STRUCTURAL ELEMENT FOR A VEHICLE
    3.
    发明申请
    STRUCTURAL ELEMENT FOR A VEHICLE 审中-公开
    车辆的结构元件

    公开(公告)号:WO2006046034A1

    公开(公告)日:2006-05-04

    申请号:PCT/GB2005/004135

    申请日:2005-10-25

    CPC classification number: B62D25/04 B62D29/001

    Abstract: A structural element (20) for a vehicle is disclosed. The element comprises an at least partially transparent body (22), having a three-dimensional array of interconnected chambers arranged to allow light to pass through the body so as to provide at least partial visibility through the element to an occupant of the vehicle when the structural element is mounted in the vehicle. An example of a structural element to which the invention may be applied is a pillar for a car.

    Abstract translation: 公开了一种用于车辆的结构元件(20)。 所述元件包括至少部分透明的主体(22),所述主体具有被连接的互连腔室的三维阵列,其布置成允许光线通过所述主体,以便当所述主体部件 结构元件安装在车辆中。 可应用本发明的结构元件的实例是用于汽车的支柱。

    HEAT SINK
    4.
    发明申请
    HEAT SINK 审中-公开
    散热器

    公开(公告)号:WO2006046022A1

    公开(公告)日:2006-05-04

    申请号:PCT/GB2005/004112

    申请日:2005-10-25

    Abstract: A heat sink for a semiconductor device is disclosed. The heat sink comprises a body of a heat-conducting material, which includes a three-dimensional array of interconnected chambers arranged so that fluid may pass through the body via the chambers. The body further includes a channel for a cooling medium, the channel passing through, but being closed off from, the array of interconnected chambers. The heat sink may be used, for example, in a liquid cooling system for a microprocessor.

    Abstract translation: 公开了一种用于半导体器件的散热器。 散热器包括导热材料体,其包括互连腔室的三维阵列,其布置成使得流体可以经由腔室穿过身体。 该主体还包括用于冷却介质的通道,该通道通过相互连接的腔室阵列而被封闭。 散热器可以用于例如用于微处理器的液体冷却系统中。

    VIEW ENHANCING SYSTEM FOR A VEHICLE
    5.
    发明申请
    VIEW ENHANCING SYSTEM FOR A VEHICLE 审中-公开
    查看车辆增强系统

    公开(公告)号:WO2006027563A1

    公开(公告)日:2006-03-16

    申请号:PCT/GB2005/003423

    申请日:2005-09-06

    Abstract: A view enhancing system for a vehicle is disclosed. The vehicle has a structural element which in normal operation tends to obstruct a vehicle operator's view. The system includes a camera (20, 22, 24) adapted to form an image of a region of the vehicle surroundings where the operator's view is obstructed by the structural element, and display means (52) connected with the camera and mounted on the structural element for displaying an image representing the view that would be seen by the operator if the structural element were transparent or not present. In a disclosed example, the structural element is a pillar. A rear view display system for a vehicle having a camera mounted on the outside of the vehicle adapted to capture an image of a rear view from the vehicle and a rear view mirror including a reflective layer and a display layer is also disclosed.

    Abstract translation: 公开了一种用于车辆的视野增强系统。 车辆具有在正常操作中容易阻碍车辆操作者观察的结构元件。 该系统包括适于形成驾驶员视野被结构元件阻挡的车辆周围区域的图像的照相机(20,22,24)以及与相机连接并安装在结构上的显示装置(52) 元素,用于显示表示如果结构元素是透明的或不存在的,操作者将看到的视图的图像。 在公开的示例中,结构元件是支柱。 还公开了一种用于车辆的后视图显示系统,其具有安装在车辆外部的照相机,其适于捕获来自车辆的后视图的图像和包括反射层和显示层的后视镜。

    PROPROTOR BLADE WITH LEADING EDGE SLOT
    6.
    发明申请
    PROPROTOR BLADE WITH LEADING EDGE SLOT 审中-公开
    带螺旋叶片的螺旋桨叶

    公开(公告)号:WO2004067380A1

    公开(公告)日:2004-08-12

    申请号:PCT/US2003/002049

    申请日:2003-01-23

    CPC classification number: B64C11/16 B64C27/467 B64C29/0033

    Abstract: A proprotor blade (27a, 27b, 127a, 127b) having a fixed, spanwise, leading edge slot (215) located in at least the inboard portion of the proprotor is disclosed. The slot (215) is formed by a selectively shaped slat (217) disposed in a selectively shaped recessed area (219) located at the leading edge (202) of the main portion of the proprotor blade. The slot (215) is selectively shaped so that a portion of the airflow over the lower airfoil surface of the proprotor blade is diverted between the main portion of the proprotor blade and the slat (217) and exits at the upper airfoil surface of the proprotor blade. The present invention may be used on both military-type tiltrotor aircraft (11) and civilian-type tiltrotor aircraft (111) with only minor variations to accommodate the different shapes of the proprotor blades.

    Abstract translation: 公开了一种具有固定的翼展方向的前缘槽(215)的推进器叶片(27a,27b,127a,127b),其位于至少在推进器的内侧部分中。 狭槽215由位于驱动器叶片的主要部分的前缘(202)上的选择性形状的凹入区域(219)中的选择性地成形的板条(217)形成。 狭槽215被选择成形,使得在推进器叶片的下翼面表面上的气流的一部分在推进叶片的主要部分和板条(217)之间转向并在推进器的上翼面上离开 刀。 本发明可以用于军用型倾转旋翼飞机(11)和民用型倾转旋翼飞机(111),只有微小的变化来适应不同形状的推进器叶片。

    HYDRAULIC STOP
    8.
    发明申请
    HYDRAULIC STOP 审中-公开
    液压停止

    公开(公告)号:WO2005039809A1

    公开(公告)日:2005-05-06

    申请号:PCT/GB2004/004354

    申请日:2004-10-15

    Abstract: A hydraulic stop (2) for use in drilling or countersinking operations comprising a rotatable body for rotating a tool (6) about its axis and a cage (20) adapted to contact the surface of a workpiece (8) when the tool has penetrated into the workpiece by a predetermined distance and to actuate a trip mechanism comprising a plungeroperated hydraulic valve (30, 32) as the tool (6) penetrates the workpiece more than the predetermined distance, wherein the plunger (28) is of adjustable length. When actuated the trip mechanism allows the body to shrink in length suddenly. The cage (20) is axially adjustable in relation to the body to set the predetermined depth at which the trip mechanism actuates. Drainage means is provided comprising a plurality of holes spaced around the circumference of the body to which the cage (20) is mounted to allow drainage of coolant whatever the axial position of the cage (20).

    Abstract translation: 一种用于钻孔或锪孔操作的液压停止件(2),包括用于使工具(6)围绕其轴线旋转的可旋转主体和当工具已经穿入时适于接触工件(8)的表面的保持架(20) 工件预定距离并且致动包括作为工具(6)的柱塞式液压阀(30,32)的脱扣机构穿过工件超过预定距离,其中柱塞(28)具有可调整的长度。 当启动时,跳闸机构允许身体突然收缩。 保持架(20)相对于主体可轴向调节以设定脱扣机构致动的预定深度。 提供排水装置,其包括围绕主体的圆周间隔开的多个孔,保持架(20)安装在该圆周上,以允许冷却剂排出,而不管保持架(20)的轴向位置如何。

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