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    • 105. 发明授权
    • Systems and methods of power output measurement
    • 功率输出测量的系统和方法
    • US08122773B2
    • 2012-02-28
    • US12543023
    • 2009-08-18
    • Roland Jeffrey WyattDylan John SeguinRichard Benjamin Knapp
    • Roland Jeffrey WyattDylan John SeguinRichard Benjamin Knapp
    • G01N3/08
    • A61B5/221A61B5/0002A61B5/6807A61B2562/0247G01L3/24
    • The present invention pertains to systems and methods for measuring power output, as in an athletic activity such as cycling. One embodiment relates to a force sensing device configured to be mounted on the bottom surface of a shoe as part of a mechanical linkage through which force is exerted. For cycling, the force sensor is mounted on the bottom surface of a cycling shoe and fitted with a cleat that interlockingly engages a bicycle pedal. To measure both positive and negative pressures on the pedal, the force sensor is pre-stressed with a compressive load to an intermediate point in its dynamic range. Strains that further compress or decompress the force sensor can thus be measured. The computing module mathematically converts the measured pressures, positive and negative, to a measurement of total power exerted by the rider. In addition, the computing module may utilize cyclical regularities in the signal to compute the rider's cadence (pedal revolutions per unit of time). Data from the force sensor is transmitted wirelessly to a remote display where it can be viewed by the rider.
    • 本发明涉及用于测量功率输出的系统和方法,如在诸如骑自行车的运动活动中。 一个实施例涉及一种力传感装置,其被配置为安装在鞋的底表面上,作为施加力的机械连杆的一部分。 对于自行车,力传感器安装在自行车鞋的底部表面上,并装配有与自行车踏板互锁的防滑板。 为了测量踏板上的正压和负压,力传感器在其动态范围内以压缩载荷预压至中间点。 因此可以测量进一步压缩或解压力传感器的菌株。 计算模块将所测量的正压和负压力数学转换为骑手施加的总功率的测量值。 此外,计算模块可以利用信号中的循环规律来计算骑手的节奏(每单位时间的踏板转数)。 来自力传感器的数据被无线传输到远程显示器,可以由骑手观看。
    • 106. 发明授权
    • Power available and limitation indicator for use with an aircraft engine
    • 用于飞机发动机的可用功率和限制指示器
    • US07212942B2
    • 2007-05-01
    • US10459114
    • 2003-06-10
    • Stephen H. Vollum
    • Stephen H. Vollum
    • G01D1/00
    • G01L3/24
    • An instrument for use in a helicopter includes a performance calculator typically housed in a control unit (16) and a display unit (14). The system receives electronic indicia (44) of current altitude, air temperature, fuel on-board and engine manifold pressure, and calculates (in substantially real time) the following: (a) maximum amount of power the engine can produce at these conditions; (b) limitations set by the aircraft manufacturer on power that may be used; (c) maximum airspeed and hover weight allowed under these conditions; (d) percent power used (the “torque gauge”); and (e) amount of power remaining available. The power display unit has an arcuate series (24) of light elements fitted around the standard MP (20) gauge to provide graphic indicia (26, 28, 30) of power available for the pilot to easily see and interpret.
    • 用于直升机的仪器包括通常容纳在控制单元(16)和显示单元(14)中的性能计算器。 该系统接收当前高度,空气温度,车上燃料和发动机歧管压力的电子标记(44),并计算(基本上实时地)以下内容:(a)发动机在这些条件下可产生的最大功率; (b)飞机制造商对可能使用的电力设定的限制; (c)在这些条件下允许的最大空速和悬停重量; (d)所使用的功率百分比(“扭矩计”); 和(e)剩余的电量。 功率显示单元具有安装在标准MP(20)计量器周围的弧形系列(24)的光元件,以提供可用于驾驶员容易看到和解释的电力的图形标记(26,28,30)。
    • 108. 发明授权
    • Display unit for displaying the output of a vehicle engine
    • 用于显示车辆发动机的输出的显示单元
    • US5259241A
    • 1993-11-09
    • US781148
    • 1991-12-31
    • Atsuo Wakayama
    • Atsuo Wakayama
    • G01L5/00F02D45/00G01L3/24
    • G01L3/24
    • A display unit for displaying the output of a vehicle engine measures and displays the output or torque of the engine during a normal running state.The unit calculates and displays the output of the engine according to an intake air quantity and engine rotational speed. The unit calculates an output for a predetermined steady run corresponding to a present vehicle speed. If the engine output calculated according to the intake air quantity and rotational speed is smaller than the steady-run output, the unit displays zeros.
    • PCT No.PCT / JP91 / 00682 Sec。 371日期1991年12月31日 102(e)日期1991年12月31日PCT 1991年5月22日PCT PCT。 公开号WO91 / 18270 日期:1991年11月28日。用于显示车辆引擎的输出的显示单元在正常行驶状态期间测量并显示发动机的输出或扭矩。 该单元根据进气量和发动机转速来计算和显示发动机的输出。 该单元计算与当前车辆速度相对应的预定稳定运行的输出。 如果根据进气量和转速计算的发动机输出小于稳定输出,则单位显示零。
    • 109. 发明授权
    • Shaft torque measurement
    • 轴扭矩测量
    • US5067355A
    • 1991-11-26
    • US552393
    • 1990-07-13
    • James R. Witte
    • James R. Witte
    • G01L3/10G01L3/24G01L5/26G01P3/56
    • G01L5/26G01L3/109G01L3/24G01P3/565
    • A method and apparatus for determining the power output of a gas turbine engine utilizes a speed sensor coupled to the engine shaft and a signal developed by a pyrometer coupled to the engine turbine for determining engine temperature. The speed sensor is normally provided in the engine for determining shaft speed and is part of the control system for the engine. The pyrometer is provided also as part of the control system to monitor gas turbine temperatures. A signal from the speed sensor derived from a toothed wheel passing adjacent the sensor is processed to obtain a train of pulse signals representative of angular rotation of the engine shaft. The pyrometer is mounted adjacent at least one of the turbine disks of the engine for detecting instantaneous temperature of each blade of the turbine disk as it passes by the pyrometer. The signal developed by the pyrometer is therefore a signal having peaks corresponding to passage of each blade at the pyrometer. A signal conditioning apparatus processes the signal from the pyrometer to develop a pulse train of shaped signals corresponding to the angular position of each turbine blade as it passes by the pyrometer. The system determines the relative phase difference between the signals developed by the speed sensor and the signals developed on the pyrometer under low load conditions and stores this information as a reference phase difference value. Phase differences under load conditions are thereafter compared to the reference value. The differences in phase are proportional to shaft twist and accordingly to shaft torque.
    • 用于确定燃气涡轮发动机的功率输出的方法和装置利用耦合到发动机轴的速度传感器和由耦合到发动机涡轮机的高温计开发的信号来确定发动机温度。 发动机通常设置速度传感器以确定轴速度,并且是用于发动机的控制系统的一部分。 高温计还作为监测燃气轮机温度的控制系统的一部分。 来自通过邻近传感器的齿轮的速度传感器的信号被处理以获得表示发动机轴的角度旋转的一串脉冲信号。 高温计安装在发动机的涡轮盘的至少一个附近,用于检测涡轮盘在通过高温计时的每个叶片的瞬时温度。 因此,由高温计开发的信号是具有对应于高温计处的每个叶片通过的峰值的信号。 信号调节装置处理来自高温计的信号,以形成对应于每个涡轮叶片在通过高温计的角位置时成形信号的脉冲串。 该系统确定由速度传感器开发的信号与在低负载条件下在高温计上开发的信号之间的相对相位差,并将该信息存储为参考相位差值。 此后将负载条件下的相位差与参考值进行比较。 相位差与轴扭转成正比,并与轴转矩成比例。