Inverter Flying Start Control Using DC Ripple Current Estimation

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Solution Overview

Problem

Conventional methods for restarting a high-voltage inverter during a flying start, especially when the counter electromotive force is small, face challenges in accurately analyzing the motor's output current, leading to longer frequency estimation times and potential damage from excessive current noise.

Innovation Solution

The proposed solution involves estimating the motor's rotation speed by analyzing the ripple current resulting from injected DC currents, allowing for quick restarts even when the counter electromotive force is small, using a control device with a rectifying module, smoothing module, inverting module, and detection module, including a current transformer, to manage switching elements and estimate rotation speed based on output currents.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional frequency estimation methods are used when counter electromotive force is small, then the inverter can be restarted, but the frequency estimation time becomes longer

Engineering Contradiction:
Improveflying start capabilityVSAvoidfrequency estimation time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent introduces DC current injection as an intermediary method to enable frequency estimation when conventional counter electromotive force analysis fails. By injecting DC current into the motor during free-running state and analyzing the resulting ripple current, the system can estimate rotation speed even when counter electromotive force is too small for conventional methods, thus resolving the time loss without sacrificing reliability

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent changes the estimation parameter from analyzing counter electromotive force directly to analyzing ripple current generated by DC injection. This parameter change enables frequency estimation in conditions where the original parameter (counter electromotive force) is insufficient, thereby reducing estimation time while maintaining accurate speed detection for reliable flying start

Inventive Principle:
Principle #35Parameter changes

2Loss of time

If DC current injection method is used to estimate rotation speed, then frequency estimation time is reduced, but device complexity increases

Engineering Contradiction:
Improvefrequency estimation timeVSAvoidcontrol device structure
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The control device is designed to perform multiple functions: normal V/f control during steady operation and DC injection-based frequency estimation during flying start. By integrating these functions into a single controller that can switch between operating modes, the patent reduces device complexity compared to having separate systems for each function

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The system performs preliminary DC current injection before the main flying start operation to estimate rotation speed. This preliminary action provides the necessary speed information in advance, enabling the main restart operation to proceed quickly without complex real-time analysis during the critical restart phase

Inventive Principle:
Principle #10Preliminary action

3Reliability

If conventional flying start method is employed when counter electromotive force magnitude is small, then the inverter can be restarted, but excessive current noise occurs

Engineering Contradiction:
Improveinverter restart capabilityVSAvoidexcessive current noise
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent uses feedback from ripple current analysis to estimate motor rotation speed during DC injection. This feedback mechanism allows the control system to accurately determine the motor's actual speed state and adjust the restart parameters accordingly, preventing excessive current noise while ensuring reliable inverter restart

Inventive Principle:
Principle #23Feedback

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach significantly reduces the time required to estimate motor rotation speed, enabling faster inverter restarts and reducing the risk of damage from excessive current noise, with the flying start operation completed within about 10% of the conventional duration.

Implementation Method 1

An inverter is an inverting device that electrically converts DC to AC

Methodology Applied
Scientific EffectInversion (DC to AC conversion):

Implementation Method 2

when a residual counter electromotive force exists in the motor, it is difficult to analyze an output current of the motor

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 3

A direct current or a direct-current voltage is applied to the alternating-current motor in the free running state before it is restarted, and a secondary current, that flows across the rotor of the motor at this time, is employed to estimate the rotational direction and the velocity

Methodology Applied
Scientific EffectRipple current generation:

Data Source

PatentEP3522359B1Device for controlling inverter
Publication Date: 2024.10.09 LSIS CO LTD
  • EP3522359B1 patent drawingFigure 1~2
  • EP3522359B1 patent drawingFigure 3~4
  • EP3522359B1 patent drawingFigure 5~6

AI summary

The present invention relates to an inverter-controlling device. The inverter-controlling device include a main controller configured to generate a predetermined command current; a comparison module configured to calculate a difference between the command current and an output current of an inverting module; a current controller configured to perform a proportional-integral (PI) control based on the difference; and a frequency estimation module configured to estimate a rotation speed of a motor based on a current response to the command current while the command current is injected to the current controller, wherein the main controller is further configured: when a flying start operation of the inverting module begins, to set an output frequency of the inverting module based on the rotation speed of the motor estimated by the frequency estimation module.