要： A gas turbine bypass flow arrangement comprises an outer housing and an inner housing, an outer bypass duct defined between the outer housing and the inner housing and an inner bypass duct defined inwardly of the inner housing. A first heat exchanger is positioned at an upstream location within the outer bypass duct and a second heat exchanger is positioned within the inner bypass duct at an upstream location. A downstream heat exchanger is positioned to be in the path of air downstream of the second heat exchanger in the inner bypass duct. Air flowing across the downstream heat exchanger passes from the inner bypass duct into the outer bypass duct. A gas turbine engine is also disclosed.
摘要翻译： 燃气轮机旁路流动装置包括外壳体和内壳体，限定在外壳体和内壳体之间的外旁通管道以及限定在内壳体内侧的内旁通管道。 第一热交换器定位在外部旁路管道内的上游位置处，并且第二热交换器位于内部旁通管道的上游位置处。 下游热交换器被定位成位于内部旁通管道中的第二热交换器下游的空气路径中。 流过下游热交换器的空气从内部旁通管道进入外部旁路管道。 还公开了一种燃气涡轮发动机。
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公开(公告)号：US20160090190A1
公开(公告)日：2016-03-31
申请号：US14866119
申请日：2015-09-25
发明人： Ryan K. Snyder , Eric J. Heims
CPC分类号： B64D45/00 , B01D46/10 , B01D2273/10 , B01D2279/60 , B64D33/02 , B64D33/08 , F02C7/05 , F02C7/052 , F02C7/055 , F02C7/14 , F02K3/115 , F05D2260/213 , F05D2260/607 , F05D2260/98 , Y02T50/671 , Y02T50/675
摘要： Aspects of the disclosure are directed to a screen configured for use in association with a cooler of an aircraft, the screen comprising: a first portion arranged as a grid and located in a line-of-sight of the cooler with respect to a fluid inlet, and a second portion located out of the line-of-sight of the cooler with respect to the fluid inlet, wherein the second portion is grid-free.
摘要翻译： 本公开的方面涉及被配置为与飞机的冷却器相关联使用的屏幕，该屏幕包括：第一部分，布置成格栅并且相对于流体入口位于冷却器的视线内 以及位于冷却器相对于流体入口的视线之外的第二部分，其中第二部分是无栅格的。
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