XC4E datasheet(21/116 Pages) AEROTECH

No. de pieza	XC4E

Descripción Electrónicos	HARDWARE MANUAL

PDF	116 Pages

Scroll/Zoom	100%

Fabricante Electrónico	AEROTECH [AEROTECH US. ALL RIGHTS RESERVED.]

Página de inicio	https://www.aerotech.com/

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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

XC4E Datasheet(PDF) 21 Page - AEROTECH US. ALL RIGHTS RESERVED.