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    • 1. 发明申请
    • HIGH THROUGHPUT MULTI-CHANNEL ROTATING DISK OR RING-DISK ELECTRODE ASSEMBLY AND METHOD
    • 高通道多通道旋转盘或环形电极组件及方法
    • WO2005057162A2
    • 2005-06-23
    • PCT/US2004/026555
    • 2004-08-16
    • HONDA MOTOR CO., LTD.HE, Ting
    • HE, Ting
    • G01N
    • G01N27/403
    • An electrochemical cell assembly including a plurality of testing cells, a reference cell, and fluid connections between the testing cells and the reference cell. Each of the testing cells includes a working electrode, which is a rotating disk or ring-disk electrode, and a counter electrode. A chemical composition, whose intrinsic kinetic properties under defined mass-transfer are to be investigated, is deposited on the working electrode. The reference cell holds a reference electrode that serves as a common reference electrode for each of the testing cells. The assembly permits simultaneous testing of many chemical compositions under identical environment.
    • 包括多个测试单元,参考单元以及测试单元和参考单元之间的流体连接的电化学电池组件。 每个测试单元包括作为旋转盘或环形盘电极的工作电极和对电极。 将研究在其中规定的质量传递下的内在动力学性质的化学组成物沉积在工作电极上。 参考单元保持用作每个测试单元的公共参考电极的参考电极。 组件允许在相同环境下同时测试许多化学成分。
    • 9. 发明申请
    • HYDRAULIC SYSTEM FOR AIRCRAFT
    • 航空液压系统
    • WO2009124027A1
    • 2009-10-08
    • PCT/US2009/038921
    • 2009-03-31
    • HONDA MOTOR CO., LTD.OYAMA, Hiroki
    • OYAMA, Hiroki
    • B64C13/42
    • F15B1/022F15B20/004F15B2211/212F15B2211/8633F15B2211/8757
    • A hydraulic system for aircraft operating devices provides a secondary pressure source for direction and deceleration control in case of loss of pressure from a primary pressure source. The system includes multiple pressure accumulators that include a primary accumulator, which supplies pressurized fluid to a first actuator, and first and second secondary accumulators, which supply pressurized fluid to second and third actuators, respectively. If the primary accumulator is disabled, the first secondary accumulator will supply pressurized fluid to the first actuator. If the first secondary accumulator is disabled, the second secondary accumulator will supply pressurized fluid to the second actuator. By providing multiple, substantially independent accumulators, direction and deceleration control is maintained even in the event of loss of the primary accumulator.
    • 用于飞机操作装置的液压系统在来自主压力源的压力损失的情况下提供用于方向和减速控制的二次压力源。 该系统包括多个压力蓄能器,其包括向第一致动器供应加压流体的主蓄能器,以及分别向第二和第三致动器供应加压流体的第一和第二次级蓄能器。 如果主蓄能器被禁用,则第一副蓄能器将向第一致动器供给加压流体。 如果第一次级蓄能器被禁用,则第二辅助蓄能器将向第二致动器供应加压流体。 通过提供多个基本独立的蓄能器,即使在主蓄能器损失的情况下也能够保持方向和减速控制。