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    Aircraft with multipurpose lower decks and associated methods of manufacture
    1.
    发明授权
    Aircraft with multipurpose lower decks and associated methods of manufacture 有权
    具有多用途下甲板和相关制造方法的飞机

    公开(公告)号：US06772977B2

    公开(公告)日：2004-08-10

    申请号：US10278717

    申请日：2002-10-22

    申请人： Paul W. Dees ,  Mithra M.K.V. Sankrithi

    发明人： Paul W. Dees ,  Mithra M.K.V. Sankrithi

    IPC分类号： B64D1100

    CPC分类号： B64C1/0009 ,  B64C1/26 ,  B64C25/04 ,  B64C25/10 ,  B64C2001/0027 ,  B64C2001/0045 ,  B64D9/003 ,  B64D11/00 ,  B64D27/18 ,  B64D37/04 ,  Y02T50/12

    摘要： Transport aircraft, such as a transonic transport aircraft, having fuselages with multipurpose lower decks. In one embodiment, the fuselage is an “area-ruled” fuselage having a first fuselage portion, a second fuselage portion positioned aft of the first fuselage portion and at least proximate to a wing, and a third fuselage portion positioned aft of the second fuselage portion. The first fuselage portion can have a first dimension, the second fuselage portion can have a second dimension less than the first dimension, and the third fuselage portion can have a third dimension greater than the second dimension. The fuselage can further include an upper deck extending at least within the first and second fuselage portions, and a lower deck extending within the first fuselage portion. The upper deck can include a first passenger portion and the lower deck can include a second passenger portion, a cargo portion, or a second passenger portion and a cargo portion.

    摘要翻译： 运输飞机，如跨音速运输机，具有多用途下甲板机身。 在一个实施例中，机身是具有第一机身部分的第一机身部分，位于第一机身部分后部并且至少靠近机翼的第二机身部分的“区域划分”机身，以及位于第二机身后方的第三机身部分 一部分。 第一机身部分可具有第一尺寸，第二机身部分可具有小于第一尺寸的第二尺寸，并且第三机身部分可具有大于第二尺寸的第三尺寸。 机身还可包括至少在第一和第二机身部分内延伸的上甲板，以及在第一机身部分内延伸的下甲板。 上甲板可以包括第一乘客部分，下甲板可以包括第二乘客部分，货物部分或第二乘客部分和货物部分。

    Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
    2.
    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。

    Wing flap seal bump
    3.
    发明授权
    Wing flap seal bump 有权
    翼翼密封凸块

    公开(公告)号：US6073889A

    公开(公告)日：2000-06-13

    申请号：US173922

    申请日：1998-10-16

    申请人： Paul W. Dees ,  Michael J. Irish ,  Thomas A. Zierten

    发明人： Paul W. Dees ,  Michael J. Irish ,  Thomas A. Zierten

    IPC分类号： B64C3/50 ,  B64C7/00

    CPC分类号： B64C7/02 ,  B64C3/50 ,  B64C7/00 ,  B64C9/24 ,  Y02T50/145 ,  Y02T50/32

    摘要： A sealing device (20) for an airplane (22). The airplane having a wing (24) and a first engine nacelle (26) attached to the wing. The wing having a wing root, a wing tip, a leading edge, a trailing edge and at least a first flap (30b) operatively connected to the leading edge. The flap being actuatable between a retracted position and an extended position. The flap in the extended position defining a gap between the flap and engine nacelle. The sealing device includes a body attached to the engine nacelle. The body having a forward portion (54), a center portion (56) and an aft portion (58). The body being positioned on the engine nacelle to contact the flap when the flap is in the extended position and forming a seal between the flap and nacelle to improve aerodynamic efficiency of the wing. The seal is formed by the flap being nested within the center portion of the body when the flap is in the extended position. The seal contours airflow along a spanwise direction defined by an axis extending between the wing root and tip to improve aerodynamic efficiency of the wing.

    摘要翻译： 一种用于飞机（22）的密封装置（20）。 具有机翼（24）和附接到机翼的第一发动机机舱（26）的飞机。 机翼具有翼根，翼尖，前缘，后缘和至少第一翼片（30b），其可操作地连接到前缘。 翼片可在缩回位置和伸出位置之间起动。 延伸位置处的翼片限定翼片和发动机舱之间的间隙。 密封装置包括附接到发动机舱的主体。 主体具有前部（54），中心部分（56）和后部（58）。 当皮瓣处于伸展位置时，身体被定位在发动机舱上以接触皮瓣，并在皮瓣和机舱之间形成密封，以提高机翼的空气动力学效率。 当翼片处于伸展位置时，该密封件由该片状物嵌套在该身体的中心部分内而形成。 密封件沿着翼展方向的气流沿由翼根和尖端之间延伸的轴限定，以提高机翼的空气动力学效率。

    Aircraft Trailing Edge Devices, Including Devices With Non-Parallel Motion Paths, and Associated Methods
    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

    IPC分类号： B64C3/50 ,  B64C13/00 ,  B64C3/18

    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。

    Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
    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。