• 空气缸体执行机构所采用机械弹簧可以达到20,000推力最大14英寸的冲程限制,主要取决于需要输出推力

    Mechanical springs used with air cylinders can be sized for up to 20,000 Ibs. of thrust and have a stroke limit of about 14 "max. depending on thrust output required."

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  • 推力限制解释了为什么总是适当使用最大直径最大限度地输出扭矩

    The thrust limitation explains why it is always appropriate to use the maximum diameter available to maximize output torque.

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  • 必定有人提出反对意见显然封闭系统不能输出对外的推力产生应变波导墙壁

    The inevitable objection raised, is that the apparently closed system produced by this arrangement cannot result in an output force, but will merely produce strain within the waveguide walls.

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  • 术语效率”是扬声器系统电能(功放推力)转化为声音输出能力

    The term "efficiency" refers to the ability of a speaker system to convert electrical energy (power from the amplifier) into acoustic output.

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  • 范围实现级调速,可输出较大推力和较大力矩

    Can be achieved within a wide range of stepless speed regulation, can output a larger and larger torque thrust.

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  • 产生电压同时,导体受到阻力(反作用力),推力转化成电能输出

    Produce voltage at the same time, by conductor resistance (reaction), namely thrust power into electricity output.

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  • 认为满足螺旋桨额定推力为目的,推进电动机需要低速输出额定转实现,即输出功率较低

    In order to satisfy the operation requirement of the rated thrust of the propeller, the propulsion motor performs only in rated torque on the low speed, so the motor power is low.

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  • 扭力输出特大推力轴承

    High twisting force output, the huge thrust bearing;

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  • 根据姿态控制推力输出特性设计了轨道控制期间卫星姿态控制方案。

    The attitude control law is designed for the orbital maneuver with considering the output character of the attitude control thrusters.

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  • 经济性好:由于G800螺杆泵专用减速机,输出结构设计承受螺杆泵工作时轴向推力所以可以减少泵类的轴承座部件,不仅省成本而且结构可靠合理。

    Economy: because of the special design of the G800 mechanical reducer with screw pump, the bearing housing parts can be reduced. Thus, the cost is reduced and the structure is more reliable.

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  • 此外由于控制输出方波,因而适合卫星喷气推力器控制模式飞轮控制模式,最后通过数字仿真验证了方波序列控制的有效性

    Moreover, it is very suitable to satellite systems equipped with on off jets and reaction wheels. Finally, numeric simulation is explored to verify the validity of pulse sequence control.

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  • 此外由于控制输出方波,因而适合卫星喷气推力器控制模式飞轮控制模式,最后通过数字仿真验证了方波序列控制的有效性

    Moreover, it is very suitable to satellite systems equipped with on off jets and reaction wheels. Finally, numeric simulation is explored to verify the validity of pulse sequence control.

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