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公开(公告)号：US20110076134A1
公开(公告)日：2011-03-31
申请号：US12570670
申请日：2009-09-30
IPC分类号： F02G1/00
CPC分类号： F01D21/003 , F05D2260/80
摘要： A plug assembly is disclosed herein for a borescope inspection path defined through apertures in spaced walls. The plug assembly includes a first plug operable to at least partially close a first aperture in an inner wall. The plug assembly also includes a second plug operable to at least partially close a second aperture in an outer wall. The plug assembly also includes a member extending along an axis and connecting the first and second plugs together in spaced relation to one another along the axis. The member is operable to elastically buckle.
摘要翻译： 本文公开了一种插塞组件，用于通过隔开的壁中的孔限定的孔镜检查路径。 插头组件包括可操作以至少部分地封闭内壁中的第一孔的第一插头。 插头组件还包括可操作以至少部分地闭合外壁中的第二孔的第二插头。 插头组件还包括沿轴线延伸的构件，并且沿着轴线将第一和第二插塞彼此间隔开地连接在一起。 该构件可操作以弹性地弯曲。
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公开(公告)号：US08511970B2
公开(公告)日：2013-08-20
申请号：US12570670
申请日：2009-09-30
IPC分类号： F01D25/00
CPC分类号： F01D21/003 , F05D2260/80
摘要： A plug assembly is disclosed herein for a borescope inspection path defined through apertures in spaced walls. The plug assembly includes a first plug operable to at least partially close a first aperture in an inner wall. The plug assembly also includes a second plug operable to at least partially close a second aperture in an outer wall. The plug assembly also includes a member extending along an axis and connecting the first and second plugs together in spaced relation to one another along the axis. The member is operable to elastically buckle.
摘要翻译： 本文公开了一种插塞组件，用于通过隔开的壁中的孔限定的孔镜检查路径。 插头组件包括可操作以至少部分地封闭内壁中的第一孔的第一插头。 插头组件还包括可操作以至少部分地闭合外壁中的第二孔的第二插头。 插头组件还包括沿轴线延伸的构件，并且沿着轴线将第一和第二插塞彼此间隔开地连接在一起。 该构件可操作以弹性地弯曲。
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公开(公告)号：US20110008165A1
公开(公告)日：2011-01-13
申请号：US12642271
申请日：2009-12-18
申请人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
发明人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
IPC分类号： F01D25/28
CPC分类号： F01D25/246 , F01D11/005 , F01D11/122 , F01D25/243 , F05D2240/11
摘要： The present invention provides engine case systems for gas turbine engines. Embodiments of the engine case systems include a plurality of ring cases and a tie-bolt case. The ring cases may house blades and vanes for the compressor and/or for the turbine. The ring cases may be stacked in series, and may be clamped together by a tie-bolt case.
摘要翻译： 本发明提供了用于燃气涡轮发动机的发动机壳体系统。 发动机箱系统的实施例包括多个环形箱和一个连接螺栓箱。 环形箱可容纳压缩机和/或涡轮机的叶片和叶片。 环形盒可以串联堆叠，并且可以通过连接螺栓壳体夹紧在一起。
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公开(公告)号：US08444380B2
公开(公告)日：2013-05-21
申请号：US12642271
申请日：2009-12-18
申请人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
发明人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
IPC分类号： F01D25/28
摘要： The present invention provides engine case systems for gas turbine engines. Embodiments of the engine case systems include a plurality of ring cases and a tie-bolt case. The ring cases may house blades and vanes for the compressor and/or for the turbine. The ring cases may be stacked in series, and may be clamped together by a tie-bolt case.
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公开(公告)号：US08613593B2
公开(公告)日：2013-12-24
申请号：US12642271
申请日：2009-12-18
申请人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
发明人： Nathan Wesley Ottow , Vance A. Mahan , Albert Wong
IPC分类号： F01D25/28
CPC分类号： F01D25/246 , F01D11/005 , F01D11/122 , F01D25/243 , F05D2240/11
摘要： The present invention provides engine case systems for gas turbine engines. Embodiments of the engine case systems include a plurality of ring cases and a tie-bolt case. The ring cases may house blades and vanes for the compressor and/or for the turbine. The ring cases may be stacked in series, and may be clamped together by a tie-bolt case.
摘要翻译： 本发明提供了用于燃气涡轮发动机的发动机壳体系统。 发动机箱系统的实施例包括多个环形箱和一个连接螺栓箱。 环形箱可容纳压缩机和/或涡轮机的叶片和叶片。 环形盒可以串联堆叠，并且可以通过连接螺栓壳体夹紧在一起。
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公开(公告)号：US20120167595A1
公开(公告)日：2012-07-05
申请号：US13339015
申请日：2011-12-28
CPC分类号： F02C7/18 , F01D25/12 , F02C3/04 , F02C3/08 , F04D29/284 , F04D29/584 , Y02T50/675
摘要： One embodiment of the present invention is a unique gas turbine engine. Another embodiment of the present invention is a gas turbine engine having a unique secondary air flow circuit. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and secondary air flow circuits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的燃气涡轮发动机。 本发明的另一实施例是具有唯一的二次空气流动回路的燃气涡轮发动机。 其他实施例包括用于燃气涡轮发动机和二次空气流动回路的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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7.发明申请公开(公告)号：US20080156473A1
公开(公告)日：2008-07-03
申请号：US11616587
申请日：2006-12-27
IPC分类号： F28D7/10
CPC分类号： F28D7/10 , F28D21/0014 , F28D2021/0021
摘要： A heat exchanger system includes a duct having a duct wall with a duct wall outer surface and a duct wall inner surface; and a heat exchanger partial shell hermetically joined to the duct wall inner surface. The heat exchanger partial shell and a shell portion of the duct wall inner surface constitute a heat exchanger. A heat exchanger inlet manifold is defined by a nonplanar inlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger outlet manifold is defined by a nonplanar outlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger inlet opening extends through the duct wall between the inlet manifold and the heat exchanger, and a heat exchanger outlet opening extends through the duct wall between the outlet manifold and the heat exchanger.
摘要翻译： 热交换器系统包括具有管道壁的管道，管道壁具有管道壁外表面和管道壁内表面; 以及与管壁内表面气密接合的换热器部分壳体。 热交换器部分壳体和管壁内表面的壳体部分构成热交换器。 热交换器入口歧管由气密地连接到管道壁外表面的非平面入口片材料限定。 热交换器出口歧管由气密地连接到管道壁外表面的非平面出口片材限定。 热交换器入口开口延伸穿过入口歧管和热交换器之间的管道壁，并且热交换器出口开口延伸穿过出口歧管和热交换器之间的管道壁。
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公开(公告)号：US09228497B2
公开(公告)日：2016-01-05
申请号：US13339015
申请日：2011-12-28
CPC分类号： F02C7/18 , F01D25/12 , F02C3/04 , F02C3/08 , F04D29/284 , F04D29/584 , Y02T50/675
摘要： One embodiment of the present invention is a unique gas turbine engine. Another embodiment of the present invention is a gas turbine engine having a unique secondary air flow circuit. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and secondary air flow circuits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
摘要翻译： 本发明的一个实施例是独特的燃气涡轮发动机。 本发明的另一实施例是具有唯一的二次空气流动回路的燃气涡轮发动机。 其他实施例包括用于燃气涡轮发动机和二次空气流动回路的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。
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9.发明授权Heat exchanger system having manifolds structurally integrated with a duct 有权具有多个歧管的热交换器系统与管道结构地一体化公开(公告)号：US07784528B2
公开(公告)日：2010-08-31
申请号：US11616587
申请日：2006-12-27
IPC分类号： F28D7/10
CPC分类号： F28D7/10 , F28D21/0014 , F28D2021/0021
摘要： A heat exchanger system includes a duct having a duct wall with a duct wall outer surface and a duct wall inner surface; and a heat exchanger partial shell hermetically joined to the duct wall inner surface. The heat exchanger partial shell and a shell portion of the duct wall inner surface constitute a heat exchanger. A heat exchanger inlet manifold is defined by a nonplanar inlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger outlet manifold is defined by a nonplanar outlet sheet of material hermetically joined to the duct wall outer surface. A heat exchanger inlet opening extends through the duct wall between the inlet manifold and the heat exchanger, and a heat exchanger outlet opening extends through the duct wall between the outlet manifold and the heat exchanger.
摘要翻译： 热交换器系统包括具有管道壁的管道，管道壁具有管道壁外表面和管道壁内表面; 以及与管壁内表面气密接合的换热器部分壳体。 热交换器部分壳体和管壁内表面的壳体部分构成热交换器。 热交换器入口歧管由气密地连接到管道壁外表面的非平面入口片材料限定。 热交换器出口歧管由气密地连接到管道壁外表面的非平面出口片材限定。 热交换器入口开口延伸穿过入口歧管和热交换器之间的管道壁，并且热交换器出口开口延伸穿过出口歧管和热交换器之间的管道壁。
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