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1.发明申请公开(公告)号：US20120280082A1
公开(公告)日：2012-11-08
申请号：US13524127
申请日：2012-06-15
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
IPC分类号： B64C7/02
CPC分类号： F01D25/28 , B64D29/06 , F02C7/20 , F05D2230/72
摘要： A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end. The fan cowl is coupled to an engine mounting pylon via a slider-type mounting system that includes at least one slider track assembly defining at least one slot therein. The at least one slot is configured to receive at least one fan cowl slider fitting.
摘要翻译： 用于容纳发动机的机舱包括尺寸适于覆盖发动机的至少第一轴向部分的风扇罩。 发动机包括入口端，排气端以及从入口端经过排气端延伸穿过发动机的轴线。 风扇罩通过滑块式安装系统联接到发动机安装塔架，滑块式安装系统包括至少一个在其中限定至少一个狭槽的滑块轨道组件。 所述至少一个狭槽被配置为容纳至少一个风扇整流罩滑块配件。
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2.发明授权公开(公告)号：US09188026B2
公开(公告)日：2015-11-17
申请号：US13524127
申请日：2012-06-15
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
CPC分类号： F01D25/28 , B64D29/06 , F02C7/20 , F05D2230/72
摘要： A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end. The fan cowl is coupled to an engine mounting pylon via a slider-type mounting system that includes at least one slider track assembly defining at least one slot therein. The at least one slot is configured to receive at least one fan cowl slider fitting.
摘要翻译： 用于容纳发动机的机舱包括尺寸适于覆盖发动机的至少第一轴向部分的风扇罩。 发动机包括入口端，排气端以及从入口端经过排气端延伸穿过发动机的轴线。 风扇罩通过滑块式安装系统联接到发动机安装塔架，滑块式安装系统包括至少一个在其中限定至少一个狭槽的滑块轨道组件。 所述至少一个狭槽被配置为容纳至少一个风扇整流罩滑块配件。
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公开(公告)号：US20100127116A1
公开(公告)日：2010-05-27
申请号：US12324429
申请日：2008-11-26
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
CPC分类号： F01D25/28 , B64D29/06 , F02C7/20 , Y02T50/671 , Y10T29/49826
摘要： A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end is provided. The method includes providing a cowl sized to cover at least a portion of the engine and coupling the cowl to the engine such that the cowl is slideable along the axis toward at least one of the inlet end and the exhaust end.
摘要翻译： 提供了一种组装用于燃气涡轮发动机的机舱的方法，其包括入口端，排气端和从入口端经过排气端延伸穿过发动机的轴线。 该方法包括提供一个整流罩，其尺寸设置成覆盖发动机的至少一部分并将整流罩耦合到发动机，使得整流罩可以沿着该轴线朝着入口端和排气端中的至少一个滑动。
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公开(公告)号：US09188025B2
公开(公告)日：2015-11-17
申请号：US13524036
申请日：2012-06-15
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
CPC分类号： F01D25/28 , B64C7/02 , B64D29/06 , F02C7/20 , F05D2230/72 , Y02T50/671
摘要： A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end. The fan cowl is coupled to an engine mounting pylon via a mounting assembly including at least one power drive system. The fan cowl is movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end.
摘要翻译： 用于容纳发动机的机舱包括尺寸适于覆盖发动机的至少第一轴向部分的风扇罩。 发动机包括入口端，排气端以及从入口端经过排气端延伸穿过发动机的轴线。 风扇罩通过包括至少一个动力驱动系统的安装组件联接到发动机安装塔。 风扇罩可相对于发动机沿着轴线朝向入口端和排气端中的至少一个移动。
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公开(公告)号：US20120280081A1
公开(公告)日：2012-11-08
申请号：US13524036
申请日：2012-06-15
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
IPC分类号： B64C7/02
CPC分类号： F01D25/28 , B64C7/02 , B64D29/06 , F02C7/20 , F05D2230/72 , Y02T50/671
摘要： A nacelle for housing an engine includes a fan cowl sized to cover at least a first axial portion of the engine. The engine includes an inlet end, an exhaust end, and an axis extending through the engine from the inlet end through the exhaust end. The fan cowl is coupled to an engine mounting pylon via a mounting assembly including at least one power drive system. The fan cowl is movable with respect to the engine along the axis toward at least one of the inlet end and the exhaust end.
摘要翻译： 用于容纳发动机的机舱包括尺寸适于覆盖发动机的至少第一轴向部分的风扇罩。 发动机包括入口端，排气端以及从入口端经过排气端延伸穿过发动机的轴线。 风扇罩通过包括至少一个动力驱动系统的安装组件联接到发动机安装塔。 风扇罩可相对于发动机沿着轴线朝向入口端和排气端中的至少一个移动。
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公开(公告)号：US08220738B2
公开(公告)日：2012-07-17
申请号：US12324429
申请日：2008-11-26
申请人： David P. Calder , Graham F. Howarth
发明人： David P. Calder , Graham F. Howarth
CPC分类号： F01D25/28 , B64D29/06 , F02C7/20 , Y02T50/671 , Y10T29/49826
摘要： A method of assembling a nacelle for a gas turbine engine that includes an inlet end, an exhaust end, and an axis that extends through the engine from the inlet end through the exhaust end is provided. The method includes providing a cowl sized to cover at least a portion of the engine and coupling the cowl to the engine such that the cowl is slideable along the axis toward at least one of the inlet end and the exhaust end.
摘要翻译： 提供了一种组装用于燃气涡轮发动机的机舱的方法，其包括入口端，排气端和从入口端经过排气端延伸穿过发动机的轴线。 该方法包括提供一个整流罩，其尺寸设置成覆盖发动机的至少一部分并将整流罩耦合到发动机，使得整流罩可以沿着该轴线朝着入口端和排气端中的至少一个滑动。
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公开(公告)号：US20100112283A1
公开(公告)日：2010-05-06
申请号：US12262840
申请日：2008-10-31
CPC分类号： B29C70/545 , B29C70/42 , B29K2995/0002 , B29L2031/3076 , Y02T50/43 , Y10T156/1057 , Y10T428/24322
摘要： Method including: (a) forming a laminate structure including a plurality of uncured prepreg sheets, wherein the laminate structure comprises an initial substantially planar configuration; (b) subjecting the laminate structure to suitable first curing conditions to provide a partially cured laminate structure while maintaining the substantially planar configuration; (c) providing the partially cured laminate structure with a plurality of perforations to provide a partially cured and perforated laminate structure; (d) shaping the partially cured and perforated laminate structure; and (e) subjecting the partially cured and perforated laminate structure to second curing conditions at least partially simultaneously with or after step (d) to provide a shaped and finally cured laminate structure.
摘要翻译： 方法包括：（a）形成包括多个未固化的预浸料片的层压结构，其中层压结构包括初始的基本上平面的构型; （b）使层压结构经受合适的第一固化条件以提供部分固化的层压结构，同时保持基本平坦的构型; （c）提供具有多个穿孔的部分固化的层压结构，以提供部分固化和穿孔的层压结构; （d）使部分固化和穿孔的层压结构成形; 和（e）在步骤（d）之后或之后至少部分同时对部分固化和穿孔的层压结构进行第二固化条件，以提供成形且最终固化的层压结构。
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