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XC4E Datasheet(PDF) 21 Page - AEROTECH US. ALL RIGHTS RESERVED. |
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XC4E Datasheet(HTML) 21 Page - AEROTECH US. ALL RIGHTS RESERVED. |
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21 / 116 page  XC4e Hardware Manual Chapter 1: Introduction 1.1.1. System Power Requirements The following equations can be used to determine total system power requirements. The actual power required from the mains supply will be the combination of actual motor power (work), motor resistance losses, and efficiency losses in the power electronics or power transformer. Use an EfficiencyFactor of approximately 90% in the following equations. Brushless Motor Output Power Rotary Motors Power Output [W] = Torque [N·m] * Angular velocity[rad/sec] Linear Motors Power Output [W] = Force [N] * Linear velocity[m/sec] Rotary or Linear Motors Power Output [W] = Bemf [V] * I(rms) * 3 Power Loss = 3 * I(rms)^2 * R(line-line)/2 Power Input = (Power Output + Power Loss) / EfficiencyFactor DC Brush Motor Power Output [W] = Torque [N·m] * Angular velocity[rad/sec] Power Loss = I(rms)^2 * R Power Input = (Pout + Ploss) / EfficiencyFactor www.aerotech.com 21 |
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