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公开(公告)号：US07243881B2
公开(公告)日：2007-07-17
申请号：US10860438
申请日：2004-06-03
申请人： Seiya Sakurai , Stephen J. Fox , Kevin W. Beyer , Douglas S. Lacy , Paul L. Johnson , Stephen L. Wells , Jack S. Noble , Paul T. Meredith , Neal V. Huynh , Russell R. Christianson , Paul M. Vijgen , Michael F. Fitzpatrick , Clayton A. Prow , Edward W. Gronenthal
发明人： Seiya Sakurai , Stephen J. Fox , Kevin W. Beyer , Douglas S. Lacy , Paul L. Johnson , Stephen L. Wells , Jack S. Noble , Paul T. Meredith , Neal V. Huynh , Russell R. Christianson , Paul M. Vijgen , Michael F. Fitzpatrick , Clayton A. Prow , Edward W. Gronenthal
IPC分类号： B64C9/22
摘要： Trailing edge devices configured to carry out multiple functions, and associated methods of use and manufacture are disclosed. An external fluid flow body (e.g., an airfoil) configured in accordance with an embodiment of the invention includes a first portion and a second portion, at least a part of the second portion being positioned aft of the first portion, with the second portion being movable relative to the first portion between a neutral position, a plurality of upward positions, and a plurality of downward positions. A guide structure can be coupled between the first and second portions, and an actuator can be operatively coupled between the first and second portions to move the second portion relative to the first portion. In one embodiment, a flexible surface can track the motion of the second portion and can expose a gap at some positions. In another embodiment, a controller can be coupled to the actuator and can be configured to direct the actuator to move the second portion to a high lift setting, a high drag setting, a roll setting, and a trim setting. In yet another embodiment, trailing edge devices on an airfoil can have scaled, mechanically similar guide structures.
摘要翻译： 被配置为执行多个功能的后端设备以及相关联的使用和制造方法被公开。 根据本发明的实施例配置的外部流体流动体（例如，翼型）包括第一部分和第二部分，第二部分的至少一部分位于第一部分的后部，第二部分是 相对于第一部分在中立位置，多个向上位置和多个向下位置之间移动。 引导结构可以联接在第一和第二部分之间，并且致动器可以可操作地联接在第一和第二部分之间，以相对于第一部分移动第二部分。 在一个实施例中，柔性表面可以跟踪第二部分的运动并且可以在某些位置暴露间隙。 在另一个实施例中，控制器可以联接到致动器，并且可以被配置为引导致动器将第二部分移动到高提升设置，高阻力设置，滚转设置和修剪设置。 在另一个实施例中，翼型件上的后缘装置可以具有缩放的机械上相似的导向结构。
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2.发明授权Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface 有权用具有柔性流动面的有间隙后缘装置控制气流的方法和装置公开(公告)号：US07258308B2
公开(公告)日：2007-08-21
申请号：US10188988
申请日：2002-07-02
申请人： Kevin W. Beyer , Stephen J. Fox , Douglas S. Lacy , Paul T. Meredith , Clayton A. Prow , Seiya Sakurai , Stephen L. Wells
发明人： Kevin W. Beyer , Stephen J. Fox , Douglas S. Lacy , Paul T. Meredith , Clayton A. Prow , Seiya Sakurai , Stephen L. Wells
IPC分类号： B64C9/16
摘要： A method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. The airfoil can include a first portion having a first leading edge, a first flow surface, and a second flow surface facing opposite from the first flow surface. The airfoil can further include a second portion having a second leading edge and a trailing edge, with at least part of the second portion being positioned aft of the first portion. The second portion is moveable relative to the first portion between a first position and a second position, with the second leading edge separated from at least part of the first portion by an airflow gap when the second portion is in the second position. The second portion includes a flexible flow surface that has a first shape when the second portion is in the first position, and has a second shape different than the first shape when the second portion is in the second position.
摘要翻译： 一种用具有柔性流动面的有间隙后缘装置控制气流的方法和装置。 翼型件可以包括具有第一前缘，第一流动表面和与第一流动表面相对的第二流动表面的第一部分。 翼型件还可以包括具有第二前缘和后缘的第二部分，其中第二部分的至少一部分位于第一部分的后部。 第二部分可相对于第一位置和第二位置之间的第一部分移动，当第二部分处于第二位置时，第二前缘与第一部分的至少一部分分开一个气流间隙。 第二部分包括柔性流动表面，当第二部分处于第一位置时具有第一形状，并且当第二部分处于第二位置时具有与第一形状不同的第二形状。
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3.发明授权Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface 有权用于具有柔性流动表面的前缘装置控制气流的方法和装置公开(公告)号：US06796534B2
公开(公告)日：2004-09-28
申请号：US10238130
申请日：2002-09-10
申请人： Kevin W. Beyer , Stephen J. Fox , Douglas S. Lacy , Seiya Sakurai
发明人： Kevin W. Beyer , Stephen J. Fox , Douglas S. Lacy , Seiya Sakurai
IPC分类号： B64C350
CPC分类号： B64C3/48
摘要： Methods and apparatuses for controlling airflow with a leading edge device having a flexible flow surface. In one embodiment, the airfoil includes a first portion having a first flow surface and a second flow surface facing opposite from the first flow surface. The second portion of the airfoil has a leading edge and is movably coupled to the first position. The second portion can move between a first position and a second position offset from the first position by an angle of from about 45° to about 90° or more. The second portion includes a flexible flow surface having a first shape when the second portion is in the first position and a second shape different than the first shape when the second portion is in the second position. A guide structure can be coupled between the first portion and the second portion. In another embodiment, the airfoil can have inbound and outbound leading edge portions with an inbound guide structure having a first mechanical arrangement and an outbound guide structure having a second mechanical arrangement different than the first.
摘要翻译： 用于具有柔性流动表面的前缘装置控制气流的方法和装置。 在一个实施例中，翼型件包括具有第一流动表面的第一部分和与第一流动表面相对的第二流动表面。 翼型件的第二部分具有前缘并且可移动地联接到第一位置。 第二部分可以在从第一位置偏移约45°至约90°或更大的角度的第一位置和第二位置之间移动。 第二部分包括当第二部分处于第一位置时具有第一形状的柔性流动表面和当第二部分处于第二位置时与第一形状不同的第二形状。 引导结构可以联接在第一部分和第二部分之间。 在另一个实施例中，翼型件可以具有入口和出口的前缘部分，其具有具有第一机械装置的入站引导结构和具有不同于第一机构的第二机械装置的出站引导结构。
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4.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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5.发明申请Aircraft Trailing Edge Devices, Including Devices With Non-Parallel Motion Paths, and Associated Methods 有权飞机后端设备，包括具有非并行运动路径的设备以及相关方法公开(公告)号：US20090146017A1
公开(公告)日：2009-06-11
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
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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6.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：US07475854B2
公开(公告)日：2009-01-13
申请号：US11284247
申请日：2005-11-21
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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7.发明授权Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods 有权飞机后缘装置，包括具有向前定位的铰链线的装置以及相关联的方法公开(公告)号：US08567726B2
公开(公告)日：2013-10-29
申请号：US13252011
申请日：2011-10-03
申请人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
发明人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
IPC分类号： B64C9/18
摘要： Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
摘要翻译： 公开了包括具有向前定位的铰链线的装置的飞机后缘装置和相关方法。 根据本发明的一个实施例的飞行器系统包括联接到机翼的翼和后缘装置。 后缘装置可以在收起位置和展开位置之间相对于翼移动，后缘装置具有前缘，后缘，上表面和下表面。 当后缘装置处于收起位置时，上表面可以与翼的交点。 后缘装置相对于机翼的运动可以包括围绕位于交叉点前方的铰链线的旋转运动，并且当机翼的后缘和后缘装置的前缘之间可以定位间隙时 后缘装置处于展开位置。
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8.发明申请Aircraft Trailing Edge Devices, Including Devices Having Forwardly Positioned Hinge Lines, and Associated Methods 有权飞机后端设备，包括具有向前定位的铰链线的设备以及相关方法公开(公告)号：US20120018588A1
公开(公告)日：2012-01-26
申请号：US13252011
申请日：2011-10-03
申请人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
发明人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
摘要： Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
摘要翻译： 公开了包括具有向前定位的铰链线的装置的飞机后缘装置和相关方法。 根据本发明的一个实施例的飞行器系统包括联接到机翼的翼和后缘装置。 后缘装置可以在收起位置和展开位置之间相对于翼移动，后缘装置具有前缘，后缘，上表面和下表面。 当后缘装置处于收起位置时，上表面可以与翼的交点。 后缘装置相对于机翼的运动可以包括围绕位于交叉点前方的铰链线的旋转运动，并且当机翼的后缘和后缘装置的前缘之间可以定位间隙时 后缘装置处于展开位置。
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9.发明授权Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods 有权飞机后缘装置，包括具有向前定位的铰链线的装置以及相关联的方法公开(公告)号：US08038103B2
公开(公告)日：2011-10-18
申请号：US12497493
申请日：2009-07-02
申请人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
发明人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
IPC分类号： B64C9/18
摘要： Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
摘要翻译： 公开了包括具有向前定位的铰链线的装置的飞机后缘装置和相关方法。 根据本发明的一个实施例的飞行器系统包括联接到机翼的翼和后缘装置。 后缘装置可以在收起位置和展开位置之间相对于翼移动，后缘装置具有前缘，后缘，上表面和下表面。 当后缘装置处于收起位置时，上表面可以与翼的交点。 后缘装置相对于机翼的运动可以包括围绕位于交叉点前方的铰链线的旋转运动，并且当机翼的后缘和后缘装置的前缘之间可以定位间隙 后缘装置处于展开位置。
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10.发明授权Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods 有权飞机后缘装置，包括具有向前定位的铰链线的装置以及相关联的方法公开(公告)号：US07708231B2
公开(公告)日：2010-05-04
申请号：US11284113
申请日：2005-11-21
申请人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
发明人： Douglas S. Lacy , Jan A. Kordel , John V. Dovey , Michael A. Balzer , Seiya Sakurai , Neal V. Huynh
IPC分类号： B64C9/18
摘要： Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed. An aircraft system in accordance with one embodiment of the invention includes a wing and a trailing edge device coupled to the wing. The trailing edge device can be movable relative to the wing between a stowed position and a deployed position, with the trailing edge device having a leading edge, a trailing edge, an upper surface, and a lower surface. The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position. The motion of the trailing edge device relative to the wing can include rotational motion about a hinge line positioned forward of the intersection point, and a gap can be positioned between the trailing edge of the wing and the leading edge of the trailing edge device when the trailing edge device is in the deployed position.
摘要翻译： 公开了包括具有向前定位的铰链线的装置的飞机后缘装置和相关方法。 根据本发明的一个实施例的飞行器系统包括联接到机翼的翼和后缘装置。 后缘装置可以在收起位置和展开位置之间相对于翼移动，后缘装置具有前缘，后缘，上表面和下表面。 当后缘装置处于收起位置时，上表面可以与翼的交点。 后缘装置相对于机翼的运动可以包括围绕位于交叉点前方的铰链线的旋转运动，并且当机翼的后缘和后缘装置的前缘之间可以定位间隙 后缘装置处于展开位置。
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