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21 条记录 (耗时 0.018 秒)

    Dual impeller pump
    8.
    发明授权
    Dual impeller pump 失效
    双叶轮泵

    公开(公告)号：US4732236A

    公开(公告)日：1988-03-22

    申请号：US852773

    申请日：1986-04-16

    申请人： David L. Jacques

    发明人： David L. Jacques

    IPC分类号： F04D29/22 ,  F04D1/00 ,  F04D29/06 ,  F01M11/06

    CPC分类号： F04D29/06 ,  F04D1/006

    摘要： A liquid scavenging pump system for scavenging oil or the like from a blower, an engine or the like. A casing is provided for housing the blower and defining an oil receiving cavity. A dual pump is mounted in the casing and has first and second pumps in communication with the casing cavity for conjoint rotation. A first inlet is provided from the casing cavity to the first pump, and a first outlet is provided from the first pump for delivering oil from the cavity to a pump or the like. A second inlet is provided from the casing cavity, remote from the first inlet, to the second pump. The second outlet from the second pump is in communication with the first inlet to the first pump to facilitate operating the pump at various attitudes. The dual pump is of the radial-vaned impeller type, but includes two sets of axially spaced impeller vanes separated by a common barrier and including a sleeve for mounting on a common drive shaft. The impeller vanes, the barrier and the sleeve all are fabricated as a single unitarily constructed structure, such as by molding.

    摘要翻译： 一种用于从鼓风机，发动机等中清除油等的液体清除泵系统。 提供了用于容纳鼓风机并限定油接收腔的壳体。 双泵安装在壳体中，并且具有与壳体腔连通的第一和第二泵，用于联合旋转。 从壳体腔向第一泵提供第一入口，并且从第一泵提供第一出口，用于将油从空腔输送到泵等。 第二入口从壳体空腔提供，远离第一入口到第二泵。 来自第二泵的第二出口与第一泵的第一入口连通，以便以各种姿态操作泵。 双泵是径向叶轮类型的，但是包括两组轴向隔开的叶轮叶片，它们由公共挡板分开并且包括用于安装在公共驱动轴上的套筒。 叶轮叶片，阻挡件和套筒都被制造为单一的整体结构，例如通过模制。

    AIRCRAFT EMERGENCY POWER SYSTEM
    9.
    发明申请
    AIRCRAFT EMERGENCY POWER SYSTEM 审中-公开
    飞机紧急动力系统

    公开(公告)号：US20130076120A1

    公开(公告)日：2013-03-28

    申请号：US13036968

    申请日：2011-02-28

    申请人： Carl A. Wagner ,  Michael Krenz ,  David L. Jacques

    发明人： Carl A. Wagner ,  Michael Krenz ,  David L. Jacques

    IPC分类号： B64D33/00

    CPC分类号： B64D33/00 ,  B64D2221/00 ,  F01D15/10 ,  F05D2270/09

    摘要： An emergency power system for use on an aircraft includes an emergency electrical generator coupled to a mechanical power source for generating emergency electrical power. An electrical power distribution network connects the emergency electrical generator to a plurality of electrical loads. A controller controls the electrical power distribution network to selectively couple and decouple the electrical loads to and from the emergency electrical generator based upon a priority rank assigned to each of the electrical loads.

    摘要翻译： 用于飞行器的应急电力系统包括耦合到用于产生应急电力的机械电源的紧急发电机。 电力分配网络将紧急发电机连接到多个电负载。 控制器控制配电网络，以便基于分配给每个电负载的优先等级来选择性地将电力负载耦合到紧急发电机和从紧急发电机分离。