公开(公告)号：WO2014176346A3

公开(公告)日：2015-04-16

申请号：PCT/US2014035161

申请日：2014-04-23

Applicant: LORD CORP ,  PTAK KEITH R ,  KRAKOWSKI FRANK J ,  SMID JOHN P ,  REDINGER W SCOTT

Inventor： PTAK KEITH R ,  KRAKOWSKI FRANK J ,  SMID JOHN P ,  REDINGER W SCOTT

IPC: E21B33/038 ,  E21B17/08 ,  E21B19/00

CPC classification number: E21B33/038 ,  E21B17/01 ,  E21B17/085 ,  E21B19/004 ,  F16L27/103

Abstract: This invention relates to an undersea riser bearing designed to operate at higher temperatures over an extended timeframe while maintaining performance advantages of high capacity laminate (HCL) elastomeric composite bearings.

Abstract translation: 本发明涉及一种海底提升管轴承，其设计成能够在更长的时间内在更高的温度下工作，同时保持高容量层压板（HCL）弹性体复合轴承的性能优点。

公开(公告)号：WO2014074831A2

公开(公告)日：2014-05-15

申请号：PCT/US2013069167

申请日：2013-11-08

Applicant: LORD CORP ,  ALTIERI RUSSELL E ,  JOLLY MARK R ,  BRANNAN WARREN F ,  MORRIS JR DONALD R ,  TRULL MICHAEL W ,  MARTIN RICHARD

Inventor： ALTIERI RUSSELL E ,  JOLLY MARK R ,  BRANNAN WARREN F ,  MORRIS JR DONALD R ,  TRULL MICHAEL W ,  MARTIN RICHARD

IPC: H01R39/24 ,  B64C27/32 ,  B64D15/12

CPC classification number: H01R39/08 ,  B64C27/32 ,  B64D15/12 ,  G01R31/04 ,  G01R31/327 ,  H01R39/24 ,  H02J5/005 ,  H04B5/0037

Abstract: Improvements to slip rings and methods for the operation thereof include an improved slip ring assembly that has a stationary element, a rotating element rotatable with respect to the stationary element, a bearing assembly coupled between the stationary element and the rotating element, and one or more contact brushes on one of the stationary element or the rotating element. In some embodiments, the bearing assembly includes a primary bearing, a secondary bearing, a shear pin coupling the secondary bearing to the primary bearing, and an electrical monitoring circuit in communication with the shear pin. In some embodiments, the one or more contact brushes includes one or more metal fiber brushes constructed of a plurality of metal fibers that are configured to transmit one or more of electrical power or data between the stationary element and the rotating element.

Abstract translation: 滑环的改进及其操作方法包括改进的滑环组件，其具有固定元件，可相对于静止元件旋转的旋转元件，联接在固定元件和旋转元件之间的轴承组件，以及一个或多个 接触刷在固定元件或旋转元件之一上。 在一些实施例中，轴承组件包括主轴承，次轴承，将次轴承连接到主轴承的剪切销以及与剪切销连通的电监控电路。 在一些实施例中，一个或多个接触刷包括由多个金属纤维构成的一个或多个金属纤维刷，所述多个金属纤维构造成在固定元件和旋转元件之间传输电力或数据中的一个或多个。

公开(公告)号：WO2013028830A3

公开(公告)日：2013-06-27

申请号：PCT/US2012052004

申请日：2012-08-23

Applicant: FORNES TIMOTHY ,  CARRUTHERS SETH ,  COX CHRISTOPHER ,  LORD CORP

Inventor： FORNES TIMOTHY ,  CARRUTHERS SETH ,  COX CHRISTOPHER

IPC: H05K9/00 ,  B64D45/02 ,  C09D5/24

CPC classification number: H05K9/0079 ,  B64D45/02 ,  C09D5/24

Abstract: A protective system is provided including a material comprising a first and second surface opposite one another and a thickness, and where the first surface has a low-electrical resistance and the second surface has a high-electrical resistance that is higher than the electrical resistance of the low-electrical resistance surface, and the material conducts charge from the first surface to the second surface through the thickness. This can be provided in a bilayer structure where a first protective layer having a low-resistivity is disposed upon a second protective layer having a high-resistivity. This protective system is particularly useful for dissipating electrical charge, for example as a lightning strike protection system for composite aircraft.

Abstract translation: 提供了一种保护系统，其包括具有彼此相对的第一表面和第二表面以及厚度的材料，并且其中第一表面具有低电阻，并且第二表面具有比电阻高的电阻 低电阻表面，并且该材料通过该厚度从第一表面向第二表面传导电荷。 这可以以双层结构提供，其中具有低电阻率的第一保护层设置在具有高电阻率的第二保护层上。 这种保护系统对于消散电荷特别有用，例如作为复合飞机的雷击保护系统。

公开(公告)号：WO2008136851A3

公开(公告)日：2009-05-07

申请号：PCT/US2007083171

申请日：2007-10-31

Applicant: LORD CORP ,  MARJORAM ROBERT H ,  HILDEBRAND STEVE F ,  IVERS DOUGLAS E ,  ERICKSEN GREGORY

Inventor： MARJORAM ROBERT H ,  HILDEBRAND STEVE F ,  IVERS DOUGLAS E ,  ERICKSEN GREGORY

IPC: F16F9/53

CPC classification number: B60G99/008 ,  B60G99/002 ,  F16F9/064 ,  F16F9/535 ,  F16F13/002

Abstract: A magneto-rheological fluid damper includes a damper body having a reservoir (108) for a magneto-rheological fluid, a piston rod (114), a piston rod guide (106) disposed within the damper body, where the piston rod guide has a passage (112) therein for receiving the piston rod. The magneto-rheological fluid damper further includes at least a first piston rod seal and at least a second piston rod seal (124, 128) arranged to seal between the piston rod guide and the piston rod. The magneto- rheological fluid damper further includes a fluid chamber (134) defined between the piston rod guide and the piston rod, the fluid chamber being in communication with the reservoir. The magneto-rheological fluid damper further includes a piston rod guide filter (120) arranged in a communication path between the fluid chamber and the reservoir to filter particulates out of the magneto-rheological fluid entering the fluid chamber. The magneto-rheological fluid damper further includes an accumulator (144) arranged between the piston rod guide and the damper body.

Abstract translation: 磁流变流体阻尼器包括具有用于磁流变流体的储存器（108）的阻尼器体，活塞杆（114），设置在阻尼器本体内的活塞杆引导件（106），其中活塞杆引导件具有 通道（112）用于接收活塞杆。 磁流变流体阻尼器进一步包括至少第一活塞杆密封件和至少第二活塞杆密封件（124,128），该密封件布置成在活塞杆引导件和活塞杆之间进行密封。 磁流变流体阻尼器还包括限定在活塞杆引导件和活塞杆之间的流体室（134），流体室与储存器连通。 磁流变流体阻尼器还包括设置在流体室和储存器之间的连通路径中的活塞杆引导过滤器（120），以过滤进入流体室的磁流变流体中的颗粒。 磁流变流体阻尼器还包括设置在活塞杆引导件和阻尼器本体之间的蓄能器（144）。

公开(公告)号：WO2009055007A2

公开(公告)日：2009-04-30

申请号：PCT/US2008012081

申请日：2008-10-24

Applicant: LORD CORP ,  MARK R JOLLY ,  BADRE-ALAM ASKARI ,  ALTIERI RUSSELL ,  MEYERS ANDREW D

Inventor： MARK R JOLLY ,  BADRE-ALAM ASKARI ,  ALTIERI RUSSELL ,  MEYERS ANDREW D

CPC classification number: B64C27/001 ,  B64C2027/004 ,  B64C2027/005 ,  F16F15/002 ,  F16F15/223

Abstract: An aircraft with at least one rotating machine creating troublesome vibrations, the aircraft comprised of an aerostructure, the aircraft including: a power source, the power source outputting a plurality of electromagnetic force generator power outputs, the aerostructure including a plurality of distributed actiye vibration control system sites, at least a first distributed active vibration electromagnetic force generator, the first distributed active vibration electromagnetic force generator including a first distributed electronic control system and a first electromagnetically driven mass, the first distributed active vibration electromagnetic force generator fixed to the aerostructure at a first distributed active vibration control system site, at least a second distributed active vibration electromagnetic force generator, the second distributed active vibration electromagnetic force generator including a second distributed electronic control system and a second electromagnetically driven mass, the second distributed active vibration electromagnetic force generator fixed to the aerostructure at a second distributed active vibration control system site, a plurality of electrical power distribution lines, the electrical power distribution lines connecting the electromagnetic force generators with the power source with the electromagnetic force generator power outputs outputted to the electromagnetic force generators, a distributed force generator data communications network, the distributed force generator data communications system network linking together the at least first and second distributed electronic control systems wherein the distributed electronic control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.

Abstract translation: 一种具有至少一个旋转机器的飞机产生麻烦的振动，该飞行器由航空结构组成，飞行器包括：电源，电源输出多个电磁力发生器功率输出，该航空结构包括多个分布式动力学振动控制 系统站点，至少第一分布式主动振动电磁力发生器，所述第一分布式主动振动电磁力发生器包括第一分布式电子控制系统和第一电磁驱动质量块，所述第一分布式主动振动电磁力发生器固定在所述空气结构 第一分布式主动振动控制系统现场，至少第二分布式主动振动电磁力发生器，所述第二分布式主动振动电磁力发生器包括第二分布式电子控制系统和第二电磁 第二分布式主动振动电磁力发生器在第二分布式主动振动控制系统现场固定到航空结构，多个电力分配线，电力分配线将电磁力发生器与电源连接，电磁 输出到电磁力发生器的力发电机功率输出，分布式力发生器数据通信网络，分布式力发生器数据通信系统网络将至少第一和第二分布式电子控制系统连接在一起，其中分布式电子控制系统将力发电机振动控制 数据通过分布式力发生器数据通信网络独立于电力配电线路，以尽量减少麻烦的振动。

公开(公告)号：WO2008097981A3

公开(公告)日：2008-11-27

申请号：PCT/US2008053062

申请日：2008-02-05

Applicant: LORD CORP ,  SMITH TYN ,  PTAK KEITH R ,  HALTOM BRYAN

Inventor： SMITH TYN ,  PTAK KEITH R ,  HALTOM BRYAN

IPC: F03D11/04

CPC classification number: F03D13/20 ,  F05B2240/9121 ,  F05B2260/96 ,  Y02E10/728

Abstract: A damper for a structural tower having a space frame construction for high elevation and heavy load applications is disclosed, with particular application directed to wind turbines. The structural tower includes one or more dampers for damping resonant vibrations or vibrations generated by non-periodic wind gusts or sustained high wind speeds. The wind tower damper includes a fluid damper comprising a housing, elastomeric chamber, piston and damping fluid, wherein relative motion between the first and second structural members drive the fluid moving piston to pump the fluid and thereby dissipate unwanted motion in the tower.

Abstract translation: 公开了一种用于具有用于高仰角和重载应用的空间框架结构的结构塔的阻尼器，特别适用于风力涡轮机。 结构塔包括一个或多个阻尼器，用于阻尼共振振动或由非周期阵风产生的振动或持续的高风速。 风塔阻尼器包括流体阻尼器，其包括壳体，弹性室，活塞和阻尼流体，其中第一和第二结构构件之间的相对运动驱动流体移动活塞以泵送流体，从而在塔中消散不期望的运动。

公开(公告)号：WO2008014466A2

公开(公告)日：2008-01-31

申请号：PCT/US2007074613

申请日：2007-07-27

Applicant: LORD CORP ,  PRESSLEY MARK W

Inventor： PRESSLEY MARK W

IPC: B29C65/00 ,  C08F2/50 ,  C08F4/40 ,  C08J5/00 ,  C09J5/00 ,  C09J5/10 ,  C09J133/00

CPC classification number: C09J5/00 ,  B29C35/0805 ,  B29C65/1403 ,  B29C65/1406 ,  B29C65/1409 ,  B29C65/1416 ,  B29C65/483 ,  B29C65/4845 ,  B29C65/485 ,  B29C65/4865 ,  B29C2035/0822 ,  B29C2035/0827 ,  B29C2035/0855 ,  B29K2101/12 ,  C08F2/50 ,  C08F4/40 ,  C08K5/07 ,  C08K5/5397 ,  C09J11/00 ,  C09J2433/00 ,  Y10T156/1002 ,  Y10T156/1028 ,  Y10T156/103 ,  Y10T156/1036 ,  Y10T428/2419 ,  Y10T428/24256 ,  Y10T428/28 ,  Y10T428/2804 ,  Y10T428/2809 ,  Y10T428/2857 ,  Y10T428/287

Abstract: An adhesive composition comprising as principal components, a polymerizable component, an ambient temperature radical polymerization catalyst system and a photoinitiator. The adhesive may optionally comprise an adhesion promoter, a toughener, an epoxy, and a filler material. Further, a two- part reactive adhesive comprising, a first part comprising, (i) at least one free radical-polymehzable monomer, (ii) at least one reducing agent, and (iii) a photoinitiator, and a second part comprising an oxidizing agent that is reactive at ambient temperature with the reducing agent to produce free radicals that are capable of initiating and propagating free radical polymerization.

Abstract translation: 一种粘合剂组合物，其包含作为主要组分的可聚合组分，环境温度自由基聚合催化剂体系和光引发剂。 粘合剂可任选地包含粘合促进剂，增韧剂，环氧树脂和填料。 此外，二部分反应性粘合剂包括第一部分，其包含（i）至少一种自由基可聚合单体，（ii）至少一种还原剂和（iii）光引发剂，第二部分包含氧化 该试剂在环境温度下与还原剂反应以产生能够引发和增殖自由基聚合的自由基。

公开(公告)号：WO2007140362A3

公开(公告)日：2008-01-17

申请号：PCT/US2007069871

申请日：2007-05-29

Applicant: LORD CORP ,  JONES PETER J ,  FUHRER ZACHARY

Inventor： JONES PETER J ,  FUHRER ZACHARY

IPC: B64C27/00 ,  B64C27/51

CPC classification number: B64C27/51 ,  F16F9/145

Abstract: The invention provides a rotary damper (20) for controlling helicopter motions. The rotary damper includes an outer canister (22) with an inner paddle wheel receiving cavity (26) which receives an inner paddle wheel (60) with upper and lower elastomeric tubular intermediate members (78,80) between the inner paddle wheel and the outer canister. The canister and inner paddle wheel form neighboring variable volume chambers (82,84) in liquid communication through liquid damping conduits. A clockwise rotation of the inner paddle wheel about the center of rotation axis (28) relative to the outer canister pumps damper liquid from a second variable volume chamber through a first liquid conduit towards a first variable volume chamber, and a counterclockwise rotation of the paddle wheel relative to the outer canister pumps the damper liquid from the first variable volume chamber through the first liquid conduit towards the second variable volume chamber with the elastomeric tubular intermediate members providing for the relative rotation and containing the damper liquid in the damper.

Abstract translation: 本发明提供了一种用于控制直升机运动的旋转阻尼器（20）。 旋转阻尼器包括带有内叶轮容纳空腔（26）的外罐（22），该内叶轮容纳空腔容纳内叶轮（60），在内叶轮和外叶轮之间具有上部和下部弹性管状中间构件（78,80） 罐。 罐和内桨叶形成通过液体阻尼导管液体连通的相邻可变容积腔室（82,84）。 内叶轮围绕旋转轴线（28）的中心相对于外罐的顺时针旋转将阻尼器液体从第二可变容积室通过第一液体导管朝向第一可变容积室泵送，并且桨的逆时针旋转 轮相对于外罐从第一可变容积腔室通过第一液体导管泵送阻尼器液体朝向第二可变容积腔室，其中弹性管状中间构件提供相对旋转并且将阻尼器液体容纳在阻尼器中。

公开(公告)号：WO2008002845A2

公开(公告)日：2008-01-03

申请号：PCT/US2007071927

申请日：2007-06-22

Applicant: LORD CORP ,  BALCZUN PAUL J

Inventor： BALCZUN PAUL J

IPC: F16D3/76 ,  F16D7/00 ,  F16F15/136

CPC classification number: F16D3/76 ,  F16D7/002 ,  F16F15/12353 ,  F16F15/124 ,  Y10T29/49229 ,  Y10T29/49826

Abstract: A multi-rate torsional coupling (20) features parallel first and second drive connections (82 and 84) between input (24) and output (22) members. The first drive connection (82) extends through a first resilient coupling (38), and the second drive connection (84) extends through a second resilient coupling (40). An angular play coupling (70) engages the second drive connection (84) at a particular torque load for transmitting additional torque through the torsional coupling (20) at a higher spring rate.

Abstract translation: 多速率扭转联轴器（20）在输入（24）和输出（22）部件之间具有平行的第一和第二驱动连接（82和84）。 第一驱动连接（82）延伸穿过第一弹性联接件（38），并且第二驱动连接（84）延伸穿过第二弹性联接件（40）。 角行程联接器（70）以特定的扭矩载荷接合第二驱动连接件（84），以用于以更高的弹簧刚度传递额外扭矩通过扭转联接器（20）。

公开(公告)号：WO2006135405A3

公开(公告)日：2007-02-22

申请号：PCT/US2005030909

申请日：2005-08-30

Applicant: LORD CORP ,  JOLLY MARK ,  HILDEBRAND STEPHEN ,  ALTIERI RUSSELL ,  IVERS DOUGLAS ,  FERGUSON MATTHEW

Inventor： JOLLY MARK ,  HILDEBRAND STEPHEN ,  ALTIERI RUSSELL ,  IVERS DOUGLAS ,  FERGUSON MATTHEW

IPC: B64C27/00

CPC classification number: F16F15/265 ,  B64C27/001 ,  B64C2027/003 ,  F16F15/22 ,  F16F15/267

Abstract: A helicopter rotating hub mounted vibration control system (20) for a helicopter rotary wing hub (22) having a periodic vibration (24) while rotating at a helicopter operational rotation frequency (26) . The helicopter rotating hub mounted vibration control system (20) includes an annular ring rotary housing (30) attachable to the helicopter rotary wing hub (22) and rotating with the helicopter rotary wing hub (22) at the helicopter operational rotation frequency (26) . The annular ring housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem (32) and preferably an adjacent coaxial rotor housing cavity subsystem (34) . The rotor housing cavity subsystem (34) contains a first coaxial frameless AC ring motor (36) having a first rotor with a first imbalance mass (40) and a second coaxial frameless AC ring motor (42) having a second rotor with a second imbalance mass (46) . The electronics housing cavity subsystem (32) contains an electronics control system (50) which receives sensor outputs and electrically controls and drives the first coaxial frameless AC ring motor (36) and the second coaxial frameless AC ring motor (42) such that the first imbalance mass (40) and the second imbalance mass (46) are directly driven at a vibration canceling rotation frequency (52) greater than the helicopter operational rotation frequency wherein the helicopter rotary wing hub periodic vibration (24) is reduced.

Abstract translation: 一种用于在直升机操作旋转频率（26）旋转的同时具有周期性振动（24）的直升机旋转翼形轮毂（22）的直升机旋转轮毂安装的振动控制系统（20）。 直升机旋转轮毂安装的振动控制系统（20）包括环形环旋转壳体（30），其可连接到直升机旋转翼毂（22）并且以直升机操作旋转频率（26）与直升机旋转翼毂（22）一起旋转， 。 环形壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体空腔子系统（32），并且优选地是相邻的同轴转子壳体空腔子系统（34）。 转子壳体腔子系统（34）包含第一同轴无框架AC环形电动机（36），其具有具有第一不平衡块（40）的第一转子和具有第二不平衡的第二转子的第二同轴无框架AC环形电动机（42） 质量（46）。 电子设备壳体腔子系统（32）包含电子控制系统（50），其接收传感器输出并电控制并驱动第一同轴无框架AC环形电动机（36）和第二同轴无框架AC环形电动机（42），使得第一 不平衡质量（40）和第二不平衡质量（46）以大于直升机旋转翼毂周期性振动（24）减小的直升机操作旋转频率的减振旋转频率（52）直接驱动。