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    Aircraft vehicular propulsion system monitoring device and method
    91.
    发明申请
    Aircraft vehicular propulsion system monitoring device and method 失效
    飞机车辆推进系统监控装置及方法

    公开(公告)号：US20040024499A1

    公开(公告)日：2004-02-05

    申请号：US10421325

    申请日：2003-04-23

    申请人： Lord Corporation

    发明人： Russell E. Altieri ,  James F. Kuhn ,  Mark R. Jolly ,  Steve C. Southward ,  Askari Badre-Alam ,  Leslie P. Fowler

    IPC分类号： G06F007/00

    CPC分类号： G01B7/31 ,  B64C29/005 ,  B64F5/60

    摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vertical propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The collar misalignment measuring system of the invention provide a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.

    摘要翻译： 描述了用于监测飞行器推进系统中的旋转轴轴和联轴器的方法和系统。 测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。 测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机，其中垂直推进动态旋转驱动轴系统和联轴器被实时监控。 车轴联轴器未对准测量系统利用多个位置传感器来提供对推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。 传感器的相对位置通过结构框架从旋转目标的外部刚性固定。 本发明的套环未对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量，其涉及在飞行器车辆的操作中的旋转轴联轴器的关键性能。 该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。

    Magnetically actuated friction damper
    92.
    发明申请
    Magnetically actuated friction damper 有权
    磁致动摩擦阻尼器

    公开(公告)号：US20030217901A1

    公开(公告)日：2003-11-27

    申请号：US09737889

    申请日：2000-12-15

    申请人： Lord Corporation

    发明人： J. David Carlson

    IPC分类号： F16F015/03

    CPC分类号： F16F15/03 ,  F16F7/08

    摘要： A friction damper a housing including a cavity formed therein; a first member disposed in said cavity and movable in said cavity; a second member disposed in said cavity; an intermediate member between the first and second members, the first member being in frictional engagement with the intermediate member; and at least one magnetic field generator mounted to magnetically couple the first and second members thereby maintaining the first member in frictional engagement with the intermediate member and wherein the first member is movable against the intermediate member to generate a damping force.

    摘要翻译： 一种摩擦阻尼器，其中形成有腔体的壳体; 第一构件，其设置在所述空腔中并可在所述空腔中移动; 设置在所述空腔中的第二构件; 第一构件和第二构件之间的中间构件，第一构件与中间构件摩擦接合; 以及安装成磁耦合第一和第二构件的至少一个磁场发生器，从而保持第一构件与中间构件摩擦接合，并且其中第一构件可抵靠中间构件移动以产生阻尼力。

    TWO-PART ADHESIVE: PART A-MONOMER,TOUGHENER(S), OPTIONAL ADHESION PROMOTOR AND REDUCING AGENT; PART B-EPOXY RESIN
    93.
    发明申请
    TWO-PART ADHESIVE: PART A-MONOMER,TOUGHENER(S), OPTIONAL ADHESION PROMOTOR AND REDUCING AGENT; PART B-EPOXY RESIN 有权
    两部分胶粘剂：A型单体，TOUGHENER（S），可选粘合促进剂和还原剂; B部分环氧树脂

    公开(公告)号：US20030216513A1

    公开(公告)日：2003-11-20

    申请号：US10147648

    申请日：2002-05-16

    申请人： Lord Corporation

    发明人： Robin F. Righettini ,  Jeffrey A. Hatcher

    IPC分类号： C08F008/00

    CPC分类号： C09J151/006 ,  C08F279/00 ,  C08F283/00 ,  C08F287/00 ,  C08F290/048 ,  C08L2666/02 ,  C08L2666/14 ,  C09J4/06 ,  C09J151/003

    摘要： Epoxy-modified, two-part acrylic structural adhesives characterized by improved T-peel strength are disclosed. These adhesives are not inhibited by oxygen. Representative embodiments include 2-part acrylic structural adhesives comprising, in a first package from about 10 to about 90 percent by weight of at least one methacrylate selected from C3-C10 alkyl monosubstituted-, C1-C6 alkyl disubstituted-, C1-C4 alkyl tri-substituted, and C1-C4 alkyl tetra-substituted cyclohexyl methacrylate. The ring substituents are prefereably in the 3, 4, and/or 5 ring position, and linear or branched C4-C10 branched alkyl methacrylates; from about 10 to about 80 percent by weight of a toughener, and an adhesion promotor; and in a second package, a bonding activator, and optional epoxy resin.

    摘要翻译： 公开了以改进的T剥离强度为特征的环氧改性的两部分丙烯酸结构粘合剂。 这些粘合剂不受氧气的抑制。 代表性实施方案包括2-部分丙烯酸结构粘合剂，其包含在约10至约90重量％的至少一种甲基丙烯酸酯的第一包装中，所述甲基丙烯酸酯选自C 3 -C 10烷基单取代的，C 1 -C 6烷基二取代的，C 1 -C 4烷基三 - 取代的，和C 1 -C 4烷基四取代的甲基丙烯酸环己酯。 环取代基优选在3,4和/或5个环位置，直链或支链的C 4 -C 10支链烷基甲基丙烯酸酯; 约10至约80重量％的增韧剂和粘合促进剂; 并且在第二包装中，结合活化剂和任选的环氧树脂。

    Magnetically actuated motion control device
    94.
    发明申请
    Magnetically actuated motion control device 失效
    磁驱动运动控制装置

    公开(公告)号：US20030209394A1

    公开(公告)日：2003-11-13

    申请号：US10140341

    申请日：2002-05-07

    申请人： Lord Corporation

    发明人： J. David Carlson

    IPC分类号： F16F015/03

    CPC分类号： F16F7/082

    摘要： A magnetically actuated motion control device includes a housing defining a cavity and including a slot therethrough. A movable member is located within the cavity and is movable relative to the housing. A magnetic field generator located on either the housing or the movable member causes the housing to press against the movable member to develop a friction force. The flux caused by the magnetic field flows through the housing, the movable member and at least one pole located along the movable member. The at least one pole comprises a first portion having a first axial dimension and a second portion having a second axial dimension where the first axial dimension is greater than the second axial dimension and as a result the magnetic flux through the second portion of the at least one pole has a greater magnitude than the magnetic flux through the first portion of the pole.

    摘要翻译： 磁力驱动的运动控制装置包括限定空腔并且包括穿过其中的槽的壳体。 可动构件位于空腔内并且可相对于壳体移动。 位于外壳或活动件上的磁场发生器使壳体压靠可移动件以产生摩擦力。 由磁场引起的磁通量通过壳体，可移动部件和沿着可移动部件定位的至少一个磁极。 所述至少一个极包括具有第一轴向尺寸的第一部分和具有第二轴向尺寸的第二部分，其中第一轴向尺寸大于第二轴向尺寸，并且结果是通过至少至少的第二部分的磁通量 一个极具有比通过极的第一部分的磁通量更大的幅度。

    Controlled equilibrium device with displacement dependent spring rates and integral damping
    96.
    发明申请
    Controlled equilibrium device with displacement dependent spring rates and integral damping 失效
    具有位移依赖弹簧刚度和积分阻尼的受控平衡装置

    公开(公告)号：US20030015830A1

    公开(公告)日：2003-01-23

    申请号：US09910386

    申请日：2001-07-20

    申请人： Lord Corporation

    发明人： Lane R. Miller ,  Douglas A. Swanson ,  Russell E. Alteri ,  Douglas E. Ivers ,  Stephen F. Hildebrand ,  William S. Jensen ,  Scott K. Miller ,  Michael D. Janowski ,  Michael F. Walch

    IPC分类号： F16F005/00

    CPC分类号： F16F13/06 ,  B60G15/08 ,  B60G15/12 ,  B60G17/0485 ,  B60G17/0525 ,  B60G17/0565 ,  B60G2202/314 ,  B60G2400/252 ,  B60G2500/2022 ,  B60G2500/2042 ,  B60G2500/2044 ,  B60G2600/02 ,  F16F7/09

    摘要： A controlled equilibrium device comprising a housing; at least one spring, each at least one spring having a spring stiffness; and a load leveling device movable through the housing between a first maximum displacement position and a second maximum displacement position, the load leveling device comprising a deadband displacement zone defined between a first deadband displacement threshold and a second deadband displacement threshold, the displacement required to reach the first and second deadband displacement thresholds being less than the displacement distances required to reach the first and second maximum displacement positions, the at least one spring stiffness being substantially constant when the displacement of the load leveling device is within the deadband zone, the stiffness of the at least one spring being modified to a second stiffness when the load leveling device is equal to or beyond either the first deadband displacement threshold or the second deadband displacement threshold.

    摘要翻译： 一种受控平衡装置，包括壳体; 至少一个弹簧，每个至少一个弹簧具有弹簧刚度; 以及负载调平装置，其可在第一最大位移位置和第二最大位移位置之间移动穿过所述壳体，所述负载均衡装置包括限定在第一死区位移阈值和第二死区位移阈值之间的死区位移区域， 第一和第二死区位移阈值小于达到第一和第二最大位移位置所需的位移距离，当负载调平装置的位移在死区区内时，至少一个弹簧刚度基本上恒定，刚度 当所述负载均衡装置等于或超过所述第一死区位移阈值或所述第二死区位移阈值时，所述至少一个弹簧被修改为第二刚度。

    Mounting assembly for an aircraft auxiliary power unit and method
    98.
    发明申请
    Mounting assembly for an aircraft auxiliary power unit and method 有权
    飞机辅助动力装置的安装组件及方法

    公开(公告)号：US20020084381A1

    公开(公告)日：2002-07-04

    申请号：US09965942

    申请日：2001-09-27

    申请人： Lord Corporation

    发明人： Jacques Lemire ,  Kirk W. Olsen ,  Francis J. DePriest ,  Thomas R. Law ,  Gerald P. Whiteford ,  Paul J. Bachmeyer

    IPC分类号： B64D027/00

    CPC分类号： B64D41/00 ,  B64D2041/002

    摘要： A system for supporting an auxiliary power unit in an aircraft tailcone wherein the auxiliary power unit is supported by a focalized suspension system supporting the power unit, the focalized suspension system having a plurality of support means each having a line of action, the lines of action intersecting at the focal point. The support system simplifies removal and installation of the auxiliary power unit from and into the aircraft's tailcone.

    摘要翻译： 一种用于在飞机尾座中支撑辅助动力单元的系统，其中所述辅助动力单元由支撑所述动力单元的聚焦悬架系统支撑，所述聚焦悬架系统具有多个支撑装置，每个支撑装置具有动作线，所述动作线 在焦点处相交。 支持系统简化了辅助动力单元从飞机尾部的拆卸和安装。

    Vibration isolation device with load dependent stiffness
    99.
    发明申请
    Vibration isolation device with load dependent stiffness 有权
    具有负载依赖刚度的隔振装置

    公开(公告)号：US20020079630A1

    公开(公告)日：2002-06-27

    申请号：US09910384

    申请日：2001-07-20

    申请人： Lord Corporation

    发明人： Paul J. Bachmeyer ,  Michael R. Blewett ,  Marvin D. Ohme

    IPC分类号： F16F005/00 ,  F16F013/00

    CPC分类号： F16F3/0876 ,  F16F3/087 ,  F16F7/003 ,  F16F2228/066

    摘要： A vibration isolation device is disclosed. More specifically the vibration isolation device of the present invention comprises means for decreasing the mount stiffness when loads above a threshold load value are applied to the device. The means for decreasing the mount stiffness comprises a shear pin with shear locations that comprise annular grooves with semielliptical cross sections.

    摘要翻译： 公开了一种隔振装置。 更具体地说，本发明的隔振装置包括用于当将高于阈值负载值的负载施加到装置时降低安装刚度的装置。 用于减小安装刚度的装置包括剪切销，剪切位置包括具有半椭圆形横截面的环形槽。