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公开(公告)号：US08360438B2
公开(公告)日：2013-01-29
申请号：US12737705
申请日：2009-08-25
申请人： Eric Wildman , Simon John Parker
发明人： Eric Wildman , Simon John Parker
IPC分类号： F16J15/14
CPC分类号： B64C9/02 , B64C7/00 , F16J15/104
摘要： A seal (500) comprises a seal body (502) having a mounting portion (504), a first leg (506) and a second leg (508), a first stiffening member (514) and a second stiffening member (516) separated by an arcuate shear seal portion (529) in which the motions of the first leg (506) and second leg (508) are relatively constrained by the second stiffening member (516).
摘要翻译： 密封件（500）包括具有安装部分（504），第一腿部（506）和第二腿部（508）的密封体（502），第一加强构件（514）和第二加强构件（516） 通过弓形剪切密封部分（529），其中第一腿部（506）和第二腿部（508）的运动由第二加强部件（516）相对地约束。
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公开(公告)号：US20110031349A1
公开(公告)日：2011-02-10
申请号：US12805615
申请日：2010-08-10
CPC分类号： B64C9/02 , B64C9/16 , B64C9/323 , F16C11/04 , Y02T50/32 , Y10T29/49826 , Y10T403/32951
摘要： A pinned lug joint comprising: a first part comprising two first lugs projecting from a bridge which extends between them; a second part pivotally coupled to the first part, the second part comprising a second lug positioned between the first lugs; and a sealing member, the sealing member being mounted to the first lugs and extending between them to seal an air gap between the second lug and the bridge at least when the second part is in a first position. The pinned lug joint may be used to attach a panel assembly to part of an aircraft.
摘要翻译： 一种被钉扎的凸耳接头，包括：第一部分，包括两个在从它们之间延伸的桥部突出的第一凸耳; 第二部分枢转地联接到第一部分，第二部分包括位于第一凸耳之间的第二凸耳; 密封构件，密封构件安装到第一凸耳并且在它们之间延伸，至少当第二部分处于第一位置时密封第二凸耳和桥之间的空气间隙。 钉扎的接头可用于将面板组件附接到飞行器的一部分。
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公开(公告)号：US06802429B1
公开(公告)日：2004-10-12
申请号：US09648020
申请日：2000-08-25
申请人： Andrew Eric Wildman
发明人： Andrew Eric Wildman
IPC分类号： A47J3610
CPC分类号： A47J36/06 , A47J27/0817
摘要： A steam kettle lid assembly includes an elongated arm movable between an up position and a down position. A steam kettle lid includes central portion non-rotatingly attached to the arm in a manner which permits floating movement of the lid for proper seating on a kettle opening, but which also prevents a condensate rim on a bottom portion of the lid from rotating out of its functional position.
摘要翻译： 蒸汽壶盖组件包括可在上升位置和下降位置之间移动的细长臂。 蒸汽壶盖包括以旋转方式附接到臂的中心部分，其允许盖的浮动运动以适当地坐在壶开口上，但是这也防止盖的底部上的冷凝物边缘从 其功能位置。
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公开(公告)号：US08556214B2
公开(公告)日：2013-10-15
申请号：US12821517
申请日：2010-06-23
申请人： Jon McAlinden , Eric Wildman
发明人： Jon McAlinden , Eric Wildman
摘要： A panel assembly for an aircraft including a panel having an upper aerodynamic surface and a leading edge, and a hinge fitting connected to an underside of the panel, defining a hinge line for the direction of rotation of the panel. The upper surface of the leading edge has an arcuate portion centered about the hinge line, and has an upturned portion forward of the arcuate portion. The panel assembly is pivotally connected to its hinge fitting to the trailing edge of the fixed wing portion and rotatable between a first position wherein the upper surfaces of the fixed wing portion and the panel are substantially flush, and a second position wherein the panel is rotated downwardly from the first position. A seal member attached to the trailing edge of the fixed wing portion, has a lower surface which seals against the upper surface of the panel during its movement.
摘要翻译： 一种用于飞行器的面板组件，包括具有上空气动力学表面和前缘的面板，以及连接到面板下侧的铰链配件，其限定了用于面板旋转方向的铰链线。 前缘的上表面具有以铰链线为中心的弓形部分，并且在弓形部分的前方具有向上的部分。 所述面板组件枢转地连接到其铰链配合到固定翼部分的后缘，并且可在第一位置和第二位置之间旋转，其中固定翼部分和面板的上表面基本齐平，以及第二位置，其中面板旋转 从第一位置向下。 附接到固定翼部分的后缘的密封构件具有在其移动期间密封面板的上表面的下表面。
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公开(公告)号：US09150302B2
公开(公告)日：2015-10-06
申请号：US12805615
申请日：2010-08-10
CPC分类号： B64C9/02 , B64C9/16 , B64C9/323 , F16C11/04 , Y02T50/32 , Y10T29/49826 , Y10T403/32951
摘要： A pinned lug joint comprising: a first part comprising two first lugs projecting from a bridge which extends between them; a second part pivotally coupled to the first part, the second part comprising a second lug positioned between the first lugs; and a sealing member, the sealing member being mounted to the first lugs and extending between them to seal an air gap between the second lug and the bridge at least when the second part is in a first position. The pinned lug joint may be used to attach a panel assembly to part of an aircraft.
摘要翻译： 一种被钉扎的凸耳接头，包括：第一部分，包括两个在从它们之间延伸的桥部突出的第一凸耳; 第二部分枢转地联接到第一部分，第二部分包括位于第一凸耳之间的第二凸耳; 密封构件，密封构件安装到第一凸耳并且在它们之间延伸，至少当第二部分处于第一位置时密封第二凸耳和桥之间的空气间隙。 钉扎的接头可用于将面板组件附接到飞行器的一部分。
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公开(公告)号：US08757543B2
公开(公告)日：2014-06-24
申请号：US12805126
申请日：2010-07-14
申请人： Eric Wildman
发明人： Eric Wildman
IPC分类号： B64C13/00
摘要： A support assembly for guiding a flap on an aircraft wing during deployment of the flap. The assembly includes an arcuate guide track mountable to an aircraft wing and defining a two-dimensional path, a carriage mounted on the guide track so as to slide along the track during flap deployment, a part-spherical bearing, and a shaft having one end attachable to a flap and the opposite end coupled to the carriage via said part-spherical bearing. The shaft is free to pivot relative to the carriage about a center of the part-spherical bearing in all directions, as the carriage slides along the track.
摘要翻译： 用于在翼片展开期间引导飞行器机翼上的翼片的支撑组件。 组件包括可安装到飞机机翼并限定二维路径的弧形导轨，安装在导轨上的滑架，以便在翼片展开期间沿着轨道滑动，部分球形轴承和具有一端的轴 可附接到翼片，并且相对端通过所述部分球形轴承联接到滑架。 当滑架沿着轨道滑动时，轴可以相对于滑架绕着部分球面轴承的中心在所有方向上自由枢转。
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公开(公告)号：US08424801B2
公开(公告)日：2013-04-23
申请号：US13064754
申请日：2011-04-13
IPC分类号： B64C13/28
CPC分类号： B64C9/22 , B64C9/02 , Y02T50/44 , Y10T74/18648 , Y10T74/18992
摘要： A support assembly for deployment and retraction of an aero surface from an aircraft is disclosed. The assembly comprises a guide track, a primary support arm having one end coupled to a carriage mounted on the track such that the primary support arm is rotatable relative to the carriage about multiple axes, and a control arm having one end coupled to the primary support arm and a second end pivotably attachable to a fixed support forming part of the structure of the aircraft. The assembly being configured such that, when the carriage is driven along the guide track, the control arm causes the primary support arm to pivot about said multiple axes to deploy and/or retract an aero surface pivotally attached to an opposite end of the primary support member along an arcuate path.
摘要翻译： 公开了一种用于从飞行器展开和缩回航空表面的支撑组件。 所述组件包括导轨，主支撑臂，其一端联接到安装在所述轨道上的滑架，使得所述主支撑臂可相对于所述滑架绕多个轴线旋转;以及控制臂，其一端联接到所述主支撑件 臂和可枢转地附接到形成飞行器的结构的一部分的固定支撑件的第二端。 组件被构造成使得当滑架沿着导轨被驱动时，控制臂使得主支撑臂围绕所述多个轴线枢转以展开和/或缩回枢转地附接到主支撑件的相对端的航空表面 沿着弧形路径的成员。
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公开(公告)号：US20110253832A1
公开(公告)日：2011-10-20
申请号：US13064754
申请日：2011-04-13
CPC分类号： B64C9/22 , B64C9/02 , Y02T50/44 , Y10T74/18648 , Y10T74/18992
摘要： A support assembly for deployment and retraction of an aero surface from an aircraft is disclosed. The assembly comprises a guide track, a primary support arm having one end coupled to a carriage mounted on the track such that the primary support arm is rotatable relative to the carriage about multiple axes, and a control arm having one end coupled to the primary support arm and a second end pivotably attachable to a fixed support forming part of the structure of the aircraft. The assembly being configured such that, when the carriage is driven along the guide track, the control arm causes the primary support arm to pivot about said multiple axes to deploy and/or retract an aero surface pivotally attached to an opposite end of the primary support member along an arcuate path.
摘要翻译： 公开了一种用于从飞行器展开和缩回航空表面的支撑组件。 所述组件包括导轨，主支撑臂，其一端联接到安装在所述轨道上的滑架，使得所述主支撑臂可相对于所述滑架绕多个轴线旋转;以及控制臂，其一端联接到所述主支撑件 臂和可枢转地附接到形成飞行器的结构的一部分的固定支撑件的第二端。 组件被构造成使得当滑架沿着导轨被驱动时，控制臂使得主支撑臂围绕所述多个轴线枢转以展开和/或缩回枢转地附接到主支撑件的相对端的航空表面 沿着弧形路径的成员。
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公开(公告)号：US20100327121A1
公开(公告)日：2010-12-30
申请号：US12821517
申请日：2010-06-23
申请人： Jon MCALINDEN , Eric WILDMAN
发明人： Jon MCALINDEN , Eric WILDMAN
摘要： A panel assembly for an aircraft including a panel having an upper aerodynamic surface and a leading edge, and a hinge fitting connected to an underside of the panel, defining a hinge line for the direction of rotation of the panel. The upper surface of the leading edge has an arcuate portion centered about the hinge line, and has an upturned portion forward of the arcuate portion. The panel assembly is pivotally connected to its hinge fitting to the trailing edge of the fixed wing portion and rotatable between a first position wherein the upper surfaces of the fixed wing portion and the panel are substantially flush, and a second position wherein the panel is rotated downwardly from the first position. A seal member attached to the trailing edge of the fixed wing portion, has a lower surface which seals against the upper surface of the panel during its movement.
摘要翻译： 一种用于飞行器的面板组件，包括具有上空气动力学表面和前缘的面板，以及连接到面板下侧的铰链配件，其限定了用于面板旋转方向的铰链线。 前缘的上表面具有以铰链线为中心的弓形部分，并且在弓形部分的前方具有向上的部分。 所述面板组件枢转地连接到其铰链配合到固定翼部分的后缘，并且可在第一位置和第二位置之间旋转，其中固定翼部分和面板的上表面基本齐平，以及第二位置，其中面板旋转 从第一位置向下。 附接到固定翼部分的后缘的密封构件具有在其移动期间密封面板的上表面的下表面。
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公开(公告)号：US06409132B1
公开(公告)日：2002-06-25
申请号：US09302650
申请日：1999-04-30
IPC分类号： E04G506
摘要： A bracket for coupling a rail having an upper slot and a lower slot to a shelf edge having an upper groove and a lower groove. The bracket comprises a central body portion, an upper flange extending generally upwardly from the body portion, a lower flange extending generally downwardly from the body portion, and a plate. The plate is received between the upper and the lower flanges such that as the plate is moved toward the body, the plate urges the upper flange and the lower flange into the upper and lower groove, respectively, to couple the bracket to the shelf edge. The bracket further comprises a first upper tang extending generally upwardly from the body portion and a first lower tang extending generally downwardly from the body portion, the upper tang and lower tang being shaped to be received in the upper and lower slot, respectively. At least one of the tangs has at least one tang groove therein to facilitate the attachment of the bracket to the rail.
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