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    • 4. 发明公开
    • VEHICLE SEAT
    • 车辆座椅
    • EP2630004A1
    • 2013-08-28
    • EP11772925.1
    • 2011-10-13
    • BAE Systems PLC
    • HOYLE, James, Brooks
    • B60N2/20B60N2/32F41H1/00B60N2/30
    • B60N2/02B60N2/20B60N2/32B60N2002/247B60N2205/30
    • A seat for a vehicle is provided. The seat is configured such that an occupant can be seated in either a lower position or in an upper position. The seat comprises a base member for accommodating an occupant in the lower position and a seat back, positioned to extend generally upwards from the region of the base member. The seat back is configured to accommodate an occupant's back. A selectively deployable perch member is also provided. The seat member has two deployment conditions. In a first condition, the perch member is configured as an extension of the seat back for when the occupant is seated in the lower position. In a second condition, the perch member is configured as an additional base member for supporting an occupant in the upper position. A fastening is provided for securing the perch member when it is in the second condition.
    • 提供车辆的座位。 座椅被配置成使得乘客可以坐在较低位置或较高位置。 座椅包括用于容纳处于下部位置的乘客的基部构件和座椅靠背,所述座椅定位成从基部构件的区域大致向上延伸。 座椅靠背配置为容纳乘客的背部。 还提供了可选择性展开的栖木部件。 座椅构件有两种展开条件。 在第一种情况下,栖木部件构造成座椅靠背的延伸部分,用于当乘员坐在下部位置时。 在第二种情况下,栖木部件构造成用于支撑处于上部位置的乘员的附加基座部件。 当处于第二状态时,提供用于固定栖木部件的紧固件。
    • 6. 发明授权
    • METHOD AND APPARATUS FOR DEFEATING HIGH-VELOCITY PROJECTILES
    • 方法和设备,可以提供高转速弹
    • EP1135663B1
    • 2006-02-15
    • EP99970856.3
    • 1999-11-09
    • Pinnacle Armor, LLC.
    • Neal, Murray L.Bain, Allan D.
    • F41H1/00
    • B32B3/10B32B9/005B32B9/047B32B2571/00F41H5/0435F41H5/0464F41H5/0492
    • A method and apparatus for defeating high-velocity projectiles. A plurality of disks (52) of equal size and having a thickness greater than 0.100 " are milled in a plurality of places (54, 56, 58). Each milled place having a radius of curvature approximately equal to the radius of curvature of the disk. The disks are then laid out in an imbricated pattern row by row such that each disk in a row is in substantially a straight line with the other disks in the row and overlaps a milled place of a disk in a row above its row and has its milled place overlapped by a disk in the row below its row. The imbricated pattern is then adhered to a flexible, high tensile strength substrate (80) and overlaid by a second high tensile strength layer (82) such that the imbricated pattern is enveloped between the substrate and the second layer. The envelope is then coupled to a soft body armor backing. In an alternative embodiment, a method and apparatus for defeating high-velocity projectiles. A plurality of disks (152) of equal size comprised of fiber induced ceramic composites are provided. The disks are laid out in an imbricated pattern row by row such that each disk in a row is in substantially a straight line with the other disks in the row and overlaps a segment of a disk in an adjacent row. The imbricated pattern is then adhered to a flexible, high tensile strength substrate and overlaid by a second high tensile strength layer such that the imbricated pattern is enveloped between the substrate and the second layer. The envelope is then coupled to a soft body armor backing.