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    • 75. 发明授权
    • Rotary head drum apparatus and magnetic recording and playback apparatus
    • 旋转磁鼓设备和磁记录播放装置
    • US06771471B2
    • 2004-08-03
    • US10057559
    • 2002-01-25
    • Motoyoshi FujimoriIchiro HashimotoAkira ItouHiroyuki Kaneko
    • Motoyoshi FujimoriIchiro HashimotoAkira ItouHiroyuki Kaneko
    • G11B502
    • G11B5/584
    • A rotary head drum apparatus and a magnetic recording and playback apparatus wherein crosstalk between a writing signal and a playback signal transferred using independent rotary transformers is reduced and facility of assembly and rework of a magnetic head are improved. A flat disk-type rotary transformer for a writing signal and another flat disk-type rotary transformer for a playback signal are disposed adjacently in a stationary drum, and a shield plate for preventing crosstalk is interposed between the two rotary transformers. Alternatively, one of a writing rotary transformer and a playback rotary transformer is formed from a flat disk-type rotary transformer while the other is formed from a cylindrical rotary transformer, and the flat disk-type rotary transformer is disposed on a bottom portion of a stationary drum while the cylindrical rotary transformer is disposed on an outer circumference of a center boss of the stationary drum.
    • 一种旋转磁头鼓装置和磁记录和重放装置,其中,使用独立旋转变压器传送的写入信号和重放信号之间的串扰减小,并且提高了磁头的装配和返工的可能性。 用于写入信号的平盘式旋转变压器和用于重放信号的另一平盘式旋转变压器相邻设置在固定的滚筒中,并且用于防止串扰的屏蔽板插入在两个旋转变压器之间。 替代地,一种书写旋转变压器和回放式旋转变压器由平盘式旋转变压器形成,而另一个由圆柱形旋转变压器形成,平盘式旋转变压器设置在 而圆柱形旋转变压器设置在固定鼓的中心凸台的外圆周上。
    • 77. 发明授权
    • Aircraft flight and voice data recorder system and method
    • 飞机飞行和语音数据记录系统及方法
    • US06735505B2
    • 2004-05-11
    • US10052202
    • 2002-01-17
    • Howard B. Levine
    • Howard B. Levine
    • G11B502
    • G07C5/085B64D45/00B64D2045/0065G07C5/008H04B7/18506
    • An onboard portion of the system is located on an aircraft for monitoring a plurality of flight parameters and detecting a predetermined exceedence indicative of a potential problem. With regard to flight data, predetermined exceedences could include abnormal attitude, control surface actuator failure, low hydraulic fluid pressure, low fuel, near stall speed, excessive engine RPM, engine failure, cabin pressure loss, and so forth. With regard to voice data, predetermined exceedences could include excessive decibel levels, excessive static, overly long periods of silence, and other audible conditions indicative of cockpit intrusion. Flight data representative of the flight parameters is transmitted via RF signals upon the detection of the predetermined exceedence. A remote portion of the system receives the transmitted RF signals carrying the flight data and records the flight data for analysis.
    • 系统的车载部分位于飞行器上用于监视多个飞行参数并检测指示潜在问题的预定超限。 对于飞行数据,预定的超越可能包括异常姿态,控制面致动器故障,低液压流体压力,低燃料,近失速速度,过大的发动机转速,发动机故障,机舱压力损失等。 关于语音数据,预定的超越可能包括过高的分贝级别,过多的静态,超长时间的沉默以及其他表示驾驶舱入侵的可听状况。 在检测到预定的超限之后,通过RF信号来传送代表飞行参数的飞行数据。 系统的远程部分接收携带飞行数据的发射的RF信号,并记录飞行数据进行分析。