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    • 36. 发明申请
    • Head and neck restraint system
    • 头颈部约束系统
    • US20060260027A1
    • 2006-11-23
    • US11439493
    • 2006-05-22
    • Carrol RhodesJason SmithGary BradleyPhillip Hawkins
    • Carrol RhodesJason SmithGary BradleyPhillip Hawkins
    • A42B7/00B62J1/28
    • B64D10/00A42B3/0473A62B35/00B60R22/00B60R22/001B64D25/02
    • A head and neck restraint system includes a headpiece, a saddle, and tensioners connecting the headpiece to the saddle. The headpiece resides on top of a crew member's head and the saddle includes a saddle strap residing under the crew member's buttocks. The tensioners are pneumatic muscles which contract when a flow of gas is provided by gas generators. The gas generators are triggered by a G-sensor or by the initiation of a predetermined event. Triggering signals pass through a manifold from an ejection seat, aircraft, or vehicle. Contraction of the pneumatic muscles pulls the headpiece toward the saddle, thereby restraining the head, neck, and spine. The system is worn as an undergarment or incorporated into a garment. A manual adjustment provides head support during flight. The system is particularly useful for preventing head and neck injuries during ejection from or crash of an aircraft or vehicle
    • 头颈部约束系统包括将头盔连接到鞍座上的头盔,鞍座和张紧器。 头盔位于船员头部的顶部,鞍座包括住在船员臀部下方的马鞍皮带。 张紧器是当气体发生器提供气体流时收缩的气动肌肉。 气体发生器由G传感器触发或通过启动预定事件。 触发信号通过歧管从喷射座,飞机或车辆。 气动肌肉的收缩将头盔朝向鞍座拉动,从而限制头部,颈部和脊柱。 该系统作为内衣穿戴或并入服装中。 手动调整在飞行中提供头部支撑。 该系统特别有用于防止在飞行器或车辆弹出或碰撞期间的头部和颈部受伤