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1. 发明授权

US09090330B2 Opening plug and method of installing the same 有权
标题翻译：打开插头和安装方法
公开(公告)号：US09090330B2
公开(公告)日：2015-07-28
申请号：US12413792
申请日：2009-03-30
申请人： Jack S. Noble , Gary D. Oakes , James Miller Wheaton
发明人： Jack S. Noble , Gary D. Oakes , James Miller Wheaton
IPC分类号： B64C1/14 , B64D29/08
CPC分类号： B64C1/1446 , B64D29/08 , Y10T29/49947
摘要： A device is used to plug an opening in a structure having a front side and a back side. The device includes a removable plug body for plugging the opening, and a retainer that is expandable into engagement with the back side of the structure to retain the plug in the opening. Means coupled with the retainer and the plug is provided for expanding the retainer.
摘要翻译：一种装置用于堵塞具有前侧和后侧的结构中的开口。该装置包括用于堵塞开口的可拆卸的塞体，以及可扩展成与结构的背面接合以将塞子保持在开口中的保持器。提供与保持器和插头相耦合的装置用于扩大保持器。

2. 发明授权

US08156887B2 Flap malfunction detection system 有权
标题翻译：襟翼故障检测系统
公开(公告)号：US08156887B2
公开(公告)日：2012-04-17
申请号：US12291194
申请日：2008-11-07
申请人： Kee How Tan , Seiya Sakurai , Gary D. Oakes , Philip Belanger , Jack S. Noble
发明人： Kee How Tan , Seiya Sakurai , Gary D. Oakes , Philip Belanger , Jack S. Noble
IPC分类号： B64C3/50
CPC分类号： B64D45/0005 , B64D2045/001
摘要： According to an embodiment, a flap malfunction indicator assembly for notifying an observer making a walk-around inspection of an aircraft of a malfunction of one or more connection points coupling a flap assembly to an aircraft wing includes a support mounted to the flap assembly having a perimeter defining an area, an indicator arm pivoted to the support and movable between a first stowed position in which a major portion of the arm is arranged substantially entirely within the area and a second deployed position in which a major portion of the arm is arranged substantially outside the area, a frangible pin or fastener securing the indicator arm to the support in the first stowed position, a trigger element mounted for rotation about a first pivot, an elongated pull linkage coupling the trigger element with a flap assembly, the pull linkage being supported for movement relative to the first pivot to cause rotation of the trigger element when malfunction of a flap assembly occurs, and a spring assembly at the support having one portion exerting a biasing force against a portion of the indicator arm located outside of the area, the spring assembly driving the indicator arm into the second deployed position when the frangible pin or fastener is broken.
摘要翻译：根据一个实施例，一种用于通知观察者对飞行器进行围绕检查以将翼片组件耦合到飞机机翼的一个或多个连接点的故障的通知的翼片故障指示器组件包括安装到翼片组件的支撑件，其具有限定区域的周边，指示臂枢转到所述支撑件并且可在第一收起位置和第二展开位置之间移动，所述第一收起位置中所述臂的主要部分基本上完全设置在所述区域内;以及第二展开位置，其中所述臂的主要部分基本上布置在所述区域外部，将所述指示器臂固定到所述第一收起位置中的所述支撑件的易碎销或紧固件，安装成围绕第一枢轴旋转的触发器元件，将所述触发器元件与翼片组件联接的细长拉动连杆，支撑相对于第一枢轴的运动，以在出现翼片组件的故障时引起触发元件的旋转在支撑件处的弹簧组件具有一部分对位于该区域外部的指示臂的一部分施加偏置力的弹簧组件，当易碎销或紧固件断裂时，弹簧组件将该指示臂驱动到第二展开位置。

3. 发明申请

US20100243809A1 OPENING PLUG AND METHOD OF INSTALLING THE SAME 有权
标题翻译：打开插头及其安装方法
公开(公告)号：US20100243809A1
公开(公告)日：2010-09-30
申请号：US12413792
申请日：2009-03-30
申请人： Jack S. Noble , Gary D. Oakes , James Miller Wheaton
发明人： Jack S. Noble , Gary D. Oakes , James Miller Wheaton
IPC分类号： B64C1/14 , B65D39/12 , B23P11/00
CPC分类号： B64C1/1446 , B64D29/08 , Y10T29/49947
摘要： A device is used to plug an opening in a structure having a front side and a back side. The device includes a removable plug body for plugging the opening, and a retainer that is expandable into engagement with the back side of the structure to retain the plug in the opening. Means coupled with the retainer and the plug is provided for expanding the retainer.
摘要翻译：一种装置用于堵塞具有前侧和后侧的结构中的开口。该装置包括用于堵塞开口的可拆卸的塞体，以及可扩展成与结构的背面接合以将塞子保持在开口中的保持器。提供与保持器和插头相耦合的装置用于扩大保持器。

4. 发明申请

US20100116193A1 Flap malfunction detection system 有权
标题翻译：襟翼故障检测系统
公开(公告)号：US20100116193A1
公开(公告)日：2010-05-13
申请号：US12291194
申请日：2008-11-07
申请人： Kee How Tan , Seiya Sakurai , Gary D. Oakes , Philip Belanger , Jack S. Noble
发明人： Kee How Tan , Seiya Sakurai , Gary D. Oakes , Philip Belanger , Jack S. Noble
IPC分类号： B64D45/00
CPC分类号： B64D45/0005 , B64D2045/001
摘要： According to an embodiment, a flap malfunction indicator assembly for notifying an observer making a walk-around inspection of an aircraft of a malfunction of one or more connection points coupling a flap assembly to an aircraft wing includes a support mounted to the flap assembly having a perimeter defining an area, an indicator arm pivoted to the support and movable between a first stowed position in which a major portion of the arm is arranged substantially entirely within the area and a second deployed position in which a major portion of the arm is arranged substantially outside the area, a frangible pin or fastener securing the indicator arm to the support in the first stowed position, a trigger element mounted for rotation about a first pivot, an elongated pull linkage coupling the trigger element with a flap assembly, the pull linkage being supported for movement relative to the first pivot to cause rotation of the trigger element when malfunction of a flap assembly occurs, and a spring assembly at the support having one portion exerting a biasing force against a portion of the indicator arm located outside of the area, the spring assembly driving the indicator arm into the second deployed position when the frangible pin or fastener is broken.
摘要翻译：根据一个实施例，一种用于通知观察者对飞行器进行围绕检查以将翼片组件耦合到飞机机翼的一个或多个连接点的故障的通知的翼片故障指示器组件包括安装到翼片组件的支撑件，其具有限定区域的周边，指示臂枢转到所述支撑件并且可在第一收起位置和第二展开位置之间移动，所述第一收起位置中所述臂的主要部分基本上完全设置在所述区域内;以及第二展开位置，其中所述臂的主要部分基本上布置在所述区域外部，将所述指示器臂固定到所述第一收起位置中的所述支撑件的易碎销或紧固件，安装成围绕第一枢轴旋转的触发器元件，将所述触发器元件与翼片组件联接的细长拉动连杆，支撑相对于第一枢轴的运动，以在出现翼片组件的故障时引起触发元件的旋转在支撑件处的弹簧组件具有一部分对位于该区域外部的指示臂的一部分施加偏置力的弹簧组件，当易碎销或紧固件断裂时，弹簧组件将该指示臂驱动到第二展开位置。

5. 发明授权

US07243881B2 Multi-function trailing edge devices and associated methods 有权
标题翻译：多功能后缘设备及相关方法
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
CPC分类号： B64C9/20 , B64C9/16 , Y02T50/32 , Y02T50/44
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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