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1. 发明授权

US08469309B2 Monolithic structure for mounting aircraft engine 有权
标题翻译：用于安装飞机发动机的整体结构
公开(公告)号：US08469309B2
公开(公告)日：2013-06-25
申请号：US12343833
申请日：2008-12-24
申请人： Alan Roy Stuart , Mark Linz
发明人： Alan Roy Stuart , Mark Linz
IPC分类号： B64D27/26 , F16M13/00 , F02C7/20
CPC分类号： B64D27/18 , B64D27/26 , B64D29/00 , Y02T50/44
摘要： Assembly includes an integral monolithic structure for mounting an engine to an aircraft. The monolithic structure includes a nacelle portion and a support structure. The nacelle portion includes an inlet region and a fan case region defining an annular wall about an axial channel. A ring member disposed in the axial channel is connected through a plurality of radial elements to the annular wall. The support structure portion includes a forward section integral with the nacelle portion and an aft section including at least one aircraft mount region for mounting the monolithic structure to an aircraft. The forward section includes an inlet stiffening region radially outward of the annular wall. When mounted on the aircraft, the nacelle portion and the support structure portion cooperate to form a first load path operable to transmit an applied nacelle maneuvering force directly to the aircraft instead of through the engine core.
摘要翻译：组件包括用于将发动机安装到飞行器的整体单块结构。整体结构包括机舱部分和支撑结构。机舱部分包括入口区域和限定围绕轴向通道的环形壁的风扇壳体区域。设置在轴向通道中的环构件通过多个径向元件连接到环形壁。所述支撑结构部分包括与所述机舱部分成一体的前部部分和包括用于将所述整体结构安装到飞行器的至少一个飞行器安装区域的后部部分。前部包括在环形壁的径向外侧的入口加强区域。当安装在飞机上时，机舱部分和支撑结构部分协作以形成第一负载路径，其可操作以将施加的机舱机动动力直接传递到飞行器而不是通过发动机机芯。

2. 发明申请

US20100155525A1 MONOLITHIC STRUCTURE FOR MOUNTING AIRCRAFT ENGINE 有权
标题翻译：用于安装飞机发动机的单片结构
公开(公告)号：US20100155525A1
公开(公告)日：2010-06-24
申请号：US12343833
申请日：2008-12-24
申请人： Alan Roy Stuart , Mark Linz
发明人： Alan Roy Stuart , Mark Linz
IPC分类号： B64D27/00 , F02K3/02 , F01D25/28
CPC分类号： B64D27/18 , B64D27/26 , B64D29/00 , Y02T50/44
摘要： Assembly includes an integral monolithic structure for mounting an engine to an aircraft. The monolithic structure includes a nacelle portion and a support structure. The nacelle portion includes an inlet region and a fan case region defining an annular wall about an axial channel. A ring member disposed in the axial channel is connected through a plurality of radial elements to the annular wall. The support structure portion includes a forward section integral with the nacelle portion and an aft section including at least one aircraft mount region for mounting the monolithic structure to an aircraft. The forward section includes an inlet stiffening region radially outward of the annular wall. When mounted on the aircraft, the nacelle portion and the support structure portion cooperate to form a first load path operable to transmit an applied nacelle maneuvering force directly to the aircraft instead of through the engine core.
摘要翻译：组件包括用于将发动机安装到飞机上的整体单体结构。整体结构包括机舱部分和支撑结构。机舱部分包括入口区域和限定围绕轴向通道的环形壁的风扇壳体区域。设置在轴向通道中的环构件通过多个径向元件连接到环形壁。所述支撑结构部分包括与所述机舱部分成一体的前部部分和包括用于将所述整体结构安装到飞行器的至少一个飞行器安装区域的后部部分。前部包括在环形壁的径向外侧的入口加强区域。当安装在飞机上时，机舱部分和支撑结构部分协作以形成第一负载路径，其可操作以将施加的机舱机动动力直接传递到飞行器而不是通过发动机机芯。

3. 发明授权

US08262050B2 Method and apparatus for mounting and dismounting an aircraft engine 有权
标题翻译：用于安装和拆卸飞机发动机的方法和装置
公开(公告)号：US08262050B2
公开(公告)日：2012-09-11
申请号：US12343848
申请日：2008-12-24
申请人： Mark Linz
发明人： Mark Linz
IPC分类号： F16M13/00
CPC分类号： B66C17/06 , B64F5/50 , B66C1/107 , Y10T29/53
摘要： Apparatus and method for removing an aircraft engine. A method includes mounting a frame assembly in supported connection with a support member of an associated aircraft. The frame assembly includes a frame member, a movable assembly mounted in movable relationship to the frame member, and a plurality of engine winches mounted in supported connection with the movable member. Each engine winch has an associated engine cable operably connected thereto. The movable assembly is movable between forward and rearward positions. The method further includes supporting the weight of at least a portion of an aircraft engine with the engine cables and moving the movable member relative to the frame member to displace the portion of the aircraft engine.
摘要翻译：用于去除飞机发动机的装置和方法。一种方法包括将框架组件与相关飞行器的支撑构件支撑连接地安装。框架组件包括框架构件，与框架构件可移动地安装的可移动组件以及与可动构件支撑连接安装的多个发动机绞盘。每个发动机绞盘具有可操作地连接到其上的相关联的发动机缆索。可移动组件可在前后位置之间移动。该方法还包括用发动机电缆支撑飞机发动机的至少一部分的重量，并相对于框架构件移动可移动构件以使飞行器发动机的该部分移位。

4. 发明申请

US20100155566A1 METHOD AND APPARATUS FOR MOUNTING AND DISMOUNTING AN AIRCRAFT ENGINE 有权
标题翻译：安装和拆卸飞机发动机的方法和装置
公开(公告)号：US20100155566A1
公开(公告)日：2010-06-24
申请号：US12343848
申请日：2008-12-24
申请人： Mark Linz
发明人： Mark Linz
IPC分类号： F16M13/00 , B23P19/04
CPC分类号： B66C17/06 , B64F5/50 , B66C1/107 , Y10T29/53
摘要： Apparatus and method for removing an aircraft engine. A method includes mounting a frame assembly in supported connection with a support member of an associated aircraft. The frame assembly includes a frame member, a movable assembly mounted in movable relationship to the frame member, and a plurality of engine winches mounted in supported connection with the movable member. Each engine winch has an associated engine cable operably connected thereto. The movable assembly is movable between forward and rearward positions. The method further includes supporting the weight of at least a portion of an aircraft engine with the engine cables and moving the movable member relative to the frame member to displace the portion of the aircraft engine.
摘要翻译：用于去除飞机发动机的装置和方法。一种方法包括将框架组件与相关飞行器的支撑构件支撑连接地安装。框架组件包括框架构件，与框架构件可移动地安装的可移动组件以及与可动构件支撑连接安装的多个发动机绞盘。每个发动机绞盘具有可操作地连接到其上的相关联的发动机缆索。可移动组件可在前后位置之间移动。该方法还包括用发动机电缆支撑飞机发动机的至少一部分的重量，并相对于框架构件移动可移动构件以使飞行器发动机的该部分移位。

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