Design of an Integrated Inductor for 45kW Aerospace Starter-Generator

M. Raza Khowja; C. Gerada; G. Vakil; S. Quadir Quadri; P. Wheeler; C. Patel

doi:10.1109/ITEC.2018.8450246

Design of an Integrated Inductor for 45kW Aerospace Starter-Generator

M. Raza Khowja
, C. Gerada
, G. Vakil
, S. Quadir Quadri
, P. Wheeler
, C. Patel

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

6 Citations (Scopus)

Abstract

A close physical and functional integration of passive components is required to make an efficient and power dense overall system. Such power dense systems are a prerequisite in aerospace and marine applications. This paper presents a design of an integrated rotor-less inductor for the application of a 45kW aerospace starter-generator. The impact of high current density inductor is investigated and compared with traditional EE core inductor in terms of total weight and volume. Both inductors are sized using area product approach and its design parameters are validated using finite element analysis. Comparative analysis between the traditional EE core and the integrated inductor has shown a significant reduction in total weight and volume. The total weight ofthe integrated inductor is reduced by 55.4% whereas the total volume is reduced by 52.7% when compared to traditional air cooled EE core inductor.

Original language	English
Title of host publication	2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	353-358
Number of pages	6
ISBN (Print)	9781538630488
DOIs	https://doi.org/10.1109/ITEC.2018.8450246
Publication status	Published - 28 Aug 2018
Event	2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018 - Long Beach, United States Duration: 13 Jun 2018 → 15 Jun 2018

Publication series

Name	2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018

Conference

Conference	2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018
Country/Territory	United States
City	Long Beach
Period	13/06/18 → 15/06/18

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

SDG 14 Life Below Water

Free Keywords

Aerospace Applications and Starter-Generator
EE Core Inductor
Integrated Inductors
Integration of Passives
Rotor-less Inductor

ASJC Scopus subject areas

Energy Engineering and Power Technology
Electrical and Electronic Engineering
Transportation

Access to Document

10.1109/ITEC.2018.8450246

Cite this

Raza Khowja, M., Gerada, C., Vakil, G., Quadir Quadri, S., Wheeler, P., & Patel, C. (2018). Design of an Integrated Inductor for 45kW Aerospace Starter-Generator. In 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018 (pp. 353-358). Article 8450246 (2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ITEC.2018.8450246

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title = "Design of an Integrated Inductor for 45kW Aerospace Starter-Generator",

abstract = "A close physical and functional integration of passive components is required to make an efficient and power dense overall system. Such power dense systems are a prerequisite in aerospace and marine applications. This paper presents a design of an integrated rotor-less inductor for the application of a 45kW aerospace starter-generator. The impact of high current density inductor is investigated and compared with traditional EE core inductor in terms of total weight and volume. Both inductors are sized using area product approach and its design parameters are validated using finite element analysis. Comparative analysis between the traditional EE core and the integrated inductor has shown a significant reduction in total weight and volume. The total weight ofthe integrated inductor is reduced by 55.4\% whereas the total volume is reduced by 52.7\% when compared to traditional air cooled EE core inductor.",

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Raza Khowja, M, Gerada, C, Vakil, G, Quadir Quadri, S, Wheeler, P & Patel, C 2018, Design of an Integrated Inductor for 45kW Aerospace Starter-Generator. in 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018., 8450246, 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018, Institute of Electrical and Electronics Engineers Inc., pp. 353-358, 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018, Long Beach, United States, 13/06/18. https://doi.org/10.1109/ITEC.2018.8450246

Design of an Integrated Inductor for 45kW Aerospace Starter-Generator. / Raza Khowja, M.; Gerada, C.; Vakil, G. et al.
2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018. Institute of Electrical and Electronics Engineers Inc., 2018. p. 353-358 8450246 (2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018).

Research output: Chapter in Book/Conference proceeding › Conference contribution › peer-review

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AU - Raza Khowja, M.

AU - Gerada, C.

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AU - Wheeler, P.

AU - Patel, C.

PY - 2018/8/28

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N2 - A close physical and functional integration of passive components is required to make an efficient and power dense overall system. Such power dense systems are a prerequisite in aerospace and marine applications. This paper presents a design of an integrated rotor-less inductor for the application of a 45kW aerospace starter-generator. The impact of high current density inductor is investigated and compared with traditional EE core inductor in terms of total weight and volume. Both inductors are sized using area product approach and its design parameters are validated using finite element analysis. Comparative analysis between the traditional EE core and the integrated inductor has shown a significant reduction in total weight and volume. The total weight ofthe integrated inductor is reduced by 55.4% whereas the total volume is reduced by 52.7% when compared to traditional air cooled EE core inductor.

AB - A close physical and functional integration of passive components is required to make an efficient and power dense overall system. Such power dense systems are a prerequisite in aerospace and marine applications. This paper presents a design of an integrated rotor-less inductor for the application of a 45kW aerospace starter-generator. The impact of high current density inductor is investigated and compared with traditional EE core inductor in terms of total weight and volume. Both inductors are sized using area product approach and its design parameters are validated using finite element analysis. Comparative analysis between the traditional EE core and the integrated inductor has shown a significant reduction in total weight and volume. The total weight ofthe integrated inductor is reduced by 55.4% whereas the total volume is reduced by 52.7% when compared to traditional air cooled EE core inductor.

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KW - Integration of Passives

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ER -

Raza Khowja M, Gerada C, Vakil G, Quadir Quadri S, Wheeler P, Patel C. Design of an Integrated Inductor for 45kW Aerospace Starter-Generator. In 2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018. Institute of Electrical and Electronics Engineers Inc. 2018. p. 353-358. 8450246. (2018 IEEE Transportation and Electrification Conference and Expo, ITEC 2018). doi: 10.1109/ITEC.2018.8450246

Design of an Integrated Inductor for 45kW Aerospace Starter-Generator

Abstract

Publication series

Conference

UN SDGs

Free Keywords

ASJC Scopus subject areas

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