عنوان

Analysis and design of power converter topologies for application in future more electric aircraft /

(Number (ISBN

9789811082139

(Number (ISBN

9811082138

Erroneous ISBN

9789811082122

Erroneous ISBN

981108212X

Title Proper

Analysis and design of power converter topologies for application in future more electric aircraft /

General Material Designation

[Book]

First Statement of Responsibility

Amit Kumar Singh.

Place of Publication, Distribution, etc.

Singapore :

Name of Publisher, Distributor, etc.

Springer,

Date of Publication, Distribution, etc.

2018.

Specific Material Designation and Extent of Item

1 online resource (xxxiv, 188 pages) :

Other Physical Details

illustrations (some color)

Series Title

Springer theses,

ISSN of Series

2190-5053

Text of Note

"Doctoral thesis accepted by the National University of Singapore, Singapore."

Text of Note

Includes bibliographical references.

Text of Note

Intro; Supervisor's Foreword; Parts of this thesis have been published in the following articles:JournalsA. K. Singh, E. Jeyasankar, P. Das and S.K. Panda, "A Matrix Based Non-isolated Three Phase AC-DC Rectifier With Large Step Down Voltage Gain," in IEEE Transactions on Power Electronics, vol. 32, no. 6, pp. 4796-4811, June 2017. (Published)A. K. Singh, E. Jeyasankar, P. Das, S. Panda, "A Single-Stage Matrix Based Isolated Three Phase AC-DC Converter with Novel Current Commutation," in IEEE Transactions on Transportation ; Acknowledgements; Declaration; Contents; Acronyms; List of Figures.

Text of Note

2.5 Steady State Analysis and Design2.5.1 Voltage Gain of the Converter; 2.5.2 Voltage Stresses; 2.5.3 Current Stresses; 2.5.4 Estimation of the Input and Output Voltage/Current Ripple for the Proposed Matrix Based AC-DC Converter; 2.5.5 Filter Design; 2.5.6 Effect of Modulation Index (m) on the THD of the Input Line Current; 2.6 Simulation of the Proposed Converter; 2.7 Closed Loop Control of the Proposed Converter; 2.7.1 Small Signal Modelling of the Proposed Converter; 2.7.2 Closed Loop Controller Design; 2.7.3 Simulation Result; 2.8 Comparative Loss Evaluation of the Proposed Converter.

Text of Note

2.8.1 Semiconductor Losses in the Proposed Converter2.8.2 Semiconductor Losses in the Traditional Six Switch Buck Rectifier; 2.8.3 Snubber Loss in the Proposed Converter and Six Switch Buck Rectifier; 2.8.4 Comparison of the Semiconductor Losses in the Proposed and the Traditional Six Switch Buck Rectifier; 2.9 Experimental Verification; 2.9.1 Prototype and Structure; 2.9.2 Controller; 2.9.3 Experimental Results; 2.10 Benchmarking of the Proposed Converter; 2.11 Conclusion; References; 3 A Matrix Based Isolated Three Phase AC-DC Converter; 3.1 Introduction.

Text of Note

3.2 Brief Review of the Isolated AC-DC Converter3.3 New Contribution of the Chapter; 3.4 Topology and Principle of Operation; 3.5 Steady State Analysis and Design; 3.5.1 Derivation of the Output Voltage of the Proposed Converter; 3.5.2 Voltage Stress/Current Stress of the Converter; 3.5.3 Magnetics Design; 3.5.4 Effect of Adding Series Capacitor and Its Design Consideration; 3.6 Simulation of the Proposed Converter; 3.7 Digital Implementation of the Proposed SVM Based ... ; 3.7.1 DSP Implementation; 3.7.2 FPGA Implementation; 3.8 Experimental Verification; 3.8.1 Experimental Results.

Text of Note

List of TablesSummary; 1 Introduction; 1.1 Aircraft System; 1.1.1 Electrical Power System in Commercial Aircrafts; 1.1.2 DC -- DC Converter for Military Aircraft; 1.2 Objective and New Contributions of This Work; 1.3 Outline of the Thesis; 1.4 Conclusion; References; 2 A Matrix Based Non-isolated Three Phase AC-DC Converter; 2.1 Introduction; 2.2 A Brief Review of Three Phase Non-isolated Buck Rectifier; 2.3 New Contributions of the Chapter; 2.4 Topology, Modulation Scheme and Principle of Operation; 2.4.1 Assumptions; 2.4.2 Modulation Scheme; 2.4.3 Modes of Operation.

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Text of Note

This thesis proposes new power converter topologies suitable for aircraft systems. It also proposes both AC-DC and DC-DC types of converters for different electrical loads to improve the performance these systems. To increase fuel efficiency and reduce environmental impacts, less efficient non-electrical aircraft systems are being replaced by electrical systems. However, more electrical systems requires more electrical power to be generated in the aircraft. The increased consumption of electrical power in both civil and military aircrafts has necessitated the use of more efficient electrical power conversion technologies. This book presents acomprehensive mathematical analysis and the design and digital simulation of the power converters. Subsequently it discusses the construction of the hardware prototypes of each converter and the experimental tests carried out to verify the benefits of the proposed solutions in comparison to the existing solutions.

Source for Acquisition/Subscription Address

Springer Nature

Stock Number

com.springer.onix.9789811082139

Title

Analysis and design of power converter topologies for application in future more electric aircraft.

International Standard Book Number

9789811082122

Electric current converters.

Hybrid electric airplanes.

Electric current converters.

Hybrid electric airplanes.

TECHNOLOGY & ENGINEERING-- Mechanical.

TEC-- 009070

TH

Number

Edition

Class number

Singh, Amit Kumar

Date of Transaction

20200823222415.0

Cataloguing Rules (Descriptive Conventions))

pn

Electronic name

[Book]

Y