METROLOGICAL APPARATUS
    21.
    发明申请
    METROLOGICAL APPARATUS 审中-公开
    计量器具

    公开(公告)号:WO2013017834A1

    公开(公告)日:2013-02-07

    申请号:PCT/GB2012/051743

    申请日:2012-07-20

    Inventor: LEE-BENNETT, Ian

    CPC classification number: G01B5/0004 G01B5/008 G01B5/201 G01B5/285

    Abstract: A stylus support carries a stylus having a stylus tip for following a workpiece surface which rotates relative to the stylus support. A transducer senses a displacement of the stylus tip as follows the surface. A support structure includes a mounting arm and an attitude arm carrying the stylus support and mounted to the mounting arm by a kinematic coupling so as to be moveable between the first attitude in which a stylus extends in a first direction and a second attitude in which the stylus extends in a direction transverse to the first, the movement being substantially centred at the stylus tip. The coupling comprises protrusions and recesses provided on opposing faces of the attitude and mounting arms, the protrusions and recesses being configured to cooperate to constrain relative motion of the opposing faces when the attitude arm is moved into one of the first and second attitudes.

    Abstract translation: 触针支架带有一个触针,该触针具有用于跟随相对于触针支撑件旋转的工件表面的触针尖端。 传感器检测触针尖端的位移如下表面。 支撑结构包括安装臂和承载触笔支架的姿态臂,并通过运动耦合安装到安装臂上,以便能够在触针沿着第一方向延伸的第一姿态和第二姿态之间移动, 触针在横向于第一方向的方向上延伸,该移动基本上位于触针尖端的中心。 联接器包括设置在姿态和安装臂的相对面上的突出部和凹部,突出部和凹部被构造为当姿势臂移动到第一和第二姿态中的一个时被配合以约束相对面的相对运动。

    LOAD INDICATOR
    22.
    发明申请
    LOAD INDICATOR 审中-公开
    负载指示器

    公开(公告)号:WO2010055354A4

    公开(公告)日:2011-04-07

    申请号:PCT/GB2009051545

    申请日:2009-11-16

    Inventor: BENNETT IAN

    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,包括一个横向探测器(18),当第一承载构件(10)朝向第二承载构件(11)移动时,该第一承载构件(10)与第一承载构件(10)配合,并继而偏转指示器构件(20) 当超过屈服点时。 对指示器部件的现场检查揭示了它是否弯曲。 指示器构件可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,探头(18)的延伸部(25)可以在过载条件下的中点横向偏转。 或者,探头(18)可在过载条件下在指示器构件(30)中形成印痕。

    MAIN LANDING GEAR WITH RIGID REAR STAY
    23.
    发明申请
    MAIN LANDING GEAR WITH RIGID REAR STAY 审中-公开
    主要着陆齿轮与刚性后方居住

    公开(公告)号:WO2011023980A2

    公开(公告)日:2011-03-03

    申请号:PCT/GB2010051351

    申请日:2010-08-16

    Inventor: BENNETT IAN

    CPC classification number: B64C25/14 B64C25/20 B64C25/34 B64C2025/125

    Abstract: A main landing gear assembly for an aircraft comprising: an elongate beam pivotally coupled about its longitudinal axis to the aircraft such that the axis of rotation of the elongate beam is generally parallel to the longitudinal axis of the aircraft fuselage; a shock strut pivotally coupled at a first end to the elongate beam and coupled at a second end to a wheel assembly; a folding forward stay pivotally coupled at a first end to the elongate beam and pivotally coupled at a second end to the shock strut; and a rigid rear stay pivotally coupled at a first end to the aircraft and pivotally coupled at a second end to the shock strut, the rigid rear stay being arranged to restrain the path of the shock strut when moving between a deployed and a retracted position such that the wheel assembly is located forward and inboard in the retracted position in comparison with its location in the deployed position.

    Abstract translation: 一种用于飞机的主起落架组件,包括:细长梁,所述细长梁围绕其纵向轴线枢转地联接到所述飞行器,使得所述细长梁的旋转轴线大致平行于所述飞机机身的纵向轴线; 减震支柱,所述减震支柱在第一端处枢转地联接到所述细长梁并且在第二端处联接到轮组件; 折叠向前支撑件,其在第一端处可枢转地联接到所述细长梁并且在第二端处可枢转地联接到所述减震支柱; 以及刚性后支柱,其在第一端处枢转地联接到飞机并且在第二端处枢转地联接到减震支柱,刚性后支架布置成当在展开位置和缩回位置之间移动时限制减震支柱的路径, 与其在展开位置中的位置相比,轮组件位于收回位置的前方和内侧。

    EMOTION DETECTION DEVICE & METHOD FOR USE IN DISTRIBUTED SYSTEMS
    25.
    发明申请
    EMOTION DETECTION DEVICE & METHOD FOR USE IN DISTRIBUTED SYSTEMS 审中-公开
    在分布式系统中使用的感应检测装置和方法

    公开(公告)号:WO2007067878A2

    公开(公告)日:2007-06-14

    申请号:PCT/US2006061558

    申请日:2006-12-04

    Inventor: BENNETT IAN

    CPC classification number: G10L15/1822 G06F2203/011 G10L15/30 G10L17/26

    Abstract: A prosody analyzer enhances the interpretation of natural language utterances. The analyzer is distributed over a client/ server architecture, so that the scope of emotion recognition processing tasks can be allocated on a dynamic basis based on processing resources, channel conditions, client loads etc. The partially processed prosodic data can be sent separately or combined -with other speech data from the client device and streamed to a server for a real-time response. Training of the prosody analyzer with real world expected responses improves emotion modeling and the real-time identification of potential features such as emphasis, intent, attitude and semantic meaning in the speaker's utterances.

    Abstract translation: 韵律分析仪增强了对自然语言说话的理解。 分析器通过客户端/服务器架构分布,从而可以基于处理资源,信道条件,客户端负载等动态分配情绪识别处理任务的范围。部分处理的韵律数据可以单独发送或组合 - 与客户端设备的其他语音数据一起流式传输到服务器进行实时响应。 用现实世界预期的反应对韵律分析仪进行训练,改善了情绪建模和实时识别潜在功能,如讲话者话语中的重点,意图,态度和语义。

    LANDING GEAR
    26.
    发明申请
    LANDING GEAR 审中-公开
    起落架

    公开(公告)号:WO2007015104A1

    公开(公告)日:2007-02-08

    申请号:PCT/GB2006/002918

    申请日:2006-08-04

    CPC classification number: B64C25/60 B64C25/22 B64C25/34 B64C25/58

    Abstract: A semi-levered landing gear for an aircraft comprises a main shock absorber strut (1) connected to the airframe; a bogie beam (4) extending fore and aft of the airframe with forward and aft wheels (J, T) and a main pivot connection (5) to the strut (1) between the forward and aft wheels (7, T) and an auxiliary actuator (49) connected between the strut (1) and the front of the bogie beam (4) at an auxiliary pivot (14). The auxiliary actuator (49) comprises a two stage telescopic hydraulic unit comprising a first stage piston and cylinder actuator (59, 63) and a second stage piston and cylinder actuator (56, 50) operating coaxially within an outer casing (50). A respective piston rod (65, 60) each extends from each end of the casing (50) and is connected to a respective one of said (strut 1) and bogie beam (4). The first stage actuator (59, 63) is operable to an extended position, and the second stage actuator (56, 60) is operable between a retracted position (Fig. 11) and an extended position (Fig. 12) defined by respective end stops (75, 77) within the outer casing (50) and serves to control the tilt position of the bogie beam (4) relative to the strut (1). The second stage actuator (56, 60), when in the retracted position with the first stage actuator (59, 63) in the extended position, limits the length of the auxiliary actuator (9) between its connections (62, 67) to the strut (1) and bogie beam (4), so as to assume a predetermined intermediate length in which the bogie beam (4) is restrained to tilt about the auxiliary pivot (14) and thereby lengthens the landing gear during take-off. The second stage actuator (56, 60), when in the extended position with the first stage actuator (59, 63) in the extended position, allows the length of the auxiliary actuator (49) to assume a predetermined maximum length in which the bogie beam (4) is tilted about the main pivot (5) to a stowing position for stowing the landing gear in the aircraft.

    Abstract translation: 用于飞机的半起落架起落架包括连接到机身的主减震器支柱(1); 在前后轮(7,T)和后轮(7,T)之间的支撑件(1)的前后轮(J,T)和主枢轴连接件(5)的前部和后部延伸的转向架梁(4) 辅助致动器(49)在辅助枢轴(14)处连接在支柱(1)和转向架​​梁(4)的前部之间。 辅助致动器(49)包括两级伸缩液压单元,其包括第一级活塞和气缸致动器(59,63)和在外壳(50)内同轴工作的第二级活塞和气缸致动器(56,50)。 相应的活塞杆(65,60)各自从壳体(50)的每个端部延伸并且连接到所述(支柱1)和转向架​​梁(4)中的相应一个。 第一级致动器(59,63)可操作到延伸位置,并且第二级致动器(56,60)可在缩回位置(图11)和由相应端限定的延伸位置(图12)之间操作 在外壳(50)内的止挡(75,77),并用于控制转向架(4)相对于支柱(1)的倾斜位置。 第二级致动器(56,60)当处于处于伸出位置的第一级致动器(59,63)的缩回位置时,将辅助致动器(9)在其连接件(62,67)之间的长度限制到 支柱(1)和转向架​​梁(4),以便呈现预定的中间长度,其中转向架梁(4)被限制在辅助枢轴(14)周围倾斜,从而在起飞期间延长起落架。 第二级致动器(56,60)当处于处于延伸位置的第一级致动器(59,63)的延伸位置时,允许辅助致动器(49)的长度呈现预定的最大长度,其中转向架 梁(4)围绕主枢轴(5)倾斜到收起位置,用于收起飞机上的起落架。

    A SURFACE PROFILING APPARATUS
    27.
    发明申请
    A SURFACE PROFILING APPARATUS 审中-公开
    表面型材设备

    公开(公告)号:WO2004048886A1

    公开(公告)日:2004-06-10

    申请号:PCT/GB2003/005080

    申请日:2003-11-21

    Abstract: Light is directed along a sample path towards the sample surface and along a reference path towards a reference surface such that light reflected by the sample surface and light reflected by the reference surface interfere. Relative movement is effected between the sample surface and the reference surface along a measurement path and the light intensity resulting from interference between light reflected from the reference surface and regions of the sample surface is sensed at intervals along the measurement path to provide a number of sets of light intensity data values with each light intensity data value representing the sensed light intensity associated with a corresponding one of said regions. The sets of light intensity data are processed to determine a position along the measurement path at which a predetermined feature occurs in the light intensity data for each sensed region and to enhance image data representing the intensity data to facilitate the detection by a user of the interference fringes.

    Abstract translation: 光沿取样路径朝向样品表面并沿着参考路径被引向参考表面,使得由样品表面反射的光和被参考表面反射的光干涉。 沿着测量路径在样品表面和参考表面之间进行相对运动,并且沿着测量路径以间隔感测从参考表面反射的光与样品表面的区域之间的干涉产生的光强度,以提供多个组 的光强度数据值,其中每个光强数据值表示与所述区域中的相应一个相关联的感测光强度。 处理光强度数据集合以确定在每个感测区域的光强度数据中发生预定特征的测量路径的位置,并且增强表示强度数据的图像数据,以便于用户检测到干扰 条纹。

    METROLOGICAL APPARATUS
    28.
    发明申请

    公开(公告)号:WO2013027028A2

    公开(公告)日:2013-02-28

    申请号:PCT/GB2012/052007

    申请日:2012-08-16

    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: 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被设置用于相对旋转,夹爪被设置成相对于工件支撑表面移动以使工件在 工件支撑表面,还包括设置成与工件支撑表面一起旋转的细长轴承,支撑夹爪并可沿长形轴承移动的可滑动构件,以及具有与相应可滑动构件和套筒的枢轴连接的连接器,其中相对旋转导致 连接器围绕它们的枢轴连接件枢转,以允许可滑动构件沿着细长轴承的运动以及颚板相对于工件支撑表面的相应运动。

    SPINOUS PROCESS CERCLAGE FOR BONE GRAFT CONTAINMENT
    29.
    发明申请
    SPINOUS PROCESS CERCLAGE FOR BONE GRAFT CONTAINMENT 审中-公开
    用于骨折装置的旋转过程

    公开(公告)号:WO2012154265A1

    公开(公告)日:2012-11-15

    申请号:PCT/US2012/025967

    申请日:2012-02-21

    CPC classification number: A61B17/7053 A61B17/70 A61B17/7062 A61B17/7068

    Abstract: A system for fusing a spine comprises a flexion limiting tether having a superior portion, and an inferior portion. The superior portion of the device is coupled to a superior portion of the spine, and the inferior portion of the device is coupled to an inferior portion of the spine thereby constraining flexion of the spine. The system also includes bone graft for fusing the superior and inferior portions of the spine together. The bone graft is disposed between the superior and inferior portions of the spine, and the tether has a width suitable for holding the bone graft in a mass disposed between the superior and inferior portions of the spine. The tether also has a porosity suitable to allow body fluids to pass therethrough so that the graft material forms a solid mass.

    Abstract translation: 用于定影脊柱的系统包括具有上部的弯曲限制系绳和下部。 装置的上部与脊柱的上部相连,装置的下部与脊柱的下部相连,从而约束脊柱的弯曲。 该系统还包括用于将脊柱的上部和下部融合在一起的骨移植物。 骨移植物设置在脊柱的上下部之间,并且系链具有适于将骨移植物保持在设置在脊柱的上部和下部之间的质量的宽度。 系链还具有适于允许体液通过其的孔隙,使得移植材料形成固体块。

    SOLAR CELL MODULE AND METHOD FOR MANUFACTURING SUCH A MODULE
    30.
    发明申请
    SOLAR CELL MODULE AND METHOD FOR MANUFACTURING SUCH A MODULE 审中-公开
    太阳能电池模块及其制造方法

    公开(公告)号:WO2012015307A1

    公开(公告)日:2012-02-02

    申请号:PCT/NL2011/050547

    申请日:2011-07-29

    CPC classification number: H01L31/022441 H01L31/0516 Y02E10/50

    Abstract: A solar cell module for back-contacted solar cells includes in a layer a number of back- contacted solar cells, placed in an ordered sequence, and a planar contacting means. The planar contacting means is arranged for providing a series connection between respective back contacts of each pair of adjacent solar cells in the ordered sequence, and is a layered connection structure with a first stratum and a second stratum. The first stratum is arranged between the layer of the solar cells and the second stratum. A first pair of adjacent solar cells is connected in series along a first conductive path in the first stratum and one solar cell of the first pair is connected in series to a next adjacent solar cell in the ordered sequence along a second conductive path in the second stratum.

    Abstract translation: 用于背面接触的太阳能电池的太阳能电池模块在一层中包括以有序的顺序放置的多个背接触太阳能电池和平面接触装置。 平面接触装置被布置成以有序的顺序提供每对相邻的太阳能电池的相应的后触点之间的串联连接,并且是具有第一层和第二层的分层连接结构。 第一层布置在太阳能电池层和第二层之间。 第一对相邻的太阳能电池沿着第一层中的第一导电路径串联连接,并且第一对中的一个太阳能电池沿着第二导电路径以有序的顺序串联连接到下一相邻太阳能电池 地层。

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