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公开(公告)号：US20150121841A1
公开(公告)日：2015-05-07
申请号：US14206232
申请日：2014-03-12
摘要： A gas turbine engine includes a core engine, a first bypass passage disposed about the core engine and a second bypass passage disposed about the first bypass passage. A flow control is disposed within the second bypass for controlling bypass airflow through the second bypass. The flow control translates axially between an open position and a closed position to vary and control airflow through the second bypass passage.
摘要翻译： 燃气涡轮发动机包括核心发动机，围绕核心发动机设置的第一旁路通道和围绕第一旁路通道设置的第二旁路通道。 流量控制器设置在第二旁路内用于控制通过第二旁路的旁路气流。 流量控制在打开位置和关闭位置之间轴向平移以改变和控制通过第二旁路通道的气流。
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公开(公告)号：US09523502B2
公开(公告)日：2016-12-20
申请号：US14173935
申请日：2014-02-06
CPC分类号： F23R3/002 , F16B19/109 , F16B21/02 , F23R3/007 , F23R3/60 , F23R2900/00017 , Y10T29/49826
摘要： A push-lock device for connecting a tile to a gas turbine engine wall includes, among other things, a housing extending longitudinally along an axis; a shaft assembly within the housing, the shaft assembly including portions of both a push-down pop-up mechanism and a locking-bracket mechanism, the locking-bracket mechanism moveable to a locked position such that the locking-bracket mechanism limits movement of a tile away from a gas turbine engine wall; and a biasing member to be positioned closer to the tile than the locking-bracket mechanism.
摘要翻译： 用于将瓦片连接到燃气涡轮发动机壁的推动锁定装置包括沿轴线纵向延伸的壳体; 所述轴组件包括在所述壳体内的轴组件，所述轴组件包括下推弹出机构和锁定支架机构的部分，所述锁定支架机构可移动到锁定位置，使得所述锁定支架机构限制 瓦片远离燃气涡轮发动机壁; 以及偏置构件，其被定位成比锁定支架机构更靠近瓦片。
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公开(公告)号：US09243515B2
公开(公告)日：2016-01-26
申请号：US13672081
申请日：2012-11-08
CPC分类号： F01D25/24 , F01D25/14 , F01D25/28 , F01D25/30 , F02C7/20 , F02K1/822 , F05D2230/642 , F23R3/60 , Y02T50/675
摘要： A turbine engine case includes a first panel, a second panel and a support hanger. The second panel defines an aperture. The support hanger includes a strut that is connected to the first panel, and a base that is pivotally connected to the strut. The base includes a pivot member that is pivotally engaged with the second panel. The base extends away from the strut and through the aperture to the pivot member.
摘要翻译： 涡轮发动机壳体包括第一面板，第二面板和支撑架。 第二个面板定义一个光圈。 支撑架包括连接到第一面板的支柱和枢轴连接到支柱的基座。 底座包括与第二面板枢转接合的枢转构件。 基座从支柱延伸并且穿过孔径延伸到枢转构件。
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公开(公告)号：US09664389B2
公开(公告)日：2017-05-30
申请号：US14568896
申请日：2014-12-12
CPC分类号： F23R3/002 , F02K1/822 , F23M5/04 , F23M2900/05004 , F23R3/007 , F23R3/60 , Y02T50/675
摘要： One exemplary embodiment of this disclosure relates to a gas turbine engine. The engine includes a first attachment member including an opening, a second attachment member including a loop at least partially extending through the opening, and a pin between the first attachment member and the loop.
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公开(公告)号：US10054080B2
公开(公告)日：2018-08-21
申请号：US13656888
申请日：2012-10-22
CPC分类号： F02K1/822 , F05D2250/25 , F05D2260/30 , Y02T50/675 , Y10T29/49234
摘要： A hanger assembly for use between a first duct and a second duct having an opening therein includes a spring having a first end and a second end, a first mount for attaching the first end to the first duct, a second mount for attaching the second end to the second duct, the second mount having an area greater than the opening, and a central aperture therethrough.
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公开(公告)号：US09568036B2
公开(公告)日：2017-02-14
申请号：US14173882
申请日：2014-02-06
CPC分类号： F16B21/165 , F02K1/822 , F02K1/827 , Y02T50/675 , Y10T29/4932
摘要： A push-lock pin for connecting a tile to a gas turbine engine wall according to an exemplary aspect of the present disclosure includes, among other things, a housing extending longitudinally along an axis; a shaft assembly within the housing, the shaft assembly including a push-down pop-up mechanism and a locking mechanism, the locking mechanism moveable to a locked position such that the locking mechanism limits movement of a tile away from a gas turbine engine wall; and a stop feature to limit movement of the tile toward the gas turbine engine wall.
摘要翻译： 根据本公开的示例性方面的用于将瓦片连接到燃气涡轮发动机壁的推动锁定销包括：沿轴线纵向延伸的壳体; 轴组件，其在所述壳体内，所述轴组件包括下推弹出机构和锁定机构，所述锁定机构可移动到锁定位置，使得所述锁定机构限制瓦片远离燃气涡轮发动机壁的运动; 以及限制瓦片朝向燃气涡轮发动机壁的运动的停止特征。
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公开(公告)号：US09249732B2
公开(公告)日：2016-02-02
申请号：US13672124
申请日：2012-11-08
CPC分类号： F02C7/20 , F01D25/14 , F01D25/28 , F02K1/80 , F02K1/82 , F05D2220/32 , F05D2230/232 , F05D2230/642 , F05D2240/54 , F05D2240/55 , F05D2250/42 , F05D2260/30 , F05D2300/174 , F05D2300/177 , F05D2300/5021 , F16B5/065 , F23R3/002 , F23R3/60
摘要： A support hanger is provided for a turbine engine. The support hanger includes a pin with a pin head, a retainer and a flexible seal. The retainer is pivotally connected to the pin head. The retainer includes a seal bearing surface facing towards the pin head. The seal includes a retainer bearing surface sealingly engaging the seal bearing surface.
摘要翻译： 为涡轮发动机提供支撑架。 支撑架包括具有销头，保持器和柔性密封件的销。 保持器枢转地连接到销头。 保持器包括面向销头的密封件支承表面。 密封件包括密封地接合密封件支承表面的保持器支承表面。
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公开(公告)号：US20140255182A1
公开(公告)日：2014-09-11
申请号：US14173882
申请日：2014-02-06
CPC分类号： F16B21/165 , F02K1/822 , F02K1/827 , Y02T50/675 , Y10T29/4932
摘要： A push-lock pin for connecting a tile to a gas turbine engine wall according to an exemplary aspect of the present disclosure includes, among other things, a housing extending longitudinally along an axis; a shaft assembly within the housing, the shaft assembly including a push-down pop-up mechanism and a locking mechanism, the locking mechanism moveable to a locked position such that the locking mechanism limits movement of a tile away from a gas turbine engine wall; and a stop feature to limit movement of the tile toward the gas turbine engine wall.
摘要翻译： 根据本公开的示例性方面的用于将瓦片连接到燃气涡轮发动机壁的推动锁定销包括：沿轴线纵向延伸的壳体; 轴组件，其在所述壳体内，所述轴组件包括下推弹出机构和锁定机构，所述锁定机构可移动到锁定位置，使得所述锁定机构限制瓦片远离燃气涡轮发动机壁的运动; 以及限制瓦片朝向燃气涡轮发动机壁的运动的停止特征。
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公开(公告)号：US20140255172A1
公开(公告)日：2014-09-11
申请号：US14173935
申请日：2014-02-06
CPC分类号： F23R3/002 , F16B19/109 , F16B21/02 , F23R3/007 , F23R3/60 , F23R2900/00017 , Y10T29/49826
摘要： A push-lock device for connecting a tile to a gas turbine engine wall includes, among other things, a housing extending longitudinally along an axis; a shaft assembly within the housing, the shaft assembly including portions of both a push-down pop-up mechanism and a locking-bracket mechanism, the locking-bracket mechanism moveable to a locked position such that the locking-bracket mechanism limits movement of a tile away from a gas turbine engine wall; and a biasing member to be positioned closer to the tile than the locking-bracket mechanism.
摘要翻译： 用于将瓦片连接到燃气涡轮发动机壁的推动锁定装置包括沿轴线纵向延伸的壳体; 所述轴组件包括在所述壳体内的轴组件，所述轴组件包括下推弹出机构和锁定支架机构的部分，所述锁定支架机构可移动到锁定位置，使得所述锁定支架机构限制 瓦片远离燃气涡轮发动机壁; 以及偏置构件，其被定位成比锁定支架机构更靠近瓦片。
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公开(公告)号：US20140093369A1
公开(公告)日：2014-04-03
申请号：US13672081
申请日：2012-11-08
IPC分类号： F01D25/24
CPC分类号： F01D25/24 , F01D25/14 , F01D25/28 , F01D25/30 , F02C7/20 , F02K1/822 , F05D2230/642 , F23R3/60 , Y02T50/675
摘要： A turbine engine case includes a first panel, a second panel and a support hanger. The second panel defines an aperture. The support hanger includes a strut that is connected to the first panel, and a base that is pivotally connected to the strut. The base includes a pivot member that is pivotally engaged with the second panel. The base extends away from the strut and through the aperture to the pivot member.
摘要翻译： 涡轮发动机壳体包括第一面板，第二面板和支撑架。 第二个面板定义一个光圈。 支撑架包括连接到第一面板的支柱和枢轴连接到支柱的底座。 底座包括与第二面板枢转接合的枢转构件。 基座从支柱延伸并且穿过孔径延伸到枢转构件。
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