推挽式的英文

• push pull
• push-pull mode
• push-pull type

• "推挽"英文翻译    push-pull
• "式"英文翻译    type; style
• "推拉式；推挽式" 英文翻译 :    push-pull
• "推挽式的" 英文翻译 :    push pull; push-pull
• "推挽式声道" 英文翻译 :    push-pull sound track
• "推挽式声迹" 英文翻译 :    push-pull recording track; push-pull track
• "推挽式输出" 英文翻译 :    output pushpulll; output, push-pull; pushpull outputt
• "推挽式变换器，推挽式变频器" 英文翻译 :    push-pull converter
• "推挽式倍频器" 英文翻译 :    push-pull multiplier
• "推挽式变换器" 英文翻译 :    pushpull converterr
• "推挽式变频器" 英文翻译 :    pushpull converterr
• "推挽式铲运机" 英文翻译 :    push-pull scraper
• "推挽式传声器" 英文翻译 :    push pull microphone; push-pull microphone
• "推挽式的连接" 英文翻译 :    push-pull
• "推挽式放大器" 英文翻译 :    amplifier, push-pull; push-pull amplifier
• "推挽式光电管" 英文翻译 :    push pull photocell; push-pull photocell
• "推挽式检波器" 英文翻译 :    push pull detector
• "推挽式连接器" 英文翻译 :    push-pull co ector; push-pull connector
• "推挽式驱动器" 英文翻译 :    push-pull driver
• "推挽式渗透泵" 英文翻译 :    push-pull osmotic pump
• "推挽式振荡器" 英文翻译 :    push-pull oscillator
• "推挽式整流器" 英文翻译 :    push pull rectifier; push-pull rectifier
• "磁力推挽式放大器" 英文翻译 :    magnetic push-pull amplifier; magneticpush-pull amplifier
• "甲类推挽式声迹" 英文翻译 :    classa pushpull sound track
• "推挽式磁放大器" 英文翻译 :    push-pull magnetic amplifier

• Aircraft - general purpose push - pull single - pole circuit - breakers - dimensions
  飞行器.通用推挽式单极电路断路器.尺寸
• Aircraft - general purpose push - pull single - pole circuit - breakers - performance requirements
  飞行器.通用推挽式单极电路断路器.性能要求
• The experiment verified the validity that push - pull class - e amplifier is more suitable for high frequency high - power inverter
  通过实验对比，推挽式双e类放大器更适合高频大功率的开发研制。
• Comparing with usual push - pull converter , the bias - magnetic can be retrained due to the clamping capacitance . but bias - magnetic can not be avoided
  推挽正激变换器相比普通的推挽式变换器,由于箝位电容的存在,偏磁可以被抑制,但并不能完全消除。
• At last , a test for the 2 - x actuator has been performed , in which the static and dynamic output of the actuator has been tested to examine the design
  对推挽式双x驱动器进行了原理性试验研究,测试推挽式双x驱动器的静态和动态输出,检验设计方案的合理性。
• The push - pull mode switch power supply is chosen as the main circuit of the other voltages with pwm control circuit , over - current protection circuit , insulated drive circuit , mosfet buffer circuit and so on
  采用高效的推挽式电路作为中低压电源的主电路，并以pwm控制电路、隔离式驱动电路、过流保护电路、 mosfet缓冲电路、软启动电路、稳压电路等作为辅助电路。
• After that , the static and dynamic properties of the actuator has been studied , the dynamic equation has been modeled . through the analysis , we can see the 2 - x actuator can provide the bidirectional force and displacement
  对于推挽式双x驱动器,初步分析了其静态和动态力学性能,建立相应的动力学方程,从理论上求证了推挽式双x驱动器能够提供双向的作用力和位移输出。
• Experiment result proved , relative to complicated structure and hig h request for laying wiring of zvs series resonant full - bridges , push - pull class - e amplifier is expected more suited for high frequency high - power output ability relatively , which is suitable for popularizing
  实验证明，相对于结构复杂，布线要求较高的全桥串联谐振逆变器，推挽式双e类放大器具有更高频率和较大功率的输出能力，适于推广一。
• Grounding on above theory , the zvs resonant of soft switch full - bridges circuit , and class - e amplifier , and push - pull class - e amplifier are analyzed respectively in theory . push - pull class - e amplifier is available by comparing results of simulation and low power experiment
  基于以上理论，分别选择了zvs谐振型全桥串联逆变器、 e类放大器以及推挽式e类放大器进行详细的理论分析，仿真比较以及小功率实验对照。
• In addition , the dynamic equation of the rotor with trailing edges and the 2 - x actuator has been modeled for analyzing the aerodynamic performance of the rotor . the result of the analysis tells us that the performance of the rotor with trailing edges can get a remarkable improvement
  进而研究旋翼动力学模型,将推挽式双x驱动器模型作为后缘附翼的一种驱动机构,分析旋翼的气动性能,仿真运算结果表明,后缘附翼智能桨叶在各方面的性能都有显著的提高。