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公开(公告)号：EP2524865B1
公开(公告)日：2015-09-09
申请号：EP12168617.4
申请日：2012-05-21
发明人： Parker, Simon John
CPC分类号： B64C9/20 , B64C9/16 , B64C2009/143
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2.发明公开
公开(公告)号：EP2669187A3
公开(公告)日：2017-04-19
申请号：EP13169031.5
申请日：2013-05-23
发明人： Parker, Simon John
CPC分类号： B64C3/00 , B64C5/08 , B64C23/065 , B64C23/072 , Y02T50/164 , Y10T29/49337
摘要： A method of attaching first 200 and second 300 aerofoil sections to each other is disclosed. The method comprises the steps of: positioning one aerofoil section in an initial assembly orientation with respect to the other aerofoil section so that hinge elements 225, 325 on each aerofoil section are in alignment with each other, inserting a hinge shaft 450 through said aligned hinge elements to initially couple the aerofoil sections together whilst the aerofoil sections are in their initial assembly orientation; and rotating one aerofoil section relative to the other aerofoil section about a compound angle defined by the hinge shaft into a second orientation in which the aerofoil sections are in their final, assembled orientation relative to each other. An aerofoil assembly 100 is also disclosed.
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公开(公告)号：EP2524865A1
公开(公告)日：2012-11-21
申请号：EP12168617.4
申请日：2012-05-21
发明人： Parker, Simon John
CPC分类号： B64C9/20 , B64C9/16 , B64C2009/143
摘要： An aircraft wing assembly, comprising: a fixed wing portion; a first flight control surface; a first actuator operatively coupled to the first flight control surface for moving the first flight control surface with respect to the fixed wing portion; a second flight control surface disposed adjacent the first flight control surface; a second actuator operatively coupled to the second flight control surface for moving the second flight control surface with respect to the fixed wing portion; a control system operatively coupled to the first and second actuators for controlling movement of the first and second flight control surfaces; and a third actuator selectively engaged with the second flight control surface for engaging and moving the second flight control surface out of a path of movement of the first flight control surface only in the event of a failure in the second actuator or its control, so as to avoid direct contact between the first and second flight control surfaces. Also, a method of operating an aircraft wing assembly.
摘要翻译： 一种飞机机翼组件，包括：固定翼部分; 第一个飞行控制面; 第一致动器，其可操作地联接到所述第一飞行控制表面，用于相对于所述固定翼部分移动所述第一飞行控制表面; 设置在第一飞行控制表面附近的第二飞行控制表面; 第二致动器，其可操作地联接到所述第二飞行控制表面，用于相对于所述固定翼部分移动所述第二飞行控制表面; 控制系统，其可操作地联接到所述第一和第二致动器，用于控制所述第一和第二飞行控制表面的运动; 以及第三致动器，其选择性地与所述第二飞行控制表面接合，用于仅在所述第二致动器或其控制中发生故障的情况下将所述第二飞行控制表面从所述第一飞行控制表面的移动路径接合和移动，从而 以避免第一和第二飞行控制表面之间的直接接触。 另外，操作飞机机翼组件的方法。
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4.发明公开A hinge assembly for rotatably mounting a control surface on an aircraft 审中-公开一种用于将控制表面可旋转地安装在飞机上的铰链组件
公开(公告)号：EP2669188A3
公开(公告)日：2017-12-27
申请号：EP13169022.4
申请日：2013-05-23
发明人： Parker, Simon John
CPC分类号： B64C9/02 , B64C9/34 , B64C2009/005
摘要： A hinge assembly (4) for rotatably mounting a control surface (3) on an aircraft comprising an actuating shaft (9), a support element (16) configured to mount the actuating shaft to a first component of an aircraft and a hinge element (17) configured to mount the actuating shaft (9) to a second component of an aircraft, wherein the actuating shaft (9) is slidabty mounted to the support element (16) and configured to slide along its longitudinal axis relative to the support element (16), and the hinge element (17) engages with the actuating shaft (9) so that the actuating shaft and the hinge element are urged to rotate relative to each other about the longitudinal axis of the actuating shaft when the actuating shaft is urged to slide along its longitudinal axis, such that one of said first and second components is urged to rotate relative to the other said component about the longitudinal axis.
摘要翻译： 一种用于在飞机上可旋转地安装控制表面（3）的铰链组件（4），所述飞行器包括致动轴（9），构造成将致动轴安装到飞机的第一部件的支撑元件（16） 所述致动轴（9）可滑动地安装到所述支撑元件（16）并且构造成沿着其纵向轴线相对于所述支撑元件（16）滑动，其中所述致动轴（9） 并且铰链元件（17）与致动轴（9）接合，使得致动轴和铰链元件在致动轴被推动时围绕致动轴的纵向轴线彼此相对旋转 沿着它的纵向轴线滑动，使得所述第一和第二部件中的一个被推动相对于另一个所述部件围绕纵向轴线旋转。
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公开(公告)号：EP2669191A2
公开(公告)日：2013-12-04
申请号：EP13169028.1
申请日：2013-05-23
发明人： Parker, Simon John
IPC分类号： B64C9/22
摘要： A slat support assembly 20 is disclosed. It comprises a slat support arm 22 which is movable to deploy a slat from a leading edge of an aircraft wing about an axis of rotation of the arm and a slat mount 27, 28 on a slat which is coupled to one end of said slat support arm by a joint 29, 32, 33. The joint is configured to allow the slat mount to slide in a direction of the axis of rotation of the arm.
摘要翻译： 公开了一种板条支撑组件20。 它包括板条支撑臂22，其可移动以从机翼的前缘围绕臂的旋转轴线部署板条，并且在板条上连接有板条安装件27,28，板条安装件27,28联接到所述板条支撑件的一端 该接头被构造成允许板条安装件沿着臂的旋转轴线的方向滑动。
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6.发明公开A hinge assembly for rotatably mounting a control surface on an aircraft 审中-公开Scharnieranordnung zur drehbaren蒙太奇einerSteuerflächean ein Flugzeug
公开(公告)号：EP2669188A2
公开(公告)日：2013-12-04
申请号：EP13169022.4
申请日：2013-05-23
发明人： Parker, Simon John
CPC分类号： B64C9/02 , B64C9/34 , B64C2009/005
摘要： A hinge assembly (4) for rotatably mounting a control surface (3) on an aircraft comprising an actuating shaft (9), a support element (16) configured to mount the actuating shaft to a first component of an aircraft and a hinge element (17) configured to mount the actuating shaft (9) to a second component of an aircraft, wherein the actuating shaft (9) is slidabty mounted to the support element (16) and configured to slide along its longitudinal axis relative to the support element (16), and the hinge element (17) engages with the actuating shaft (9) so that the actuating shaft and the hinge element are urged to rotate relative to each other about the longitudinal axis of the actuating shaft when the actuating shaft is urged to slide along its longitudinal axis, such that one of said first and second components is urged to rotate relative to the other said component about the longitudinal axis.
摘要翻译： 一种用于将飞行器上的控制表面（3）可旋转地安装在飞行器上的铰链组件（4），包括致动轴（9），构造成将致动轴安装到飞行器的第一部件上的支撑元件（16） 17），其构造成将所述致动轴（9）安装到飞行器的第二部件，其中所述致动轴（9）可滑动地安装到所述支撑元件（16）并且构造成沿着其纵向轴线相对于所述支撑元件 16），并且铰链元件（17）与致动轴（9）接合，使得致动轴和铰链元件在致动轴被推动时相对于致动轴的纵向轴线相对于彼此旋转 沿着其纵向轴线滑动，使得所述第一和第二部件中的一个被推动相对于另一个所述部件围绕纵向轴线旋转。
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公开(公告)号：EP2669191A3
公开(公告)日：2017-04-19
申请号：EP13169028.1
申请日：2013-05-23
发明人： Parker, Simon John
摘要： A slat support assembly 20 is disclosed. It comprises a slat support arm 22 which is movable to deploy a slat from a leading edge of an aircraft wing about an axis of rotation of the arm and a slat mount 27, 28 on a slat which is coupled to one end of said slat support arm by a joint 29, 32, 33. The joint is configured to allow the slat mount to slide in a direction of the axis of rotation of the arm.
摘要翻译： 公开了一种板条支撑组件20。 它包括一个板条支承臂22，该板条支承臂22可移动以从飞机机翼的前缘围绕臂的旋转轴线展开板条，并且板条上的板条安装件27,28连接到所述板条支承件的一端 通过接头29,32,33连接臂。接头构造成允许板条安装件沿着臂的旋转轴线的方向滑动。
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9.发明公开Method of coupling aerofoil surface structures and an aerofoil assembly 审中-公开Verfahren zur Kopplung vonTragflächenstrukturenund eineTragflächenbaugruppe
公开(公告)号：EP2669187A2
公开(公告)日：2013-12-04
申请号：EP13169031.5
申请日：2013-05-23
发明人： Parker, Simon John
CPC分类号： B64C3/00 , B64C5/08 , B64C23/065 , B64C23/072 , Y02T50/164 , Y10T29/49337
摘要： A method of attaching first 200 and second 300 aerofoil sections to each other is disclosed. The method comprises the steps of: positioning one aerofoil section in an initial assembly orientation with respect to the other aerofoil section so that hinge elements 225, 325 on each aerofoil section are in alignment with each other, inserting a hinge shaft 450 through said aligned hinge elements to initially couple the aerofoil sections together whilst the aerofoil sections are in their initial assembly orientation; and rotating one aerofoil section relative to the other aerofoil section about a compound angle defined by the hinge shaft into a second orientation in which the aerofoil sections are in their final, assembled orientation relative to each other. An aerofoil assembly 100 is also disclosed.
摘要翻译： 公开了将第一个200和第二个机翼部分彼此连接的方法。 该方法包括以下步骤：将一个机翼部分相对于另一机翼部分以初始组装方向定位，使得每个机翼部分上的铰链元件225,325彼此对准，将铰链轴450穿过所述对准的铰链 元件最初将机翼部分连接在一起，同时机翼部分处于其初始组装方向; 并且围绕由铰链轴限定的复合角度将一个机翼部分相对于另一个机翼部分旋转成第二取向，其中机翼部分相对于彼此处于其最终的组装取向。 还公开了机翼组件100。
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