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    • 72. 发明授权
    • Assembly for connecting multi-duct conduits
    • 用于连接多管道导管的组件
    • US4834825A
    • 1989-05-30
    • US98856
    • 1987-09-21
    • Robert AdamsAndrew J. Cousin
    • Robert AdamsAndrew J. Cousin
    • F16L39/00
    • F16L39/00
    • An assembly for the coupling of a multi-duct conduit system for sealing the outer and inner ducts of adjacent conduit sections in end to end relationship. There is provided a primary coupling housing which includes preferably a premolded body portion which is insertible into the outer most housing of a ducted system. The body system in the body portion comprises first and second half body portions. Each first and second half body portion is adapted to receive a plurality of ducts into bores in the body housing so that a first plurality of ducts enters and is insertible into the body portion at a first end and the second adjoining plurality of duct members are insertible into the body portion on the second end, the first and second portions of ducts being slidably engaged into the body portion and meeting substantially at a center point within the body portion, for defining a continuous pathway within the ducts for housing transmission lines therewithin.
    • 一种用于连接多管道管道系统的组件,用于密封相邻导管段的外管道和内管道的端对端关系。 提供了一种主联接器壳体,其优选地包括可插入到管道系统的外部最外壳中的预制主体部分。 主体部分中的身体系统包括第一和第二半体部分。 每个第一和第二半体部分适于将多个管道容纳在主体壳体中的孔中,使得第一多个管道在第一端处进入并可插入主体部分中,并且第二相邻的多个管道构件可插入 在第二端的主体部分中,管道的第一和第二部分可滑动地接合到主体部分中,并且基本上在主体部分内的中心点处会合,用于在管道内限定用于容纳其中的传输线的连续路径。
    • 73. 发明授权
    • Wide dynamic range microphone
    • 宽动态范围麦克风
    • US09008323B2
    • 2015-04-14
    • US13530227
    • 2012-06-22
    • Olli HailaKieran HarneyGary W. ElkoRobert Adams
    • Olli HailaKieran HarneyGary W. ElkoRobert Adams
    • H03G3/20H04R3/00H04R1/40H04R19/00
    • H04R17/02H04R1/406H04R3/005H04R19/005H04R2430/00H04R2499/11
    • A microphone system has an output and at least a first transducer with a first dynamic range, a second transducer with a second dynamic range different than the first dynamic range, and coupling system to selectively couple the output of one of the first transducer or the second transducer to the system output, depending on the magnitude of the input sound signal, to produce a system with a dynamic range greater than the dynamic range of either individual transducer. A method of operating a microphone system includes detecting whether a transducer output crosses a threshold, and if so then selectively coupling another transducer's output to the system output. Some embodiments combine the outputs of more than one transducer in a weighted sum during transition from one transducer output to another, as a function of time or as a function of the amplitude of the incident audio signal.
    • 麦克风系统具有输出和至少具有第一动态范围的第一换能器,具有与第一动态范围不同的第二动态范围的第二换能器,以及耦合系统以选择性地将第一换能器或第二换能器 换能器到系统输出,取决于输入声音信号的大小,以产生动态范围大于任一单个换能器的动态范围的系统。 操作麦克风系统的方法包括检测换能器输出是否跨越阈值,如果是,则选择性地将另一换能器的输出耦合到系统输出。 作为时间的函数或作为入射音频信号的幅度的函数,一些实施例将来自一个换能器输出的转换期间的多于一个换能器的输出以加权和组合。
    • 78. 发明授权
    • Flight control system and method of using piezoelectric modal sensors to mitigate flexible body dynamics
    • 飞行控制系统和使用压电模态传感器减轻柔性体动力学的方法
    • US07645970B2
    • 2010-01-12
    • US11623196
    • 2007-01-15
    • Robert AdamsWilliam Schwind
    • Robert AdamsWilliam Schwind
    • G05D1/00B64C13/16
    • G05D1/107
    • A flight control system is provided with one or more modal sensors that are each configured to measure the rate and possibly acceleration for a flexible body mode of the flight vehicle. The modal sensor's rate and suitably acceleration are subtracted from the rate and acceleration measured by the IMU such that the values provided to the flight controller more closely represent only the rate and acceleration of the flight vehicle's rigid airframe component. A piezoelectric modal sensor is capable of sensing a particular flexible body mode over variations in the modal frequency without inducing additional phase loss in the control loop in order to maintain suitable phase and gain margins. Sensors are suitably provided for at least and possibly only the 1st lateral bending modes in the pitch and yaw channels.
    • 飞行控制系统设置有一个或多个模态传感器,每个模态传感器被配置为测量飞行器的柔性身体模式的速率和可能的加速度。 从IMU测量的速率和加速度中减去模态传感器的速率和适当的加速度,使得提供给飞行控制器的值更接近地代表飞行器刚性机身部件的速率和加速度。 压电模态传感器能够通过模态频率的变化来感测特定的柔性体模式,而不会在控制回路中引起额外的相位损失,以保持合适的相位和增益余量。 传感器适当地设置在俯仰和偏航通道中的至少和可能仅第一横向弯曲模式。
    • 80. 发明申请
    • Programmable-gain amplifier systems to facilitate low-noise, low-distortion volume control
    • 可编程增益放大器系统,便于低噪声,低失真音量控制
    • US20090091390A1
    • 2009-04-09
    • US12286662
    • 2008-09-30
    • David M. HossackRama ThakarRobert AdamsJoseph Burke
    • David M. HossackRama ThakarRobert AdamsJoseph Burke
    • H03G3/00H03F3/16
    • H03G1/0088H03G3/001
    • Programmable-gain amplifier systems are provided that are particularly suited for reducing degrading audio effects such as zipper noise. In one embodiment, these systems switchably couple an electronic potentiometer between an amplifier's inverting input terminal and interleaved tap points along a resistor that is coupled to the amplifier's output terminal. This arrangement introduces a number of fine gain steps between the gain steps that are realized with adjacent ones of the interleaved tap points to substantially reduce or eliminate zipper noise in a audio system that processes the system's output signal. The interleaved tap points facilitate efficient operation of the potentiometer during gain changes. They also permit the potentiometer to be effectively bypassed between gain changes so that distortion effects are substantially eliminated.
    • 提供了可编程增益放大器系统,其特别适合于减少诸如拉链噪声的降级音频效应。 在一个实施例中,这些系统可将电子电位器在放大器的反相输入端和沿耦合到放大器输出端的电阻的交错抽头之间切换耦合。 这种布置在相邻的交错抽头点实现的增益步骤之间引入了许多精细增益步骤,以显着地减少或消除处理系统输出信号的音频系统中的拉链噪声。 交错的分接点有助于增益变化时电位器的有效运行。 它们还允许在增益变化之间有效地绕过电位器,从而基本上消除了失真效应。