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    IN-FLIGHT DETECTION OF WING FLAP FREE WHEELING SKEW
    1.
    发明申请
    IN-FLIGHT DETECTION OF WING FLAP FREE WHEELING SKEW 有权
    飞行检测飞轮免费轮辋

    公开(公告)号：US20100100355A1

    公开(公告)日：2010-04-22

    申请号：US12253747

    申请日：2008-10-17

    申请人： Alan D. Marx ,  Gary A. Emch ,  Mark J. Gardner ,  Richard I. Apfel ,  Michael E. Renzelmann ,  Christopher D. Feet ,  Michael R. Finn ,  Mark S. Good ,  Gregory J. Seehusen

    发明人： Alan D. Marx ,  Gary A. Emch ,  Mark J. Gardner ,  Richard I. Apfel ,  Michael E. Renzelmann ,  Christopher D. Feet ,  Michael R. Finn ,  Mark S. Good ,  Gregory J. Seehusen

    IPC分类号： G06F15/00

    CPC分类号： B64D45/0005 ,  B64D2045/001

    摘要： A method for detecting freewheeling skew failures in the wing flaps of an aircraft includes measuring the outputs of flap skew sensors when the aircraft is in flight (IF) and the flaps are extended to a selected position, and when the aircraft is next on the ground (OG) and the flaps are extended to the selected position. The respective differences between the IF and OG outputs of symmetrical pairs of the flap skew sensors are computed, and then the respective difference between the computed IF output difference and the computed OG output difference of each symmetrical pair of the sensors is computed. The computed IF and OG difference of each symmetrical pair of the sensors is then compared with each of predetermined maximum and minimum threshold value to determine whether a freewheeling skew failure exists in any of the flaps of the aircraft.

    摘要翻译： 一种用于检测飞行器翼片中的续流偏斜故障的方法，包括当飞机处于飞行中（IF）时测量襟翼歪斜传感器的输出，并且襟翼延伸到选定的位置，并且当飞机在地面上时 （OG），并且襟翼延伸到所选位置。 计算襟翼偏斜传感器的对称对的IF和OG输出之间的各自的差异，然后计算计算的IF输出差和每对传感器对的计算的OG输出差的相应差。 然后将每个对称的传感器对的计算的IF和OG差与预定的最大和最小阈值中的每一个进行比较，以确定是否存在飞行器的任何襟翼中的空转歪斜故障。

    In-flight detection of wing flap free wheeling skew
    2.
    发明授权
    In-flight detection of wing flap free wheeling skew 有权
    飞翼检测机翼翼片自由轮偏移

    公开(公告)号：US07945425B2

    公开(公告)日：2011-05-17

    申请号：US12253747

    申请日：2008-10-17

    申请人： Alan D. Marx ,  Gary A. Emch ,  Mark J. Gardner ,  Richard I. Apfel ,  Michael E. Renzelmann ,  Christopher D. Feet ,  Michael R. Finn ,  Mark S. Good ,  Gregory J. Seehusen

    发明人： Alan D. Marx ,  Gary A. Emch ,  Mark J. Gardner ,  Richard I. Apfel ,  Michael E. Renzelmann ,  Christopher D. Feet ,  Michael R. Finn ,  Mark S. Good ,  Gregory J. Seehusen

    IPC分类号： G06F11/30

    CPC分类号： B64D45/0005 ,  B64D2045/001

    摘要： A method for detecting freewheeling skew failures in the wing flaps of an aircraft includes measuring the outputs of flap skew sensors when the aircraft is in flight (IF) and the flaps are extended to a selected position, and when the aircraft is next on the ground (OG) and the flaps are extended to the selected position. The respective differences between the IF and OG outputs of symmetrical pairs of the flap skew sensors are computed, and then the respective difference between the computed IF output difference and the computed OG output difference of each symmetrical pair of the sensors is computed. The computed IF and OG difference of each symmetrical pair of the sensors is then compared with each of predetermined maximum and minimum threshold value to determine whether a freewheeling skew failure exists in any of the flaps of the aircraft.

    摘要翻译： 一种用于检测飞行器翼片中的续流偏斜故障的方法，包括当飞机处于飞行中（IF）时测量襟翼歪斜传感器的输出，并且襟翼延伸到选定的位置，并且当飞机在地面上时 （OG），并且襟翼延伸到所选位置。 计算襟翼偏斜传感器的对称对的IF和OG输出之间的各自的差异，然后计算计算的IF输出差和每对传感器对的计算的OG输出差的相应差。 然后将每个对称的传感器对的计算的IF和OG差与预定的最大和最小阈值中的每一个进行比较，以确定是否存在飞行器的任何襟翼中的空转歪斜故障。

    METHODS AND APPARATUS TO CONTROL MOVEMENT OF A COMPONENT
    4.
    发明申请
    METHODS AND APPARATUS TO CONTROL MOVEMENT OF A COMPONENT 审中-公开
    控制组件运动的方法和装置

    公开(公告)号：US20140033909A1

    公开(公告)日：2014-02-06

    申请号：US13566807

    申请日：2012-08-03

    申请人： Robert M. Murphy ,  Kelly T. Jones ,  Robert E. Fisher ,  Mark J. Gardner

    发明人： Robert M. Murphy ,  Kelly T. Jones ,  Robert E. Fisher ,  Mark J. Gardner

    IPC分类号： F15B15/00

    CPC分类号： F15B15/22 ,  B64D45/00 ,  B64D2045/0085 ,  F15B15/00 ,  F15B15/149 ,  F15B15/28 ,  F16F9/20 ,  F16F9/46 ,  F16F9/56

    摘要： Methods and apparatus to control movement of a component are disclosed herein. An example apparatus includes a housing defining a bore and a piston disposed inside the bore. The piston is to be coupled to a movable component disposed outside of the bore. The example apparatus further includes a fluid flowline in fluid communication with a first chamber of the bore and a second chamber of the bore. The first chamber is on a first side of the piston, and the second chamber on a second side of the piston. The example apparatus also includes a valve to control fluid flow through the fluid flowline. The valve is to be in a first state to enable the piston to dampen movement of the component, and the valve is to be in a second state to enable the piston to hold the component substantially stationary.

    摘要翻译： 本文公开了控制部件的运动的方法和装置。 示例性装置包括限定孔的壳体和设置在孔内的活塞。 活塞将联接到设置在孔外侧的可移动部件。 该示例设备还包括与孔的第一室流体连通的流体流线和孔的第二室。 第一腔室位于活塞的第一侧，第二腔室位于活塞的第二侧。 该示例性装置还包括用于控制通过流体流动管线的流体流动的阀。 该阀将处于第一状态，以使活塞能够抑制部件的运动，并且该阀将处于第二状态，以使活塞能够将部件保持在基本静止。

    Duplex skewed-roller brake disc
    6.
    发明授权
    Duplex skewed-roller brake disc 有权
    双面偏斜辊制动盘

    公开(公告)号：US06719106B1

    公开(公告)日：2004-04-13

    申请号：US10321960

    申请日：2002-12-17

    申请人： Mark J. Gardner

    发明人： Mark J. Gardner

    IPC分类号： B60T712

    CPC分类号： B64C13/28 ,  F16D59/00 ,  F16D65/18 ,  F16D2121/14 ,  F16D2127/10 ,  Y02T50/44

    摘要： A skewed-roller brake assembly 10 is provided, including a first rotor disc 12 and a second rotor disc 12. A stator disc 14, positioned between the first and second rotor discs 12, includes a plurality of skewed-roller slots 16 formed through the stator disc 14. A pair of roller elements 20 are positioned within each of the plurality of skewed-roller slots 16 such that a first of the pair of roller elements 21 protrudes from the stator disc 14 in the direction of the first rotor disc 22 and a second of said pair of roller elements 23 protrudes from the stator disc 14 in the direction of the second rotor disc 24. When the first and second rotor discs 12 are moved towards the stator disc 14, the first of the pair of roller elements 21 and the second of the pair of roller elements 23 rotate in concert while transmitting frictional torque to the first rotor disc 12 and the second rotor disc 12 respectively.

    摘要翻译： 提供了一种偏斜辊制动器组件10，其包括第一转子盘12和第二转子盘12.位于第一和第二转子盘12之间的定子盘14包括多个倾斜辊槽16， 一对辊元件20定位在多个倾斜辊槽16的每一个内，使得一对辊元件21中的第一个从定子盘14沿第一转子盘22的方向突出，并且 所述一对滚子元件23中的第二个从定子盘14沿第二转子盘24的方向突出。当第一和第二转子盘12朝向定子盘14移动时，该对滚子元件21中的第一个 并且一对滚子元件23中的第二个一起转动，同时将摩擦转矩分别传递到第一转子盘12和第二转子盘12。

    No-back/offset gear box
    7.
    发明授权
    No-back/offset gear box 有权
    无背/偏移齿轮箱

    公开(公告)号：US06231012B1

    公开(公告)日：2001-05-15

    申请号：US09180778

    申请日：1998-11-12

    申请人： Michael J. Cacciola ,  Mark J. Gardner ,  Stephen T. Steadman

    发明人： Michael J. Cacciola ,  Mark J. Gardner ,  Stephen T. Steadman

    IPC分类号： B64C358

    CPC分类号： F16D9/08 ,  B64C13/34 ,  B64D45/0005 ,  B64D2045/001 ,  F16H35/00 ,  F16H2035/005 ,  Y10T403/11

    摘要： Referring to FIG. 2, disclosed is an aircraft compound no-back/offset gearbox (2) with an integral load proportional safety (no-back) brake (50). The four gears are all 16 diametral pitch, involute external spur gears with 20 degree standard pressure angles. The two gear stages are interconnected with a mechanical fuse or shearout (40) designed to fail under excess shear loads and protect components downstream of the input shaft (10) from excess torque in the event of a system jam. The shearout (40) is essentially a quill shaft with external splines at both ends and an hourglass-shaped shear neckdown in the middle. The purpose of the no-back brake (50) is to prevent air loads from causing slat movement in the event of a torque tube disconnect. Referring to Figure, the no-back consists of a set of ball ramp (22) and brake plate components connected to the gearbox's output shaft. The ball ramp device converts part of the back driving torque into the axial force required to clamp the brake stack components (30) and restrain the output shaft. In this way, the back driving torque is reacted to structure and movement of the slat is prevented.

    摘要翻译： 参考图 2，公开了具有整体负载比例安全（无背）制动器（50）的飞机复合无背/偏移齿轮箱（2）。 四个齿轮均为16个直径节距，具有20度标准压力角的渐开线外直齿轮。 两个齿轮级与机械保险丝或剪切套（40）相互连接，设计成在过大的剪切载荷下失效，并在系统堵塞的情况下保护输入轴（10）下游的部件免受过大的扭矩。 剪力纱（40）基本上是一个带有轴向两端的花键轴和在中间的沙漏形剪切颈缩。 无背制动器（50）的目的是在扭矩管断开的情况下防止空气负载引起板条运动。 参考图，无背部由一组球道（22）和连接到变速箱输出轴的制动板组件组成。 滚珠坡道装置将后驱动扭矩的一部分转换成夹紧制动叠片部件（30）所需的轴向力并限制输出轴。 以这种方式，反向驱动扭矩反应结构，并且防止了板条的移动。

    Zinc aminophylline and its use in the treatment of bronchospasms
    8.
    发明授权
    Zinc aminophylline and its use in the treatment of bronchospasms 失效
    锌氨茶碱及其在治疗支气管扩张中的应用

    公开(公告)号：US4368197A

    公开(公告)日：1983-01-11

    申请号：US204861

    申请日：1980-11-07

    申请人： Eli Shefter ,  Francis X. Smith ,  Mark J. Gardner

    发明人： Eli Shefter ,  Francis X. Smith ,  Mark J. Gardner

    IPC分类号： C07D473/08 ,  A61K31/555 ,  C07F3/06 ,  C07F9/66

    CPC分类号： C07D473/08

    摘要： There is disclosed zinc complexes of amine salts of theophylline. The preferred compound disclosed is the zinc complex of aminophylline. These compounds are useful as bronchodilators and have antibronchospasmotic activity. They are substantially insoluble and do not impart an unpleasant taste to oral formulations. In addition, they are storage stable. The compounds are prepared by reacting a water soluble simple zinc salt with the amine salt of theophylline at temperatures of from 60.degree.-90.degree. C. for about 8 to 16 hours.

    摘要翻译： 公开了茶碱胺盐的锌络合物。 所公开的优选化合物是氨茶碱的锌络合物。 这些化合物可用作支气管扩张剂并具有抗纤维蛋白溶解作用。 它们基本上是不溶的，并且不会给口服制剂带来不愉快的味道。 另外，它们是储存稳定的。 通过使水溶性简单锌盐与茶碱胺盐在60〜90℃的温度下反应约8〜16小时来制备化合物。