公开(公告)号：WO2013027028A3

公开(公告)日：2013-04-25

申请号：PCT/GB2012052007

申请日：2012-08-16

Applicant: TAYLOR HOBSON LTD ,  LEE-BENNETT IAN ,  BARBOSA RONY MORENO

Inventor： LEE-BENNETT IAN ,  BARBOSA RONY MORENO

IPC: G01B7/008 ,  G01B5/008 ,  G01B11/00 ,  G01B21/04

CPC classification number: G01B7/008 ,  G01B5/0004 ,  G01B5/201 ,  G01B21/04

Abstract: A workpiece centring assembly comprising a workpiece support surface and sleeve, the workpiece support surface and sleeve being arranged for relative rotation, and jaws arranged for movement with respect to the workpiece support surface to centre the workpiece on the workpiece support surface, further comprising elongate bearings arranged for rotation with the workpiece support surface, slidable members supporting the jaws and arranged for movement along the elongate bearings, and connectors having pivotal couplings to respective slidable members and the sleeve, wherein the relative rotation causes the connectors to pivot about their pivotal couplings to allow movement of the slidable members along the elongate bearings and consequential movement of the jaws with respect to the workpiece support surface.

Abstract translation: 一种工件定心组件，包括工件支撑表面和套筒，工件支撑表面和套筒布置成相对旋转，并且夹爪布置成相对于工件支撑表面移动以将工件居中在工件支撑表面上，还包括细长轴承 布置成与工件支撑表面一起旋转，可滑动构件支撑夹爪并布置成沿着细长轴承运动，以及具有可枢转联接器到相应的可滑动构件和套筒的连接器，其中相对旋转使得连接器绕其枢转联接器枢转到 允许可滑动构件沿着细长轴承移动，并且夹爪相对于工件支撑表面的相应运动。

公开(公告)号：WO2011098745A2

公开(公告)日：2011-08-18

申请号：PCT/GB2010/000244

申请日：2010-02-10

Applicant: MESSIER-DOWTY LTD ,  BENNETT, Ian ,  MENEZES, Robert ,  SHAW, Paul

Inventor： BENNETT, Ian ,  MENEZES, Robert ,  SHAW, Paul

IPC: B64C25/34

CPC classification number: B64C25/34 ,  B64C25/48 ,  B64C25/50 ,  B64C2025/345

Abstract: There is described a landing gear having a bogie including a elongated beam (2) for accommodating at least two axles receiving each a pair of ground engaging wheels, at least one axle (5) being pivotally mounted on the elongated beam. The landing gear further includes axle travel limitation means (10) extending between said pivotable axle and said elongated beam to be hitched up thereto, said travel limitation means being deformable one way starting from an stable and lockable state thereof corresponding to a landing position of said pivotable axle. There are also described independently lockable and actuatable telescopic struts.

Abstract translation: 描述了一种具有转向架的起落架，该转向架包括用于容纳至少两个接收每一个地面接合轮的轴的细长梁（2），至少一个轴（5）可枢转地安装在细长梁上。 起落架还包括在所述可枢转轴与所述细长梁之间延伸的轴行进限制装置（10），所述轴行程限制装置（10）在与之相连的所述细长梁之间延伸，所述行驶限制装置可自其稳定和可锁定的状态单向变形， 可枢转轴。 还描述了独立的可锁定和可致动的伸缩支柱。

公开(公告)号：WO2011048394A1

公开(公告)日：2011-04-28

申请号：PCT/GB2010/050716

申请日：2010-04-30

Applicant: MESSIER-DOWTY LIMITED ,  HILLIARD, Matthew ,  BENNETT, Ian

Inventor： HILLIARD, Matthew ,  BENNETT, Ian

IPC: B64C25/34

CPC classification number: B64C25/34

Abstract: An aircraft landing gear assembly including a bogie beam, a landing gear strut (1) having a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam (3), and a stop (13) arranged to limit pivotal movement of the bogie beam relative to the landing gear strut, wherein the stop comprises at least one elongate member arranged to be deflectable in bending when the bogie beam reaches a pivotal limit.

Abstract translation: 包括转向架梁的飞机起落架组件，具有被布置成可枢转地联接到飞行器的第一端的起落架支柱（1）和枢转地联接到转向架梁（3）的第二端以及设置在所述转向架梁 以限制转向架相对于起落架支柱的枢转运动，其中止挡包括布置成当转向架梁达到枢转极限时可弯曲弯曲的至少一个细长构件。

公开(公告)号：WO2010027265A3

公开(公告)日：2011-03-03

申请号：PCT/NL2009050534

申请日：2009-09-04

Applicant: SOLLAND SOLAR ENERGY HOLDING B V ,  VON MOLTKE BODO ,  BOTHE FRANK ,  PODLOWSKI LARS ,  PLOMP BERT ,  KLOOS MARIO ,  TJENGDRAWIRA CAROLINE ,  BENNETT IAN ,  DE JONG PAUL

Inventor： VON MOLTKE BODO ,  BOTHE FRANK ,  PODLOWSKI LARS ,  PLOMP BERT ,  KLOOS MARIO ,  TJENGDRAWIRA CAROLINE ,  BENNETT IAN ,  DE JONG PAUL

IPC: H01L31/05 ,  B23K1/005 ,  B23K26/08 ,  B23K26/10 ,  H01L31/048 ,  H01L31/18

CPC classification number: B23K1/0056 ,  H01L31/048 ,  H01L31/0516 ,  H01L31/18 ,  Y02E10/50

Abstract: Method for manufacturing a photovoltaic module (1) comprising: a) providing an electrically conductive substrate, the substrate being provided with a predetermined electrical pattern; b) depositing a solder paste (7) onto the electrically conductive substrate at pre-defined interconnection locations; c) placing a first encapsulant layer (3) provided with a pattern of openings onto the electrically conductive substrate, the pattern of openings corresponding with the locations of the solder paste (7); d) placing back-contact solar cells (4) on the first encapsulant layer so as to have a match of the electrical pattern of the back-contact solar cells with the electrical pattern of the electrically conductive substrate; e) placing a second encapsulant layer (5) on the back-contact solar cells (4), and placing a glass layer (6) on the second encapsulant layer (5); f) applying heat and pressure to the components (2, 3, 4, 5, 6, 7) to cause the encapsulant materials to flow and form a monolithic photovoltaic module, characterised by local application of at the interconnection locations utilizing a laser to couple its energy locally into the solar cell from the side of the glass layer, so as to cause the solder paste to reflow between each interconnection location and its respective matching connection location on the back-contact solar cell for establishing electrical interconnection between the back-contact solar cells and the electrically conductive substrate.

Abstract translation: 一种用于制造光伏模块（1）的方法，包括：a）提供导电基板，所述基板设置有预定的电气图案; b）在预定的互连位置处将焊膏（7）沉积到导电衬底上; c）将具有开口图案的第一密封剂层（3）放置在所述导电基底上，所述开口图案对应于所述焊膏（7）的位置; d）将反接触太阳能电池（4）放置在第一密封剂层上以使背接触太阳能电池的电气图案与导电基板的电气图案相匹配; e）将第二密封剂层（5）放置在所述背接触太阳能电池（4）上，以及将玻璃层（6）放置在所述第二密封层（5）上; f）向组件（2,3,4,5,6,7）施加热和压力以使密封剂材料流动并形成单片光伏模块，其特征在于利用激光耦合在互连位置处的局部应用 其能量从玻璃层的一侧局部地进入太阳能电池，从而使焊膏在每个互连位置与其背面接触太阳能电池上的相应匹配连接位置之间回流，以建立背接触 太阳能电池和导电基板。

公开(公告)号：WO2011017363A1

公开(公告)日：2011-02-10

申请号：PCT/US2010/044300

申请日：2010-08-03

Applicant: SIMPIRICA SPINE, INC. ,  FIELDING, Louis ,  BENNETT, Ian ,  KOTHARI, Manish ,  ALAMIN, Todd ,  MALANDAIN, Hugues ,  LITHERLAND, Craig ,  CAHILL, Colin

Inventor： FIELDING, Louis ,  BENNETT, Ian ,  KOTHARI, Manish ,  ALAMIN, Todd ,  MALANDAIN, Hugues ,  LITHERLAND, Craig ,  CAHILL, Colin

IPC: A61B17/70

CPC classification number: A61B17/7068 ,  A61B17/7053 ,  A61B17/7062 ,  A61B17/7067 ,  A61B17/842 ,  A61B2090/064

Abstract: A system for restricting spinal flexion includes superior and inferior tether structures joined by a pair of compliance members. Compliance members comprise tension members which apply a relatively low elastic tension on the tether structures. By placing the tether structures on or over adjacent spinous processes, flexion of a spinal segment can be controlled in order to reduce pain.

Abstract translation: 用于限制脊柱屈曲的系统包括由一对顺应性构件连接的上部和下部系绳结构。 合规构件包括在系绳结构上施加相对较低的弹性张力的张力构件。 通过将系绳结构置于相邻的棘突之上或之上，可以控制脊椎节段的屈曲以减轻疼痛。

公开(公告)号：WO2010055354A3

公开(公告)日：2011-01-06

申请号：PCT/GB2009051545

申请日：2009-11-16

Applicant: MESSIER DOWTY LTD ,  BENNETT IAN

Inventor： BENNETT IAN

IPC: G01L1/06 ,  B64C25/00

CPC classification number: G01L1/06 ,  B64C25/00 ,  B64D2045/008

Abstract: An overload detecting assembly comprising a lateral probe (18) which cooperates with a first load bearing member (10) as it moves towards a second load bearing member (11) and in turn deflects an indicator member (20) which may take a permanent set when a yield point is exceeded. Ready inspection of the indicator member reveals whether or not it has been bent. The indicator member may comprise a cantilevered beam (24) formed in a sleeve (20) coaxial with the load bearing members (10, 11). Alternatively, an extension (25) of the probe (18) may deflect laterally at a midpoint under overload conditions. Alternatively, the probe (18) may form an impression in an indicator member (30) under overload conditions.

Abstract translation: 一种过载检测组件，包括横向探针（18），当侧向探针（18）向第二承载构件（11）移动时与第一负载承载构件（10）协作，并且使指示器构件（20）偏转，所述指示器构件 当超过屈服点时。 指示器构件的准备检查显示是否弯曲。 指示器构件可以包括形成在与承载构件（10,11）同轴的套筒（20）中的悬臂梁（24）。 或者，探针（18）的延伸部（25）可以在过载条件下的中点处横向偏转。 或者，探针（18）可以在过载条件下在指示器构件（30）中形成印模。

公开(公告)号：WO2010027265A2

公开(公告)日：2010-03-11

申请号：PCT/NL2009/050534

申请日：2009-09-04

Applicant: SOLLAND SOLAR ENERGY HOLDING B.V. ,  VON MOLTKE, Bodo ,  BOTHE, Frank ,  PODLOWSKI, Lars ,  PLOMP, Bert ,  KLOOS, Mario ,  TJENGDRAWIRA, Caroline ,  BENNETT, Ian ,  DE JONG, Paul

Inventor： VON MOLTKE, Bodo ,  BOTHE, Frank ,  PODLOWSKI, Lars ,  PLOMP, Bert ,  KLOOS, Mario ,  TJENGDRAWIRA, Caroline ,  BENNETT, Ian ,  DE JONG, Paul

IPC: H01L31/05 ,  H01L31/18 ,  H01L31/048

CPC classification number: B23K1/0056 ,  H01L31/048 ,  H01L31/0516 ,  H01L31/18 ,  Y02E10/50

Abstract: Method for manufacturing a photovoltaic module (1) comprising: a) providing an electrically conductive substrate, the substrate being provided with a predetermined electrical pattern; b) depositing a solder paste (7) onto the electrically conductive substrate at pre-defined interconnection locations; c) placing a first encapsulant layer (3) provided with a pattern of openings onto the electrically conductive substrate, the pattern of openings corresponding with the locations of the solder paste (7); d) placing back-contact solar cells (4) on the first encapsulant layer so as to have a match of the electrical pattern of the back-contact solar cells with the electrical pattern of the electrically conductive substrate; e) placing a second encapsulant layer (5) on the back-contact solar cells (4), and placing a glass layer (6) on the second encapsulant layer (5); f) applying heat and pressure to the components (2, 3, 4, 5, 6, 7) to cause the encapsulant materials to flow and form a monolithic photovoltaic module, characterised by local application of at the interconnection locations utilizing a laser to couple its energy locally into the solar cell from the side of the glass layer, so as to cause the solder paste to reflow between each interconnection location and its respective matching connection location on the back-contact solar cell for establishing electrical interconnection between the back-contact solar cells and the electrically conductive substrate.

Abstract translation: 一种用于制造光伏模块（1）的方法，包括：a）提供导电基板，所述基板设置有预定的电气图案; b）在预定的互连位置处将焊膏（7）沉积到导电衬底上; c）将具有开口图案的第一密封剂层（3）放置在所述导电基底上，所述开口图案对应于所述焊膏（7）的位置; d）将反接触太阳能电池（4）放置在第一密封剂层上以使背接触太阳能电池的电气图案与导电基板的电气图案相匹配; e）将第二密封剂层（5）放置在所述背接触太阳能电池（4）上，以及将玻璃层（6）放置在所述第二密封层（5）上; f）向组件（2,3,4,5,6,7）施加热和压力以使密封剂材料流动并形成单片光伏模块，其特征在于利用激光耦合在互连位置处的局部应用 其能量从玻璃层的一侧局部地进入太阳能电池，从而使焊膏在每个互连位置与其背面接触太阳能电池上的相应匹配连接位置之间回流，以建立背接触 太阳能电池和导电基板。

公开(公告)号：WO2009149407A9

公开(公告)日：2009-12-10

申请号：PCT/US2009/046492

申请日：2009-06-05

Applicant: SIMPIRICA SPINE, INC. ,  FIELDING, Louis ,  MALANDAIN, Hugues ,  BENNETT, Ian ,  ALAMIN, Todd

Inventor： FIELDING, Louis ,  MALANDAIN, Hugues ,  BENNETT, Ian ,  ALAMIN, Todd

IPC: A61B17/70

Abstract: Fastening mechanisms for releasably locking a tether are provided. The mechanisms find application with orthopedic internal-fixation implants and make the implants more reliable and their implantation less invasive. A method for releasably locking a tether comprises advancing the tether through a tether aperture in a clamp body. The tether enters the tether aperture in a first plane and exits in a second plane generally transverse to the first plane. Positioning a fastener element in a fastener aperture in the clamp body captures the tether between the clamp body and the fastener element thereby releasably locking the tether in position relative to the clamp body.

公开(公告)号：WO2009047367A3

公开(公告)日：2009-11-12

申请号：PCT/EP2008063743

申请日：2008-10-13

Applicant: MESSIER DOWTY LTD ,  BENNETT IAN

Inventor： BENNETT IAN

IPC: B64C25/00 ,  B64C25/22 ,  B64C25/34 ,  B64C25/58 ,  B64C25/60 ,  F16F9/06

CPC classification number: B64C25/34 ,  B64C25/58 ,  B64D2045/008 ,  F16F9/3264

Abstract: A landing gear for an aircraft comprises: a shock absorber strut (1) with upper and lower telescoping portions (2, 3), the upper portion (2) being connectable to the airframe of the aircraft; an arm (4) to extend fore and aft relative to the aircraft and carrying a landing wheel, (7, 71), and pivotally connected by a main pivot (5) to the lower portion (3) of the shock absorber strut; and a load reacting unit (9) connected between the arm (4) and the shock absorber strut (1) for reacting to load applied between the arm and shock absorber strut on landing, and an indicator (60) for monitoring the load applied to the load reacting unit (9) on landing. The load reacting unit (9) may be connected between a forward end of the arm (4) and the upper portion (2) of the shock absorber strut to make the gear act as a semi-levered landing gear. Alternatively, the load reacting unit (9) may be connected between the arm (4) and the lower portion (3) of the shock absorber strut to act as a pitch trimmer. The arm (4) may comprise a bogie beam with fore and aft landing wheels (7, 71) with the main pivot (5) therebetween. The load reacting unit (9) preferably comprises a fluid pressure unit and the indicator (60) comprises a mechanical indicator that operates at a predetermined pressure threshold.

Abstract translation: 一种用于飞机的起落架，包括：具有上伸缩部分和下伸缩部分（2,3）的减震器支柱（1），所述上部分（​​2）可连接至所述飞机的机身; 相对于飞行器前后延伸并且承载着陆轮（7,71）并且通过主枢轴（5）枢转地连接到减震器支柱的下部（3）的臂（4） 以及连接在所述臂（4）和所述减震器支柱（1）之间的负载反应单元（9），用于对在着陆时施加在所述臂和减震器支柱之间的负载作出反应，以及指示器（60），用于监测施加到 负载反应单元（9）着陆。 负载反应单元（9）可连接在臂（4）的前端和减震器支柱的上部（2）之间，以使齿轮起到半摇臂起落架的作用。 可选地，负载反应单元（9）可以连接在减震器支杆的臂（4）和下部（3）之间以用作间距修剪器。 臂（4）可以包括具有前部和后部着陆轮（7,71）的转向架梁，其间具有主枢轴（5）。 负载反应单元（9）优选地包括流体压力单元，并且指示器（60）包括在预定压力阈值下操作的机械指示器。

公开(公告)号：WO2008051802A3

公开(公告)日：2008-07-10

申请号：PCT/US2007081822

申请日：2007-10-18

Applicant: SIMPIRICA SPINE INC ,  ALAMIN TODD ,  BENNETT IAN ,  FIELDING LOUIS ,  CAHILL COLIN

Inventor： ALAMIN TODD ,  BENNETT IAN ,  FIELDING LOUIS ,  CAHILL COLIN

IPC: A61B17/00

CPC classification number: A61B17/7062 ,  A61B17/7053 ,  A61B17/7055 ,  A61B17/842

Abstract: Methods, apparatus and systems for constraining spinous processes to elastically limit flexion of two or more adjacent spinal segments rely on placing a tether structure over at least three adjacent vertebral bodies or two adjacent vertebral bodies and the sacrum. The tether structures may be continuous, for example in the form of a continuous loop, or may be discontinuous, for example in the form of a loop or elongate element having at least two anchor structures for securing in bone.

Abstract translation: 方法，设备和系统用于约束棘突以弹性地限制两个或更多个相邻的脊柱节段的弯曲依靠放置系绳结构在至少三个相邻的椎骨体或两个相邻椎体和骶骨。 系绳结构可以是连续的，例如以连续环的形式，或者可以是不连续的，例如以具有用于固定在骨头中的至少两个锚定结构的环或细长元件的形式。