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公开(公告)号：US08245976B2
公开(公告)日：2012-08-21
申请号：US12356029
申请日：2009-01-19
IPC分类号： B64C1/14
CPC分类号： B64C21/02 , B64C21/08 , B64C2230/20 , B64C2230/22 , B64D2241/00 , Y02T50/166
摘要： A door assembly has a first door integrated with a second door. The first door has a first door cowl. The second door is pivotably mounted to the first door and has a second door cowl forming at least a portion of the first door cowl. The door assembly includes at least one actuator coupled to the first and second doors. Each one of the first and second doors is pivotable between open and closed positions and defines an opening when moved to the open position. The openings of the first and second doors face in opposite directions. The actuator is operative to pivotably move at least one of the first and second doors between the open and closed positions.
摘要翻译： 门组件具有与第二门一体的第一门。 第一扇门有一个第一扇门。 第二门可枢转地安装到第一门，并且具有形成第一门罩的至少一部分的第二门罩。 门组件包括耦合到第一和第二门的至少一个致动器。 第一和第二门中的每一个可在打开位置和关闭位置之间枢转，并且当移动到打开位置时限定开口。 第一和第二门的开口面向相反的方向。 致动器可操作以在打开位置和关闭位置之间枢转地移动第一和第二门中的至少一个。
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公开(公告)号：US08484894B2
公开(公告)日：2013-07-16
申请号：US13551474
申请日：2012-07-17
IPC分类号： E05D15/50
CPC分类号： B64C21/02 , B64C21/08 , B64C2230/20 , B64C2230/22 , B64D2241/00 , Y02T50/166
摘要： A method of operating a door assembly may include pivoting a first door about a first pivot axis from a closed position to an open position such that the first door acts as an inlet. The method may further include pivoting the first door to the closed position, and pivoting a second door about a second pivot axis from a closed position to an open position when the first door is in the closed position such that the second door acts as an outlet facing in a direction opposite the first door. The method may additionally include pivoting the second pivot axis about the first pivot axis when pivoting the second door, the second door being of a smaller size than the first door and forming at least a portion of the first door.
摘要翻译： 操作门组件的方法可以包括将第一门围绕第一枢转轴线从关闭位置枢转到打开位置，使得第一门用作入口。 该方法还可以包括将第一门枢转到关闭位置，并且当第一门处于关闭位置时使第二门围绕第二枢转轴线从关闭位置枢转到打开位置，使得第二门作为出口 面向与第一扇门相对的方向。 该方法可以另外包括在枢转第二门时枢转第二枢轴围绕第一枢转轴线，第二门的尺寸比第一门小，并形成第一门的至少一部分。
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公开(公告)号：US20120280088A1
公开(公告)日：2012-11-08
申请号：US13551474
申请日：2012-07-17
CPC分类号： B64C21/02 , B64C21/08 , B64C2230/20 , B64C2230/22 , B64D2241/00 , Y02T50/166
摘要： A method of operating a door assembly may include pivoting a first door about a first pivot axis from a closed position to an open position such that the first door acts as an inlet. The method may further include pivoting the first door to the closed position, and pivoting a second door about a second pivot axis from a closed position to an open position when the first door is in the closed position such that the second door acts as an outlet facing in a direction opposite the first door. The method may additionally include pivoting the second pivot axis about the first pivot axis when pivoting the second door, the second door being of a smaller size than the first door and forming at least a portion of the first door.
摘要翻译： 操作门组件的方法可以包括将第一门围绕第一枢转轴线从关闭位置枢转到打开位置，使得第一门用作入口。 该方法还可以包括将第一门枢转到关闭位置，并且当第一门处于关闭位置时使第二门围绕第二枢转轴线从关闭位置枢转到打开位置，使得第二门作为出口 面向与第一扇门相对的方向。 该方法可以另外包括在枢转第二门时枢转第二枢轴围绕第一枢转轴线，第二门的尺寸比第一门小，并形成第一门的至少一部分。
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公开(公告)号：US20100181435A1
公开(公告)日：2010-07-22
申请号：US12356029
申请日：2009-01-19
CPC分类号： B64C21/02 , B64C21/08 , B64C2230/20 , B64C2230/22 , B64D2241/00 , Y02T50/166
摘要： A door assembly has a first door integrated with a second door. The first door has a first door cowl. The second door is pivotably mounted to the first door and has a second door cowl forming at least a portion of the first door cowl. The door assembly includes at least one actuator coupled to the first and second doors. Each one of the first and second doors is pivotable between open and closed positions and defines an opening when moved to the open position. The openings of the first and second doors face in opposite directions. The actuator is operative to pivotably move at least one of the first and second doors between the open and closed positions.
摘要翻译： 门组件具有与第二门一体的第一门。 第一扇门有一个第一扇门。 第二门可枢转地安装到第一门，并且具有形成第一门罩的至少一部分的第二门罩。 门组件包括耦合到第一和第二门的至少一个致动器。 第一和第二门中的每一个可在打开位置和关闭位置之间枢转，并且当移动到打开位置时限定开口。 第一和第二门的开口面向相反的方向。 致动器可操作以在打开位置和关闭位置之间枢转地移动第一和第二门中的至少一个。
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公开(公告)号：US20130206917A1
公开(公告)日：2013-08-15
申请号：US13370314
申请日：2012-02-10
摘要： A system and method to enable natural laminar flow over a fluid-dynamic body using a variable camber Krueger flap is disclosed. A sequence of flap positions is deployed where the variable camber Krueger flap is below and aft of the wing leading edge before reaching a configured takeoff and landing position. The variable camber Krueger flap is positioned in a high position relative to a wing leading edge when the variable camber Krueger flap is fully deployed.
摘要翻译： 公开了一种使用可变外倾角Krueger瓣使流体动力体上的自然层流流动的系统和方法。 部署一系列的襟翼位置，其中可变弧度Krueger挡板在达到配置的起飞和着陆位置之前在机翼前缘的下方和后方。 当可变外倾角Krueger挡板完全展开时，可变弯度Krueger挡板相对于机翼前缘定位在较高的位置。
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6.发明申请AIRCRAFT FLAP MECHANISM HAVING COMPACT LARGE FOWLER MOTION PROVIDING MULTIPLE CRUISE POSITIONS 有权具有提供多个巡航位置的紧凑型大型运动的飞机翼片机构公开(公告)号：US20130075537A1
公开(公告)日：2013-03-28
申请号：US13242296
申请日：2011-09-23
摘要： A trailing edge flap mechanism incorporates a support beam, a flap carrier beam supporting an aerodynamic flap, a first link interconnecting a first and second rotation points and a second link interconnecting third and fourth rotation points. The support beam has a ground connection on a first fixed axis of rotation. A connecting link has a ground connection on a second fixed axis of rotation and is connected to the first link intermediate the first and second rotation points. An actuator is connected with a drive link pivotally engaged to the first link for initial forward and aft movement of a nose profile of the Fowler flap substantially parallel to the wing lower surface with extending aft movement providing a rapidly changing angle of the flap with respect to the wing upper surface.
摘要翻译： 后缘翼片机构包括支撑梁，支撑气动翼片的翼片承载梁，互连第一和第二旋转点的第一连杆和互连第三和第四旋转点的第二连杆。 支撑梁在第一固定旋转轴线上具有接地连接。 连接链路在第二固定旋转轴线上具有接地连接，并且在第一和第二旋转点之间连接到第一连杆。 致动器与驱动连杆连接，该驱动连杆枢转地接合到第一连杆，用于使Fowler翼片的鼻部轮廓基本上平行于机翼下表面的初始向前和向后运动，具有延伸的后部运动，从而提供相对于翼片的快速变化的角度 机翼上表面。
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7.发明授权公开(公告)号：US07815981B2
公开(公告)日：2010-10-19
申请号：US11384399
申请日：2006-03-21
申请人： Hiroshi Iwanaga , Seiya Sakurai
发明人： Hiroshi Iwanaga , Seiya Sakurai
IPC分类号： C09K19/00
CPC分类号： H01L51/5253 , Y10T428/10 , Y10T428/1023 , Y10T428/1086 , Y10T428/2495 , Y10T428/24967 , Y10T428/2955 , Y10T428/3154 , Y10T428/31786
摘要： A gas barrier film comprising a gas barrier laminate on a substrate film, wherein the gas barrier laminate comprises at least one three-layer unit consisting of a silicon nitride layer, a silicon oxynitride layer adjacent to the silicon nitride layer, and a silicon nitride layer adjacent to the silicon oxynitride layer. The gas barrier film has excellent transparency and gas barrier property.
摘要翻译： 一种阻气性膜，其在基材膜上具有阻气性叠层体，其特征在于，所述阻气性层压体包含至少一层由氮化硅层，与氮化硅层相邻的氮氧化硅层和氮化硅层构成的三层单元， 邻近氮氧化硅层。 阻气膜具有优异的透明性和阻气性。
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8.发明授权Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods 有权飞机后缘装置，包括具有非平行运动路径的装置，以及相关方法公开(公告)号：US07744040B2
公开(公告)日：2010-06-29
申请号：US12264831
申请日：2008-11-04
申请人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
发明人： Douglas S. Lacy , Kevin W. Beyer , Stephen T. Brown , Paul W. Dees , Neal V. Huynh , Jan A. Kordel , Clayton A. Prow , Seiya Sakurai
IPC分类号： B64C3/50
CPC分类号： B64C9/16 , B64C2009/143
摘要： Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods are disclosed. A device in accordance with one embodiment includes a wing and an inboard trailing edge device coupled to the wing and movable relative to the wing between a first stowed position and a first deployed position along a first motion path. An outboard trailing edge device can be coupled to the wing outboard of the inboard trailing edge device, and can be movable relative to the wing along a second motion path that is non-parallel to the first motion path. An intermediate trailing edge device can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path that is non-parallel to both the first and second motion paths. Each of the trailing edge devices can open a gap relative to the wing when moved to their respective deployed positions.
摘要翻译： 公开了包括具有非平行运动路径的装置和相关方法的飞行器后缘装置。 根据一个实施例的装置包括机翼和内侧后缘装置，其联接到机翼并且可沿着第一运动路径在第一收起位置和第一展开位置之间相对于机翼移动。 外侧后缘装置可以联接到内侧后缘装置的翼外侧，并且可以沿着不平行于第一运动路径的第二运动路径相对于机翼移动。 中间后缘装置可以联接在内侧和后侧后缘装置之间，并且可以沿着不平行于第一和第二运动路径的第三运动路径移动。 每个后缘装置可以在移动到它们各自的展开位置时相对于机翼打开间隙。
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9.发明申请Link Mechanisms, Including Stephenson II Link Mechanisms for Multi-Position Flaps and Associated Systems and Methods 有权链接机制，包括Stephenson II链接机制的多位置襟翼和相关系统和方法公开(公告)号：US20100140414A1
公开(公告)日：2010-06-10
申请号：US12331193
申请日：2008-12-09
申请人： Kevin W. Beyer , Seiya Sakurai
发明人： Kevin W. Beyer , Seiya Sakurai
摘要： Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes an airfoil having an external flow surface with an upper portion and a lower portion, and with the airfoil forming a base link. The system further includes a six-bar linkage coupled to the airfoil and having a Stephenson II configuration, including a binary second link pivotably connected to the airfoil, a ternary third link pivotably connected to the second link, a binary fourth link pivotably connected to the third link, a ternary fifth link pivotably connected to the airfoil and the fourth link, and a binary sixth link pivotably connected to the third link and the fifth link. The system can further include a deployable leading edge panel carried by the linkage, with the leading edge panel being movable via the linkage between a stowed position and at least one deployed position.
摘要翻译： 公开了包括用于多位置襟翼的斯蒂芬森II链接机构和相关系统和方法的链接机构。 根据特定实施例的系统包括具有外部流动表面的机翼，其具有上部和下部，并且翼型形成基部连杆。 该系统还包括联接到翼型件并具有斯蒂芬森II构造的六杆连杆，其包括可枢转地连接到翼型件的二元第二连杆，可枢转地连接到第二连杆的三元第三连杆，可枢转地连接到第二连杆的二进制第四连杆 第三连杆，可枢转地连接到翼型件和第四连杆的三元第五连杆，以及可枢转地连接到第三连杆和第五连杆的二元第六连杆。 所述系统还可以包括由所述联动装置承载的可展开的前缘面板，所述前缘面板可通过所述连接件在收起位置与至少一个展开位置之间移动。
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10.发明授权Seal assemblies for use with drooped spoilers and other control surfaces on aircraft 有权用于飞机上的下垂扰流板和其他控制面的密封组件公开(公告)号：US07611099B2
公开(公告)日：2009-11-03
申请号：US11220446
申请日：2005-09-07
申请人： Jan A. Kordel , Seiya Sakurai , Bret A. Bowers , Christopher G. Glassmoyer , Darren B. Williams
发明人： Jan A. Kordel , Seiya Sakurai , Bret A. Bowers , Christopher G. Glassmoyer , Darren B. Williams
IPC分类号： B64C3/50
CPC分类号： B64C7/00 , B64C9/18 , B64C2009/143 , Y02T50/32 , Y10S277/916
摘要： Aerodynamic seals for use with control surfaces on aircraft are described herein. In one embodiment, a seal assembly for use with an aircraft includes a first seal member and a second seal member. The first seal member has a first proximal portion configured to be attached to a fixed airfoil portion of the aircraft, and a first distal portion configured to extend outwardly from the fixed airfoil portion toward a movable control surface. The second seal member has a second proximal portion configured to be attached to the movable control surface, and a second distal portion configured to extend outwardly from the control surface toward the fixed airfoil portion. In this embodiment, the second distal portion is further configured to movably contact the first distal portion to at least partially seal the gap between the fixed airfoil portion and the movable control surface as the control surface moves relative to the fixed airfoil portion.
摘要翻译： 这里描述了用于与飞机上的控制表面一起使用的气动密封件。 在一个实施例中，与飞行器一起使用的密封组件包括第一密封构件和第二密封构件。 第一密封构件具有构造成附接到飞机的固定翼型部分的第一近端部分，以及构造成从固定翼型部分朝向可移动控制表面向外延伸的第一远端部分。 第二密封构件具有构造成附接到可移动控制表面的第二近端部分，以及被配置为从控制表面朝向固定翼型部分向外延伸的第二远端部分。 在该实施例中，第二远端部分进一步构造成当控制表面相对于固定翼型部分移动时，可移动地接触第一远端部分以至少部分地密封固定翼型部分和可移动控制表面之间的间隙。
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