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    • 1. 发明公开
    • Aircraft cargo handling
    • 对于飞机货运交通
    • EP1275579A3
    • 2003-06-11
    • EP02077874.2
    • 1996-10-18
    • VICKERS INCORPORATED
    • Swiatlowski, Gerald G.Evans, Richard L.Swartz, Dave
    • B64D9/00
    • B64D9/00B64D2009/006
    • A system and method for loading cargo as cargo units in an aircraft cargo handling system having a cargo loading bay (14) that opens laterally of the aircraft (12) and at least one cargo stowing bay (16,18,20) adjacent to the cargo loading bay (14) longitudinally of the aircraft (12). Two self-erecting power drive units (26,28) are disposed in the cargo loading bay (14) such that the associated rollers are oriented to propel cargo units (24) in orthogonal directions. The two power drive units (26,28) in the loading bay (14) are also disposed adjacent to each other such that, when both are in the erected position, the rollers of each unit simultaneously engage a single overlying cargo unit (24). The power drive units (26,28) may be simultaneously placed in the erected position with the motors de-energized, such that orthogonal orientation of the de-energized drive rollers effectively prevents movement of an overlying cargo unit (24) engaged by both rollers, whereby the cargo unit (24) so engaged is prevented from inadvertent movement out of the loading bay (14). The power drive units (26,28) are equipped with a sensor for detecting when a cargo unit (24) overlies the power drive unit, and a controller is responsive to such sensors for removing power from the power drive units when not in use.
    • 3. 发明公开
    • Aircraft cargo handling
    • 飞机货物处理
    • EP1275579A2
    • 2003-01-15
    • EP02077874.2
    • 1996-10-18
    • VICKERS INCORPORATED
    • Swiatlowski, Gerald G.Evans, Richard L.Swartz, Dave
    • B64D9/00
    • B64D9/00B64D2009/006
    • A system and method for loading cargo as cargo units in an aircraft cargo handling system having a cargo loading bay (14) that opens laterally of the aircraft (12) and at least one cargo stowing bay (16,18,20) adjacent to the cargo loading bay (14) longitudinally of the aircraft (12). Two self-erecting power drive units (26,28) are disposed in the cargo loading bay (14) such that the associated rollers are oriented to propel cargo units (24) in orthogonal directions. The two power drive units (26,28) in the loading bay (14) are also disposed adjacent to each other such that, when both are in the erected position, the rollers of each unit simultaneously engage a single overlying cargo unit (24). The power drive units (26,28) may be simultaneously placed in the erected position with the motors de-energized, such that orthogonal orientation of the de-energized drive rollers effectively prevents movement of an overlying cargo unit (24) engaged by both rollers, whereby the cargo unit (24) so engaged is prevented from inadvertent movement out of the loading bay (14). The power drive units (26,28) are equipped with a sensor for detecting when a cargo unit (24) overlies the power drive unit, and a controller is responsive to such sensors for removing power from the power drive units when not in use.
    • 一种系统和方法,用于将货物作为货物单元装载在飞机货物装卸系统中,所述货物装卸系统具有在飞机(12)的侧面打开的货物装载隔间(14)和至少一个货物装载隔间(16,18,20) (12)纵向的货物装载舱(14)。 两个自立式动力驱动单元(26,28)设置在货物装载隔间(14)中,使得相关联的滚轮定向成沿正交方向推进货物单元(24)。 装载隔间(14)中的两个动力驱动单元(26,28)也彼此相邻布置,使得当两者都处于竖立位置时,每个单元的滚轮同时接合单个上覆的货物单元(24) 。 动力驱动单元(26,28)可以在电动机断电的情况下同时放置在竖立位置,使得断开驱动辊的正交定向有效地防止由两个辊接合的上面的货物单元(24)的移动 由此防止如此接合的货物单元(24)无意地移出装载隔间(14)。 动力驱动单元(26,28)配备有用于检测货物单元(24)何时覆盖动力驱动单元的传感器,并且控制器响应于这些传感器在不使用时从动力驱动单元移除动力。
    • 5. 发明公开
    • Aircraft cargo handling
    • Frachtbeförderungfürein Luftfahrzeug
    • EP0769450A2
    • 1997-04-23
    • EP96307572.6
    • 1996-10-18
    • VICKERS INCORPORATED
    • Evans, Richard L.Swiatlowski, Gerald G.Swartz, Dave
    • B64C1/20B64D9/00
    • B64D9/00B64D2009/006
    • A system and method for loading cargo as cargo units in an aircraft cargo handling system having a cargo loading bay (14) that opens laterally of the aircraft and at least one cargo stowing bay (6) adjacent to the cargo loading bay (18,20) longitudinally of the aircraft. Two self-erecting power drive units (26,28) are disposed in the cargo loading bay such that the associated rollers are oriented to propel cargo units in orthogonal directions. The two power drive units in the loading bay are also disposed adjacent to each other such that, when both are in the erected position, the rollers of each unit simultaneously engage a single overlying cargo unit (24). The power drive units may be simultaneously placed in the erected position with the motors de-energized, such that orthogonal orientation of the de-energized drive rollers effectively prevents movement of an overlying cargo unit engaged by both rollers, whereby the cargo unit so engaged is prevented from inadvertent movement out of the loading bay. The power drive units are equipped with a sensor for detecting when a cargo unit overlies the power drive unit, and a controller is responsive to such sensors for removing power from the power drive units when not in use.
    • 一种用于将货物装载在具有在飞行器侧面打开的货物装载舱(14)和与货物装载舱(18,20)相邻的至少一个货物装载舱(6))的飞行器货物处理系统中的货物装载的系统和方法, )飞机纵向。 两个自立式动力驱动单元(26,28)设置在货物装载舱中,使得相关联的辊定向成在正交方向上推进货物单元。 装载舱中的两个动力驱动单元也彼此相邻设置,使得当两者处于竖立位置时,每个单元的辊同时接合单个上覆的货物单元(24)。 动力驱动单元可以同时放置在竖立位置,同时电动机断电,使得断电驱动辊的正交定向有效地防止由两个辊接合的上层货物单元的运动,由此所接合的货物单元 防止无意中移出装载舱。 动力驱动单元配备有传感器,用于检测货物单元何时覆盖动力驱动单元,并且控制器响应于这种传感器,以在不使用时从动力驱动单元移除动力。