Back to Search Start Over

A Hybrid Seven-Level Dual-Inverter Scheme With Reduced Switch Count and Increased Linear Modulation Range.

Authors :
Pal, Souradeep
Gopakumar, K.
Loganathan, Umanand
Abu-Rub, Haitham
Zielinski, Dariusz
Source :
IEEE Aerospace & Electronic Systems; Feb2023, Vol. 38 Issue 2, p2013-2021, 9p
Publication Year :
2023

Abstract

This work presents a hybrid seven-level dual inverter scheme with increased linear modulation range. The hybrid inverter structure is formed by supplying the load from primary side by using a cascaded structure of a two-level inverter and H-bridge (HB) and secondary side of the load is supplied by a floating-capacitor-fed two-level inverter. The combination of primary two-level space vector structure (SVS) with secondary two-level SVS and primary three-level SVS of HB form a seven-level SVS that can further be extended to an eight-level hexagonal SVS. This structure then reduced to a 12-sided eight-level SVS to avoid exceeding motor phase voltage rating. Subsequently by using this eight-level SVS in an unique pulsewidth modulation mode, the proposed topology can increase the modulation range linearly from $0.577V_{\text{dc}}$ to $0.637V_{\text{dc}}$ peak phase fundamental voltage for any load power factor (pf), where dc-link voltage is $V_{\text{dc}}$. An 11 $\%$ increase in modulation range ($0.637V_{\text{dc}}/0.577V_{\text{dc}}$) is possible devoid of lower order harmonics (predominantly $5{\text{th}}$ , $7{\text{th}}$ , $11{\text{th}}$ , $13{\text{th}}$ , etc.) in phase voltage for unity pf load in comparison to the conventional six-step operation of two-level and multilevel hexagonal SVS. To balance HB capacitors voltages in this work, a concept of indirect space vector redundancy is used. The efficacy of the proposed inverter scheme is verified through various experimental results at different steady-state and transient conditions. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
08858985
Volume :
38
Issue :
2
Database :
Complementary Index
Journal :
IEEE Aerospace & Electronic Systems
Publication Type :
Academic Journal
Accession number :
160686201
Full Text :
https://doi.org/10.1109/TPEL.2022.3217439