HYDRAULIC FUEL PUMP APPARATUS FOR A FUEL DELIVERY CHASSIS, SUITABLE FOR REFUELING AIRCRAFT, AND RELATED DEVICES, SYSTEMS AND METHODS
    1.
    发明申请
    HYDRAULIC FUEL PUMP APPARATUS FOR A FUEL DELIVERY CHASSIS, SUITABLE FOR REFUELING AIRCRAFT, AND RELATED DEVICES, SYSTEMS AND METHODS 审中-公开
    用于燃料输送管理的液压燃油泵装置,适用于修理飞机,以及相关设备,系统和方法

    公开(公告)号:US20140257579A1

    公开(公告)日:2014-09-11

    申请号:US14204691

    申请日:2014-03-11

    Abstract: Embodiments include a modular fuel pump apparatus for an aircraft refueling chassis and related devices, systems and methods. In one exemplary embodiment, a pump module includes a hydraulic motor driven by a hydraulic pump connected to a chassis motor. A chassis engine is operated at a substantially constant RPM, which causes the hydraulic pump to output hydraulic fluid to the pump module at a substantially constant hydraulic pressure. The speed of the hydraulic motor can be varied by a proportional flow control valve disposed between the hydraulic pump and the hydraulic motor, thereby varying the speed of the fuel pump and the flow rate of the fuel. A controller is configured to operate the pressure control valve such that the flow of the fuel is maintained at a predetermined flow rate.

    Abstract translation: 实施例包括用于飞机加油底盘和相关装置,系统和方法的模块化燃料泵装置。 在一个示例性实施例中,泵模块包括由连接到底盘马达的液压泵驱动的液压马达。 底盘发动机以基本恒定的RPM操作,这使得液压泵以基本上恒定的液压压力将液压流体输出到泵模块。 液压马达的速度可以通过设置在液压泵和液压马达之间的比例流量控制阀来改变,由此改变燃料泵的速度和燃料的流量。 控制器被配置为操作压力控制阀,使得燃料的流量保持在预定流量。

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