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    • 1. 发明申请
    • Belt tension indicator
    • 皮带张力指示器
    • US20070114774A1
    • 2007-05-24
    • US10596581
    • 2004-12-17
    • Heinz-Jurgen LangHermann WetterDavid Carine
    • Heinz-Jurgen LangHermann WetterDavid Carine
    • B60R22/00
    • B60N2/2809B60N2/2806B60N2002/2815B60R22/28B60R22/48B60R2022/286B60R2022/287B60R2022/4841
    • A tension detector has a flexible strap (350) having its end stitched into a loop (352) that wraps round a central shaft (354). A U-shaped one-piece coil spring has two coiled end portions (356) and (358) wrapped round the shaft (354). The end portions (356) and (358) are inter-connected by a central stirrup (360). A tether strap (316) has a loop (362) sewn into its end which engages round the stirrup (360). The ends of the shaft (354) are journalled in side walls of a housing (366). Each side wall has an inwardly direct abutment projection (368). The upper surface of the housing (366) includes a window (370) through which an arcuate indicator (372) is visible. The indicator (372) has side legs (374) and (376) that are slidably mounted on the stirrup (360). When the strap (316) is relaxed, the left hand end of the arcuate indicator (372) is visible through the window (370). When the strap (316) is tightened, the arcuate indicator (372) pivots to the position shown in FIG. 11 in which its right hand end, which is of a different color to its left hand end, is visible through the window (370), indicating that the strap (316) has been tightened adequately. In the event of a crash, the coiled end portions (356) and (358) of the spring over-ride the abutment projections (368) and partially unwrap from the shaft (354) so that an extended stirrup portion (360) projects from the housing (366).
    • 张力检测器具有柔性带(350),其具有端部缝合成环绕中心轴(354)的环(352)。 U形一体式螺旋弹簧具有缠绕在轴(354)上的两个螺旋端部(356)和(358)。 端部(356)和(358)通过中心箍筋(360)相互连接。 绳带(316)具有缝合到其末端的环(362),其围绕马镫(360)接合。 轴(354)的端部被轴颈安装在壳体(366)的侧壁中。 每个侧壁具有向内直接的邻接突起(368)。 壳体(366)的上表面包括窗口(370),弧形指示器(372)可以通过该窗口可见。 指示器(372)具有可滑动地安装在马镫(360)上的侧腿(374)和(376)。 当带(316)松弛时,弓形指示器(372)的左手端通过窗口(370)可见。 当带子(316)被紧固时,弓形指示器(372)枢转到图6中所示的位置。 其中其右手端与其左手端具有不同的颜色,通过窗口(370)可见,指示带(316)已经被充分地拧紧。 在碰撞的情况下,弹簧的螺旋端部(356)和(358)超过邻接突起(368)并且部分地从轴(354)展开,使得延伸的箍筋部分(360)从 壳体(366)。
    • 2. 发明申请
    • Safety Seat
    • 安全座椅
    • US20070222262A1
    • 2007-09-27
    • US10598855
    • 2005-03-11
    • David Carine
    • David Carine
    • B60N2/48
    • B60N2/885B60N2/888
    • A deformable, polypropylene-moulding lining (11), is provided in a head rest. It has a crosspiece (12), clipped (14) to the head support (5) and right and left deformable wings (15, 16). These are longer than the support wings (5, 6) of the head part (4), extending past distal edges (17) of the support wings. The deformable wings are spaced inwards from the support wings, with voids (18) defined between them. The deformable wings are divided into two in their forwards extent by a living hinge (19) into a front portion (20) and a rear portion (21). The living hinge is positioned just inside the distal edges of the shell wings. The injection moulded lining has its own foam materiel lining (22), the whole being covered with upholstery (23). The result of the arrangement is that if an occupant's head H impacts the lining in side impact of the vehicle equipped with the seat, the relevant lining wing will be pressed against the shell wing. This involves energy absorbing (maximum acceleration limiting) deformation of not only the foam material, but also of the lining wing and to a less extent of the shell wing. With the lining wing deformation (24), the front portion (20) of the lining wing pivots forwards about the shell edge (17), from a position swept back with respect to the shell wing to a position generally in line with the compressed inner portion of the lining.
    • 在头枕中提供可变形的聚丙烯成型衬里(11)。 它具有横档(12),夹头(14)到头部支撑件(5)和左右可变形机翼(15,16)。 它们比头部(4)的支撑翼(5,6)更长,延伸穿过支撑翼的远侧边缘(17)。 可变形翼片与支撑翼片间隔开,其间限定有空隙(18)。 可变形翼片通过活动铰链(19)在其向前的范围内被分成两部分,分成前部(20)和后部(21)。 活动铰链位于壳翼的远侧边缘的内侧。 注塑衬里有自己的泡沫材料衬里(22),整个被覆盖了室内装饰(23)。 安排的结果是,如果乘客的头部H撞击配备有座椅的车辆的侧面碰撞中的衬里,则相关的衬里翼将被压靠在壳翼上。 这涉及不仅泡沫材料的能量吸收(最大加速度限制)变形,而且还涉及衬里翼的能量吸收(最大加速度限制)变形以及壳翼的较小程度。 随着衬里翼变形(24),衬里翼的前部(20)围绕壳边缘(17)从相对于壳翼向后扫掠的位置向前枢转到与压缩内部 内衬的一部分。