• No results found

Ultrafast Direct Current Protection Systems for Faster Fault Isolation in Multi-terminal LVDC and MVDC Distribution.

N/A
N/A
Protected

Academic year: 2020

Share "Ultrafast Direct Current Protection Systems for Faster Fault Isolation in Multi-terminal LVDC and MVDC Distribution."

Copied!
148
0
0

Loading.... (view fulltext now)

Full text

(1)

ABSTRACT

MACKEY, LANDON KENT. Ultrafast Direct Current Protection Systems for Faster Fault Isolation in Multi-terminal LVDC and MVDC Distribution. (Under the direction of Dr. Iqbal Husain.)

Energy has quickly risen to be one of the key factors affecting modern society. Finite resources of

fossil fuels contribute to pollution, destabilization, and climate change. The energy sector is making

efforts to shift heating and transportation to electric energy from carbon based fuels while shifting the

generation of electricity from the conventional centralized, fossil fuel and nuclear heavy system

towards more distributed and renewable energy means. Many emerging technologies in distributed

renewable energy are non-synchronous or direct current in nature. The proliferation of power

semiconductors and power electronics allows cost effective and efficient voltage manipulation in direct

current that was not available at the dawn of the modern electric system, which relied on the

wire-wound transformer for voltage transformation. Despite these advancements, the great challenge

facing direct current distribution systems is providing safe, fast, efficient, and affordable protection

systems to maintain system stability and isolate faults. Direct current protection systems must isolate

faults without the aid of a natural current zero crossing, without consuming large amounts of energy,

and on a sub-millisecond timescale. The focus of this doctoral study and research project is to explore

direct current system dynamics during fault, review available technologies, identify viable protection

topologies, and design new methods of safety interrupting medium voltage direct current faults. This

study revealed many elements that are necessary for effective isolation of direct current faults, primarily

the ability to appropriately manage the surge energy and to provide isolation fast enough to prevent

voltage collapse in power electronic converter dominated distribution systems. Direct current faults

have been characterized using analytical analysis of fault condition, computer simulation software, and

testing of grid connected converters in the laboratory. The resulting characteristics provided the basis

for the list of requirements for developed medium voltage direct current circuit breakers. Circuit

breaker designs were simulated using computer models such as PLECS, PSCAD, COMSOL, Matlab and

Simulink and testing in the laboratory using functional test prototypes at both reduced scale and full

power capacity. It is found that each of the reviewed circuit breaker topologies studied, designed, and

(2)

most efficient, yet operates too slowly and cannot quench a drawn electrical arc alone. The resonant

circuit breaker is the lowest cost and highly efficient, however is limited to overcurrent fault isolation.

The solid-state circuit breaker is highly controllable; the fastest of all designs, yet consumes significant

power and requires active cooling while in operation. Finally, the hybrid circuit breaker is highly

efficient, fast enough to prevent voltage collapse, and controllable for all fault conditions, however is

the most expensive of available topologies. As a result of this research, a new type of hybrid direct

current circuit breaker has been designed, and is currently under second generation development for

medium voltage applications. The so-called Progressively Switched Hybrid Circuit Breaker is a

bidirectional full function circuit breaker that minimizes the surge on the power system, limits fault

current during shutdown, and ensures maximum efficiency during operation. A scalable medium

voltage second-generation circuit breaker is under development with aims of isolating faults between

(3)

© Copyright 2019 by Landon Kent Mackey

(4)

Ultrafast Direct Current Protection Systems for Faster Fault Isolation in Multi-terminal LVDC and MVDC Distribution

by

Landon Kent Mackey

A dissertation submitted to the Graduate Faculty of North Carolina State University

in partial fulfillment of the requirements for the Degree of

Doctor of Philosophy

Electrical Engineering

Raleigh, North Carolina

2019

APPROVED BY:

Dr. Srdjan Lukic Dr. Leonard White

Dr. Gregory Buckner Dr. Iqbal Husain

(5)

DEDICATION

This work is dedicated to all those who are working diligently to make this world a better place for

(6)

BIOGRAPHY

The author was born in Michigan, USA. He received the Bachelor of Science degree in Electrical

Engineering with a concentration on Renewable Electrical Energy Systems (REES) and the Master of

Science in Electrical Power Systems Engineering from North Carolina State University, Raleigh, USA in

2015 and 2016 respectively. Since January of 2017 he has been pursueing the Doctorate of Philosophy in

Electrical Engineering at North Carolina State University at the Future Renewable Electric Energy

Delivery and Management (FREEDM) Systems Center, Raleigh, USA.

He began his work in the direct current (DC) microgrid field during six years of military service in

the United States Navy where he operated and maintained the nuclear power plant of a Los Angeles

class nuclear fast attack submarine. Throughout his education he continued to pursue experience

outside of the classroom through internships at ABB Corporate Research Center, Dättwil, Aargau,

Switzerland developing a next generation Modular Multilevel Converter testing platform, and at Ford

Motor Company, Dearborn, Michigan, USA developing dc fast charge integration systems for battery

electric vehicles. He participated in undergraduate research under the guidance of Dr. Iqbal Husain

during the final year of his B.S. degree researching Future Smart DC Distribution Grids, and worked

with industry sponsor Pos-En ® to develop a Modular Energy Generator for deployment in Costa Rica

to support critical infrastructure. Throughout graduate school he has mentored undergraduate

students and peers, worked with advocacy groups of under-represented minorities in the sciences,

served on several student leadership boards, and project teams to maintain active involvement with

and provide support to his community.

His research interests include developing technologies and system which promote the

integration of distributed renewable energy resources to the electric grid, or developing islanded direct

current microgrids supplied by renewable energy. Future goals in the field include continued

contribution towards the next generation electric grid including smart grid, a direct current electric

(7)

ACKNOWLEDGEMENTS

Thank you to all of my friends, family, and colleagues who have supported me through my journey of

life. I especially thank Dr. Iqbal Husain for seeing my potential, and investing in my future. Your

mentorship and guidance has been instrumental in my accomplishments, and have helped to develop

me into the man I am today.

I would also like to thank coffee for waking me up, beer for calming me down, and backpacking

(8)

TABLE OF CONTENTS

LIST OF TABLES . . . ix

LIST OF FIGURES. . . x

TERMINOLOGY . . . xv

Chapter 1 Low and Medium Voltage Direct Current Multi-terminal Distribution and Pro-tection . . . 1

1.1 Introduction . . . 1

1.2 Global Trends Toward the Adoption of Direct Current Systems . . . 2

1.3 Advantages of Direct Current Distribution . . . 3

1.3.1 Low Voltage Direct Current Applications . . . 5

1.3.2 High Voltage Direct Current Transmission . . . 6

1.3.3 Islanded and Non-conventional DC Distribution Systems . . . 6

1.4 Challenge of Protecting Direct Current Systems . . . 7

1.4.1 Interruption Speed . . . 7

1.4.2 Absence of a Current Zero-Crossing . . . 8

1.4.3 Organization of Subsequent Chapters . . . 10

Chapter 2 DC Circuit Protection Technologies: A Review of Proposed Topologies . . . 11

2.1 Existing Solutions for Protecting Direct Current Systems . . . 11

2.2 DC Circuit Breakers . . . 12

2.2.1 Mechanical Circuit Breakers . . . 13

2.2.2 Resonant Style Circuit Breakers . . . 13

2.2.3 Solid-State Circuit Breakers . . . 15

2.2.4 Hybrid Circuit Breakers . . . 16

2.3 Medium Voltage Direct Current Distribution Protection . . . 17

(9)

Chapter 3 Active Damping and Advanced Control of a Thomson Coil Actuated Ultrafast

Me-chanical Switch . . . 19

3.1 Thomson coil actuated ultrafast mechanical switches for hybrid DC circuit breaker . . . 19

3.2 Reclosing issue with passive damping mechanism . . . 23

3.3 Proposed active damping for Thomson coil actuated switches . . . 24

3.4 Design of the active damping control . . . 28

3.5 Experimental tests of active damping . . . 30

3.5.1 Test Setup . . . 31

3.5.2 Measurement and Control of Test Setup . . . 31

3.5.3 Comparison of COMSOL simulation with test results . . . 33

3.5.4 Contribution of opening voltage . . . 35

3.5.5 Contribution of damping voltage . . . 38

3.5.6 Contribution of damping pulse timing . . . 39

3.6 Lessons Learned . . . 41

3.7 Conclusions . . . 42

Chapter 4 Design and Optimization of a Mechanically Switched Z-Source Resonant DCCB . . 44

4.1 Introduction . . . 44

4.1.1 Background of Z-Source Circuit Breakers . . . 45

4.1.2 Background of Ultrafast Mechanical Switches . . . 47

4.2 Circuit Breaker Design . . . 47

4.2.1 Simulation . . . 48

4.2.2 Analytical Assessment . . . 49

4.2.3 Test Bench Experimentation . . . 51

4.3 Comparison of Simulation, Analytical and Experimental Platforms . . . 54

4.4 Result and Analysis . . . 55

4.5 Preliminary Design Conclusions . . . 57

4.6 Background of the Z-Source Topology . . . 58

(10)

4.7 Mechanically Switched Z-Source DCCB . . . 59

4.7.1 Efficiency Improvement with Mechanically Switches . . . 61

4.7.2 Arcing Challenge in DC Mechanical Switches . . . 62

4.8 Analysis of System Response and Simulation . . . 64

4.8.1 System Dynamics During Bolted Fault . . . 64

4.8.2 System Dynamics During Step Change in Load . . . 67

4.9 Mechanically Switched Z-Source Design . . . 68

4.9.1 Zero-Crossing Time Calculation . . . 68

4.9.2 Component Optimization . . . 69

4.9.3 Control and Protection Logic . . . 71

4.10 Simulation and Prototype Results . . . 73

4.10.1 Simulation Validation . . . 73

4.10.2 Experimental Test Prototype Results . . . 74

4.10.3 Comparison with Other DCCBs . . . 76

4.11 Conclusion . . . 77

Chapter 5 Progressively Switched Solid-State and Hybrid Direct Current Circuit Breakers. . 79

5.1 Introduction . . . 79

5.2 DC Fault Characteristics . . . 81

5.3 Progressively Switched Solid-State DCCB . . . 83

5.3.1 Progressively Switched DCCB Design . . . 84

5.3.2 Progressively Switched DCCB Capabilities . . . 85

5.3.3 Progressively Switched DCCB Test Prototype . . . 87

5.4 Results . . . 87

5.4.1 Two-Stage Progressively Switched DCCB Results . . . 88

5.4.2 Four-Stage Progressively Switched DCCB Results . . . 88

5.4.3 Validation of Computer Model with Test Prototype . . . 91

5.5 Solid-State Circuit Breaker Conclusions . . . 92

(11)

5.7 DC Protection . . . 93

5.7.1 DC Distribution Fault Characterization . . . 93

5.7.2 Isolation Speed Challenge with Hybrid DCCBs . . . 95

5.8 Proposed Progressive Switching of Hybrid DCCBs . . . 96

5.9 Prototype Design . . . 102

5.9.1 Progressively Switched Main Breaker . . . 102

5.9.2 Actively Damped Ultrafast Mechanical Switch . . . 103

5.9.3 Modular Commutating Switch . . . 105

5.9.4 Integrated Sensing, Communication, and Breaker Controls . . . 106

5.10 Experimental Results . . . 107

5.11 Conclusions and Summary . . . 108

Chapter 6 Conclusions and Future Work - Scalability of Progressively Switched Hybrid Cir-cuit Breakers . . . .111

6.1 Scalability of Progressive Main Breakers . . . 111

6.2 Laboratory Scaling of the Progressively Switched DCCB Prototype . . . 112

6.3 Scalability Considerations . . . 114

6.3.1 Presspack Solid-State Switches and Puck Style MOVs . . . 114

6.3.2 Radial Lead Solid-State Switches and Radial Lead MOVs . . . 115

6.3.3 Module Topology Solid-State Switches and Module MOVs . . . 116

(12)

LIST OF TABLES

Table 3.1 Combinations of opening voltages, damping voltages and damping delays tested. 31

Table 4.1 Experimental Setup Parameters. . . 52

Table 4.2 Circuit Breaker Design and Test Parameters . . . 60

Table 4.3 Mechanical Switch Compared to Thyristor . . . 62

Table 4.4 Mechanical Switch Test Parameters . . . 63

Table 4.5 Comparison of Analytical and Simulation Models . . . 67

Table 4.6 Simulation Results for LS y s=2.5 mH, LE Q =10 mH and CE Q=190µF . . . 73

Table 4.7 Simulation Results for LS y s=1 mH, LE Q =10 mH and CE Q=190µF . . . 73

Table 4.8 Experimental Test Results . . . 76

Table 5.1 Four-Stage Progressive DCCB Parameters . . . 88

Table 5.2 Dielectric Strength of UFMS . . . 105

Table 5.3 Progressively switched hybrid DCCB parameters . . . 109

(13)

LIST OF FIGURES

Figure 1.1 Illustration of the global trend towards DC systems. . . 2

Figure 1.2 Many conversion steps between centralized generation and end consumer. . . . 3

Figure 1.3 A DC microgrid interconnected to the legacy AC grid and a DC microgrid. . . 4

Figure 1.4 Rapid voltage collapse of a DC distribution system compared to AC system. . . . 8

Figure 1.5 AC fault with a repetitive current-zero crossing facilitating fault isolation. . . 9

Figure 1.6 Direct current, pulsating, and variable current sources do not guarantee a current zero crossing. . . 10

Figure 2.1 Oscillatory mechanical circuit breaker. . . 14

Figure 2.2 Resonant style circuit breaker. . . 14

Figure 2.3 Solid-state circuit breaker. . . 16

Figure 2.4 Hybrid circuit breaker. . . 17

Figure 3.1 A hybrid DC circuit breaker (DCCB). . . 20

Figure 3.2 Diagram of the Thomson coil actuator based fast mechanical switch. . . 21

Figure 3.3 Design of the ultrafast mechanical switch. . . 22

Figure 3.4 The ultrafast mechanical switch prototype. The based plate is approximately 30 cm by 30 cm. . . 23

Figure 3.5 Successful opening driven by 400 V. . . 24

Figure 3.6 Opening driven by 420 V followed by a reclosing. . . 25

Figure 3.7 Multiphyics interaction in the actuator. . . 26

Figure 3.8 3D view of the FEM model. . . 26

Figure 3.9 Induced current in the disc, 60µs after energizing the opening coil, simulation in axisymmetric 2D view. . . 27

Figure 3.10 Induced current in the disc, 440µs after energizing the damping coil, simulation in axisymmetric 2D view. . . 27

(14)

Figure 3.12 Driving force (from 0 to 2 ms) and damping forces (from 2 to 4 ms), simulation

results. . . 29

Figure 3.13 Speed and displacement curves corresponding to Fig. 3.12 forces, simulation

results. . . 30

Figure 3.14 Test setup of the active damping method. . . 32

Figure 3.15 Opening operations with varying opening voltages and damping delays with a

damping voltage of 322 V. . . 32

Figure 3.16 Opening operations with varying opening voltages and damping delays with a

damping voltage of 345 V. . . 33

Figure 3.17 Measurement and control diagram of the Thomson coil actuated, actively

dam-ped, ultrafast mechanical switch. . . 34

Figure 3.18 Comparison of Experimental test-bench results to COMSOL simulated results. . 35

Figure 3.19 UFMS motion for various opening voltages, with 2.0 ms damping delay and 322

V damping voltage. . . 36

Figure 3.20 UFMS motion for various opening voltages, with 2.0 ms damping delay and 345

V damping voltage. . . 37

Figure 3.21 UFMS motion for various opening voltages, with 3.0 ms damping delay and 322

V damping voltage. . . 37

Figure 3.22 UFMS motion for various opening voltages, with 3.0 ms damping delay and 345

V damping voltage. . . 38

Figure 3.23 UFMS motion for various opening and damping voltages, with 3.0 ms delay. . . . 39

Figure 3.24 UFMS motion for various damping pulse timings with 430 V opening voltage and

322 V damping voltage. . . 40

Figure 3.25 UFMS motion for various damping pulse timings with 430 V opening voltage and

345 V damping voltage. . . 40

Figure 3.26 UFMS velocity pattern for various opening voltages, with 2.0 ms damping delay

and 322 V damping voltage . . . 41

Figure 3.27 UFMS velocity pattern for various opening voltages, with 3.0 ms damping delay

(15)

Figure 4.1 Z-Source Circuit Breaker Circuit Diagram . . . 46

Figure 4.2 FREEDM Systems Center Ultra-Fast Mechanical Switch Prototype (IEEE 2016) . 48 Figure 4.3 Simulation setup in PSCAD . . . 49

Figure 4.4 Voltage and current profile of UFMS (top) and energy absorbed and current inrush to MOV (bottom). . . 50

Figure 4.5 Current ripple and voltage ripple induced in the fast mechanical switch and impedance network during fault condition. . . 50

Figure 4.6 Z-Source Circuit Breaker Simplified Analytical Schematic . . . 51

Figure 4.7 Z-Source Circuit Breaker Test Bench Prototype . . . 52

Figure 4.8 Z-Source Circuit Breaker Source Current. . . 53

Figure 4.9 Z-Source Circuit Breaker Switch Current. . . 54

Figure 4.10 Experimental Z-Source Circuit Breaker Source (solid lines) and Switch Current (dashed lines). . . 54

Figure 4.11 Experimental and Simulation Source Current. . . 55

Figure 4.12 Experimental and Simulation Switch Current. . . 56

Figure 4.13 Comparison of Theoretical and Experimentald td i to voltage . . . 56

Figure 4.14 Prototype Isolation of Mechanically Switch Z-Source Circuit Breaker . . . 57

Figure 4.15 Bidirectional, mechanically switched Z-Source DCCB . . . 61

Figure 4.16 Mechanical switch isolation waveform with (a) 10 A and (b) 22 A . . . 63

Figure 4.17 Z-Source circuit breaker simplified analytical schematic . . . 64

Figure 4.18 Experimental current transient time comparison with (blue)LS y s=0m H and (orange)LS y s=2.5m H . . . 66

Figure 4.19 Zero crossingst1&t2and compensated nonlineart20 . . . 70

Figure 4.20 Optimization distribution oft20withL/C ratio . . . 71

Figure 4.21 Logic flow diagram of protective action . . . 72

Figure 4.22 Z-Source test prototype experimental waveform . . . 74

Figure 4.23 Z-Source circuit breaker test prototype waveform . . . 75

Figure 4.24 Z-Source circuit breaker test prototype waveform . . . 76

(16)

Figure 5.1 Comparison of typical DC and AC fault differences during short circuit fault

conditions . . . 81

Figure 5.2 Comparison of progressive switching voltage and current simulation output of 1, 4 and 8 switching steps . . . 83

Figure 5.3 Progressively switched solid-state DCCB schematic (shown with 4 stages) . . . 84

Figure 5.4 Four-stage, 380VD C, progressively switched solid-state DCCB . . . 86

Figure 5.5 Two-stage progressively switched DCCB experimental test waveforms . . . 87

Figure 5.6 Four-stage progressively switched 380 volt DCCB test bench . . . 89

Figure 5.7 Four-stage progressively switched DCCB infrared image during continuous ope-ration . . . 89

Figure 5.8 Four-stage progressively switched DCCB experimental test waveforms . . . 90

Figure 5.9 Four-stage progressively switched DCCB experimental test waveforms . . . 91

Figure 5.10 Four-stage progressively switched DCCB experimental test waveforms . . . 91

Figure 5.11 Simplified analytical model of a hybrid DCCB . . . 94

Figure 5.12 Opening sequence of a hybrid DCCB . . . 96

Figure 5.13 Operation of a hybrid DCCB . . . 97

Figure 5.14 Progressively switched, actively damped UFMS hybrid DCCB functional diagram 98 Figure 5.15 Progressively switched hybrid DCCB schematic . . . 98

Figure 5.16 Operation of proposed progressive hybrid DCCB . . . 100

Figure 5.17 Simulation of 2ms UFMS operating in a 1 stage hybrid DCCB, and 4 stage and 8 stage progressively switched hybrid DCCBs . . . 101

Figure 5.18 Simulation of progressively switched DCCB . . . 101

Figure 5.19 Four-stage progressively switched MB . . . 103

Figure 5.20 Four-stage progressively switched MB experimental test waveforms . . . 104

Figure 5.21 UFMS vacuum gap vs. time . . . 104

Figure 5.22 Control logic flowchart for progressive shutdown . . . 107

Figure 5.23 Progressively switched, actively damped UFMS, hybrid DCCB test prototype . . . 108

(17)

Figure 5.25 Current, voltage and displacement waveforms from progressive hybrid test,

pro-cessed for clarity . . . 109

Figure 6.1 Output current and voltage waveforms of an early 25 volt, 2.5 amp, 2 stage pro-gressively switched solid-state DCCB . . . 113

Figure 6.2 Output current and voltage waveforms of the 425 volt, 20 amp, 4 stage progressi-vely switched hybrid DCCB . . . 113

Figure 6.3 Output current and voltage waveforms of the 1,000 volt, 3 amp, 4 stage progressi-vely switched solid-state DCCB . . . 114

Figure 6.4 Presspack solid-state switch device . . . 115

Figure 6.5 Puck style MOVs . . . 115

Figure 6.6 TO-247 style radial lead MOSFET package . . . 116

Figure 6.7 Radial lead style MOVs . . . 116

Figure 6.8 Module style solid-state switches . . . 117

Figure 6.9 PSCAD Fault Simulation Diagram of 15 kV Modular DCCB . . . 117

Figure 6.10 PSCAD Schematic of 15 kV Modular DCCB . . . 117

(18)

TERMINOLOGY

AC Alternating current

CS Commutating switch

DC Direct current

DCCB Direct current circuit breaker

DSP Digital signal processor

ESFI Electrical Safety Foundation International

FEM Finite element method

HVAC High voltage alternating current

HVDC High voltage direct current

IEC International Electrotechnical Commission

IEEE Institute of Electrical and Electronic Engineers

IEGT Injection-enhanced gate transistor

IGCT Integrated gate-commutated thyristor

IGBT Insulated-gate bipolar transistor

LED Light emitting diode

LVDC Low voltage direct current

MB Main breaker

MMF Magnetomotive force

MOSFET Metal oxide field effect transistor

MOV Metal oxide varistor

MVDC Medium voltage direct current

NEC National Electric Code

NFPA National Fire Protection Association

OSHA Occuptational Safety & Health Administration

SiC Silicon Carbide

TCA Thomson coil actuator

(19)

TRV Transient recovery voltage

UFMS Ultrafast mechanical switch

VSC Voltage source converter

(20)

CHAPTER

1

LOW AND MEDIUM VOLTAGE DIRECT

CURRENT MULTI-TERMINAL

DISTRIBUTION AND PROTECTION

1.1 Introduction

The production, transmission, and distribution of electric energy comprises one of the largest

infrastructure networks ever created, yet it is still rapidly growing. The International Energy Agency

estimates that 1.1 billion people, approximately 14% of the global population is does not yet have access

to electric energy, however global energy consumption continues to rise. The existing electric energy

distribution infrastructure originates back to the late nineteenth century where centralized generation

far away from the consumer is transmitted to the population regions, voltages is adjusted accordingly

(21)

electric grid continues to evolve and adopt new technologies, this legacy system exhibits its struggle to

meet changing requirements, and new options to manage global energy distribution must be assessed.

This preliminary dissertation analyzes a growing global trend toward direct current (DC) loads,

generation sources, and distribution networks and deals with the most significant challenge facing DC

systems, circuit protection. DC circuit protection has unique requirements and presents new obstacles

that are not associated with conventional alternating current (AC) system protection.

1.2 Global Trends Toward the Adoption of Direct Current Systems

Direct current devices are tenaciously expanding throughout modern society and infrastructure from

low to high voltage levels. The low voltage sector shows drastic growth in portable consumer

electronics, light emitting diode (LED) lighting, digital systems, electrified transportation, and inverter

driven appliances as illustrated in Fig. 1.1.

Figure 1.1Illustration of the global trend towards DC systems.

Similarly, high voltage direct current (HVDC) bulk power transfer dominates the modern electric

power transmission sector across the world, proving to be more efficient, higher power density, and

more cost effective than traditional high voltage alternating current (HVAC) overhead lines. However,

(22)

power from centralized power stations unidirectionally to the end consumer. This poses significant

challenges to the electric distribution infrastructure to adopt the proliferating distributed renewable

energy resources which may cause bidirectional power flow on legacy systems, affect voltage droop

profiles, and bypass protective features. The legacy alternating current distribution system requires

multiple stages of conversion between alternating and direct current to finally arrive at the load, which

is likely direct current, resulting in costly and inefficient electric power distribution as shown in Fig. 1.2.

Figure 1.2Many conversion steps between centralized generation and end consumer.

The introduction of semiconductors has lead to exponential growth in DC systems. These devices

allow the modification of voltage levels without need of a magnetic field, allowing DC voltages to be

stepped up and down with ease, and paved the way for the digital age. Nearly all residential and

commercial energy is consumed in direct current, with industrial applications being the primary

consumer of line-fed AC energy.

1.3 Advantages of Direct Current Distribution

Direct current energy sources, such as solar farms; and DC loads, like portable electronics, occupy an

ever growing presence on the modern electric grid. A DC distribution network would eliminate tens of

millions of AC to DC converters that are used in nearly all of our devices. Every portable electronic

device, digital system, inverter driven devices, and more are entirely DC. This was established early on

(23)

to the immediate uptake of DC in all motor vehicles. A DC grid can be stand-alone, known as islanded,

or can be grid connected to the legacy power system, as shown in Fig. 1.3.

Figure 1.3A DC microgrid interconnected to the legacy AC grid and a DC microgrid.

Several of the many advantages of DC distribution over the legacy AC distribution system include:

1. No skin effect.The entire diameter of a cable is used for DC distribution rather than the outer 8.5 mm used at 60 Hz due to the skin effect, resulting in more effective use of cables and overhead

lines.

2. Only real power.With no frequency component, the only controlable aspect of a DC grid is the voltage level for power sharing. As such generators or converters have an additional degree of

(24)

3. Fewer Conductors.DC systems require only two or three conductors, dependent upon the neutral reference point arrangement. AC systems require a minimum of 4 conductors for

traditional three phase operation.

4. No Magnetic Field.Without a time varying current component, a magnetic field is not generated, this results in reduced corona discharge, no proximity effect, and no interference to surrounding

personnel or equipment.

5. HVDC to MVDC Conversion.Current conversion to and from HVDC to AC transmission levels requires large valve stations including reactors, capacitor banks, grid frequency matching, and

additional equipment. HVDC to MVDC conversion is drastically simplified without the need for

such reactive compensation.

6. No Frequency Control.Connection to the DC distribution grid does not require frequency matching, enabling ease of distributed generation connection.

7. Offshore Energy Harvesting.HVDC is the primary means of transmitting offshore wind power to shore for consumption. However, this currently requires the windfarm be operated

synchronously, collected as an offshore substation, converted to HVDC, transmitted to shore for

conversion back to AC for distribution. This process would be greatly simplified with a meshed

DC grid and would expand the ability of other offshore energy harvesting technologies[1].

8. Enhanced Controlability.Voltage source converters that dominate DC distribution systems are able to compensate for changes in load on the nanosecond level, dependent upon switching

frequency. Comparable AC systems rely upon mechanical governors and electric field adjustment

to correct for load changes.

1.3.1 Low Voltage Direct Current Applications

All computerized and digital electronics operate on LVDC and are well suited for DC microgrids to

ensure sensitive electronics are not susceptible to interference[2]. 380 Volt DC distribution has already

been identified as a common low voltage distribution level with uptake widely seen in battery banks,

(25)

system, low voltage DC distribution also maintains the highest level of stability and continuity through

selected tripping of protection devices[4]. Portable electronics ranging from very small and low power devices such as pace-makers and watches ranging ot high power large devices such as electric vehicles

are all direct current. At an even larger scale, chemical energy storage is growing in popularity to stiffen

electric grids and reduce the intermittency of renewable energy resources like wind and solar energy.

Low voltage DC applications are generally easier to protect at low power levels and is achieved by fuses,

power electronic switches, small relays or other mechanical switches that are able to manage the arc

that is drawn.

1.3.2 High Voltage Direct Current Transmission

HVDC is not limited by the insulation rating of transformers as modern HVDC valve stations are able to

achieve voltages exceeding one megavolt[5]. These ultra-high voltages, cominbined with lack of skin

effect or proximity effect and the need for only two conductors makes far less expensive than long

distances AC transmission. Additionally, with minimal time varying component, HVDC observes

reduced power loss and environmental impacts due to corona discharge[6].

HVDC systems at this point in time are all two-terminal systems for bulk power transfer and have

no DC side protection. This means that if a fault were to occur or if the system needed to be secured,

the entire two-terminal system is shut down at each end. Therefore DC circuit protection is not

required until such a point in time that HVDC systems branch into multi-terminal networks.

1.3.3 Islanded and Non-conventional DC Distribution Systems

An increasing number of applications which are not connected to the existing utility grid are designed

and operated in purely DC. Space flight and exploration are all entirely DC as they operate on

photovoltaic (PV) and radioisotope thermal generation (RTG) which both produce direct current. As

nearly all loads on spacecraft are DC and they are not connected to the terrestrial electric grid, there is

no need for AC on these missions. Modern aircraft systems are increasingly utilizing multiple power

electronic converter systems for conversion and conditioning of the power system, which is in most

aircraft, entirely DC[7]. The Navy and large marine ships are investigating the use of multiple small

(26)

to shift toward electric pod propulsion, replacing the conventional shaft driven propeller. Shipboard DC

distribution allows for smaller, more fuel efficient generators to be ran at their optimum efficiency

speed rather than dictated by the ship speed requirement or the frequency of the bus. Transoceanic

cargo liners who do not connect to shore power frequently are under scrutiny due to large diesel engines

running for days on end while ships are loaded and unloaded at port just to provide auxiliary power to

the ship, which could be accomplished more efficiently with a small DC generator connected to the bus.

Other islanded applications include off-shore energy harvesting beyond that of just wind, which has

already established DC as the subsea transmission medium of choice and coastal desalination.

1.4 Challenge of Protecting Direct Current Systems

Although the applications and generation sources are available for DC distribution, the challenge

remains to safely protect these systems by interrupting the current in the event of a fault. Modeling of

DC distribution systems is far more dynamic than for AC systems, specifically based upon energy

storage and distributed generation and the individual dynamics of each converter, therefore event

based protection is required to ensure protection is provided under all circumstances[9]. The most

accepted and capable means of fault detection and locating is through Differential Protection Strategies

[10–12]. Differential detection does have limitations due to traveling waves, interference, and

harmonics injected to the line through the grid connected converters[13]. Centralized Protection Strategies are also possible, yet require low latency communication to all devices in the distribution

network[14]. DC faults can pose exceptionally demanding protection challenges in terms of speed of

propogation and fault current magnitude due connected energy storage and fast response time of

Voltage Source Converters (VSCs)[15].

Two primary challenges are exhibited in interrupting fault current in multiterminal DC circuits,

interruption speed and the lack of a current zero crossing.

1.4.1 Interruption Speed

Low system inductance from decoupling of motors and generators through power electronics results in

faults rise much faster in DC systems than in AC systems, as shown in the first few milliseconds of Fig.

(27)

two or three time greater than nominal fault current for several milliseconds before experiencing

voltage collapse of the system. Therefore, DC circuit breakers must operate in several milliseconds,

rather than 30 to 70 milliseconds that are common for AC electromechanical circuit breakers. The

widely accepted time for showing DC distribution protection has been 5 milliseconds, however recent

publications and Advance Research Projects Agency-Energy (ARPA-E) solicitations are pursuing

protection methods as fast as 500 microseconds.

Figure 1.4Rapid voltage collapse of a DC distribution system compared to AC system.

1.4.2 Absence of a Current Zero-Crossing

In AC systems, there is a natural current zero crossing point on each phase at a rate of21f, or once every

10 to 8.3 milliseconds for 50 and 60 Hz, respectively. This provides a recurring and natural point for any

arc that is drawn to be subsequently extinguished provided that the dielectric strength of the

(28)

overcurrent fault in an AC distribution system, even with a large DC offset at the beginning of the

envelope, the current waveform continues to cross zero periodically until it is extinguished. This allows

any mechanical switch which can open contacts far enough to overcome the voltage differential

between the contacts to interupt an AC fault whether it be an open air contact, oil bath, vacuum, or for

high voltage switches, Sodium Hexafloride (S F6) or other gas.

Figure 1.5AC fault with a repetitive current-zero crossing facilitating fault isolation.

However, DC does not cross zero at any time, this removes the systems natural ability to

commutate any arc that is drawn. This same occurance is found in pulse power applications, such as a

Wave Energy Converter (WEC) which creates current pulses as it moves back and forth in the surf, or

variable current sources, such as a bouy or other non linear generator as shown in Fig. 1.6.

Without a symmetrical current to balance the energy and to ensure a zero crossing, natural fault

current commutation cannot be used to interupt faults in these systems. Therefore not only does the

current need to be forced to zero by an artificial means, but the non-symmetrical energy must be

managed. The following section identifies methods to force the current to zero and absorb the transient

(29)

Figure 1.6Direct current, pulsating, and variable current sources do not guarantee a current zero crossing.

1.4.3 Organization of Subsequent Chapters

The rest of this dissertation reviews work done to date, and planned future work in the field.

• Chapter 2 - DC Circuit Protection Technologies: A Review of Proposed Topologies

• Chapter 3 - Active Damping and Advanced Control of a Thomson Coil Actuated Ultrafast

Mechanical Switch

• Chapter 4 - Design and Optimization of a Mechanically Switched Z-Source Resonant DCCB

• Chapter 5 - Progressively Switched Solid-State and Hybrid Direct Current Circuit Breakers

• Chapter 6 - Conclusions and Future Work - Scalability of Progressively Switched Hybrid Circuit

(30)

CHAPTER

2

DC CIRCUIT PROTECTION

TECHNOLOGIES: A REVIEW OF PROPOSED

TOPOLOGIES

2.1 Existing Solutions for Protecting Direct Current Systems

There are several methods that can be employed to isolate a DC system fault:

1. Fuses:Thermal fuses are common in low voltage and lower power systems where a metalic element is heated during an over current condition to the point of melting, creating an open

contact and securing current flow. This method absorbs the excess energy through the thermal

action of destroying the element and then must be replaced to reintroduce current flow once the

fault condition is corrected. This solution is commonly used in 12 VDC systems in automobiles

(31)

several hundred volts, dependent upon system dynamics, as large enough current surge or fault

condition will ionize the air between the two contacts and continue to supply fault current.

2. De-energize the System:Securing all sources of energy to the system will isolate a DC fault quickly, as the power electronic converters that supply DC systems can be shutdown in

microseconds. Once all generation sources are shutdown, the remaining energy in the system will

be discharged through the fault or operational loads and the fault condition will stop, and the

system can be re-energized once the condition that caused the fault is corrected. This is common

in HVDC or other two-terminal systems where shutting down of the entire system would be the

same as isolating the fault, however if there are multiple generation sources, and multiple

terminals, this will cause all devices on the system to lose power. Additionally, in the event that

multiple generation sources are feeding the fault, the shutdown must be coordinated to secure all

sources to the fault at the same time, to prevent damage to any one converter that is left to supply

the fault current alone, requiring a centralized control strategy.

3. Circuit BreakersA circuit breaker is a device that locally determines if a fault condition occurs and stops the current from flowing using a switch. The switching device can be mechanical or

solid-state. Circuit breakers come in many different shapes, sizes, and styles and can be designed

to operate locally or remotely, and can provide many types of circuit protection in addition to

over current conditions such as under-voltage, over power, rate of current change, and many

more. These are the most flexible and dependable circuit protection devices and can be designed

for all voltage levels.

2.2 DC Circuit Breakers

Direct current circuit breakers (DCCBs) provide the highest degree of controlability, protection, and

flexibility for multiterminal DC distribution systems. However, DCCBs must operate within

milliseconds to provide protection, and manage the transient energy that would be discharged through

(32)

2.2.1 Mechanical Circuit Breakers

Mechanical circuit breakers create a gap between contacts either in air, vacuum, oil, or a non-ionizing

gas likeS F6in high voltage circuit breaker switches. Mechanical DCCBs are able to draw and quench an arc either through oscillation such as a capacitive discharge as shown below in a oscillatory mechanical

circuit breaker in Fig 2.1. Up to several hundred volts and at low currents, some devices are able to

create a large mechanical gap between contacts or insert an insulating separation device to quench the

arc. These devices are commonly used at lower power applications such as small rooftop solar arrays

Mechanical DCCBs can be operated by springs, solenoids, repulsion coil, pneumatic, or

hydraulic actuators. To achieve millisecond level protection and to keep the devices simple, most are

either solenoid or repulsion coil coil actuated. It is important to note that a mechanical switch is not a

DC circuit breaker. A mechanical DCCB must have a means in which to absorb or counteract the

transient energy and quench any arc that is drawn during a fault isolation condition. In Fig. 2.1 the arc

is counteracted through the discharge of the capacitor in the parallel branch and any excess energy

from the transient surge or the capacitive discharge is dissipated in the surge arrestor as heat.

Mechanical DCCBs are the most efficient and robust as they do not require any cooling and they

have relatively zero on state power consumption. However, these devices are the slowest of all DCCBs

and are generally limited to lower power levels as high power arcs are difficult to interrupt without

catastrophic damage to the device.

2.2.2 Resonant Style Circuit Breakers

Resonant style circuit breakers, such as a Z-Source circuit breaker shown in Fig. 2.2 create an artificial

current zero through resonant ringing between energy storage devices and commutate off the thyristor

iS C R by reverse biasing it during the resonant transient. Many arrangements of resonant circuit

breakers have been designed and tested, yet all operate based on the same principle of exchanging

energy between two or more energy storage devices at their resonant frequency during transient.

Resonant circuit breakers are very fast to operate and relatively inexpensive to build, and in the

case of the thyristor based Z-Source DCCB shown in Fig. 2.2 provides automatic overcurrent protection

(33)

Figure 2.1Oscillatory mechanical circuit breaker.

to the power handling capability of the thyristor that full load current must pass through, creating an

on-state power consumption. However, without significant additional complexity they are

unidirectional and only offer over-current protection, as even manual operation of these DCCBs

requires that a current transient be introduced in the system, placing strain on the converters, loads,

and the circuit breaker itself

(34)

2.2.3 Solid-State Circuit Breakers

Solid-state circuit breakers can be used with a variety of components and can be either unidirectional

or bidirectional by design[16, 17]. Although similar in design to the mechanical DCCB, a solid-state

circuit breaker does not draw an arc, it opens a doped channel within the semiconductor device which

stops electron flow, with the exception of a small leakage current. Solid-state DCCBs must be used in

conjunction with a snubber and/or an arrestor to absorb the energy in the system as shown in Fig. 2.3. The solid-state switch is opened within several nanoseconds of the gate signal being removed, therefore

the system inertia due to any inductance in the system, parasitic or by design, will cause a rapid

over-voltage condition at the device terminals, which will destroy the device if the surge exceeds the

voltage rating. Some of the most common solid-state switches used in solid-state circuit breakers

include:

• IGBT - Insulated Gate Bipolar Transistor

• IGCT - Integrated Gate-Commutated Thyristor

• GTO - Gate Turn Off Thyristor

• IEGT - Injection-Enhanced Gate Transistor

• ETO - Emitter Turn Off Thyristor

• SCR - Silicon Controlled Rectifier

• MOSFET - Metal Oxide Field Effect Transistor

• JFET - Junction Field Effect Transistor

Each component has a unique characteristic dependent upon the needs of the application, as

some have a constant voltage dropVdsuch as SCR and IGBT, where some have a temperature constant

on-state resistance,Rd s,o n, such as MOSFET and JFET. Others are normally on or normally off, have

either current or voltage dependant gates, etc.

Solid-state circuit breakers are the fastest and most energy dense of the DCCBs and they are fully

(35)

circuit breaker, a solid-state DCCB relies on the sensing and control of an outside digital signal

processor or controller. Solid-state DCCBs have significant on-state power consumption leading to

reduced efficiency, and need for supplemental cooling in many applications. Operation during a fault is

also limited to the thermal handling capabilities defined by the device based upon theI2T curve for each specific device, which determines how quickly the device will self-heat as current increases during

an overcurrent fault condition.

Figure 2.3Solid-state circuit breaker.

2.2.4 Hybrid Circuit Breakers

A hybrid circuit breaker combines the high efficiency of a mechanical normal current path and the high

speed power electronic shutdown capabilities of a solid-state DCCB as shown in Fig. 2.4. Together these

two designs provide high speed, controllability, and efficiency. During operation normal load current is

directed through the fast mechanical switch, and a commutating switch, also known as a auxiliary

circuit breaker. In the event of a fault the main breaker turns on and the commutating switch turns off,

redirecting current through the main breaker. Then the fast mechanical switch opens under no-current

condition, mitigating any arc from being drawn across its contacts. Once the fast mechanical switch is

open, the main breaker turns off and stops current flow the same way that the solid-state DCCB does.

Hybrid circuit breakers are capable of achieving very high power levels with minimal on state

power loss through the commutating switch. These circuit breakers are dependent upon the speed of

the fast mechanical switch as the limiting factor for full isolation and shutdown. Advances in repulsion

(36)

Hybrid circuit breakers hold the greatest possibility to balance the high efficiency requirements

of a DC distribution system, while providing adequate isolation times to ensure system stability. Hybrid

DCCBs while more efficient than a solid-state DCCB do have the drawbacks of slower operation time,

and higher system cost, due to the construction of effectively two circuit breakers in parallel.

Figure 2.4Hybrid circuit breaker.

2.3 Medium Voltage Direct Current Distribution Protection

Medium voltage direct current (MVDC) is identified as a promising solution to the aging legacy electric

grid, and is being actively pursued for non-grid connected applications such as electrified

transportation including, Navy and shipping, high speed rail, aviation, hyperloop, and electric personal

vehicles.

This research is funded by, and in support of, the University of North Carolina (UNC) Coastal

Studies Institute (CSI) North Carolina Renewable Ocean Energy Program (NCROEP). This research has

generated technologies aimed at meeting the NCROEP mission of facilitate the study of, harnessing,

and distribution of energy harvest off-shore from a variety of renewable energy resources.

MVDC Distribution and Protection provide many benefits beyond renewable ocean energy

harvesting as well, such as:

(37)

• Distributed generation and storage

• Electrification and Decentralization

• Distributed Renewable Electrical Energy Resources

• Transportation Paradigm Shift

• Transactive Energy Markets and "Prosumers"

• Military Applications (Navy, Aviation, Forward deployed units)

• Cruise Ships and other Maritime Applications

• Installation and Maintenance Platforms (Oil, offshore wind, floating drydocks)

2.4 Dissertation Purpose

This preliminary dissertation identifies the challenges and proposes solutions to the most difficult

aspect of low and medium voltage direct current systems, DC circuit breakers. The fundamental

challenge of DC circuit protection is investigated and requirements for low and medium voltage

distribution circuit protection are established based upon system dynamics and fault response. Finally,

solutions for high speed, high efficiency, bidirectional circuit protection are presented in theory,

(38)

CHAPTER

3

ACTIVE DAMPING AND ADVANCED

CONTROL OF A THOMSON COIL

ACTUATED ULTRAFAST MECHANICAL

SWITCH

3.1 Thomson coil actuated ultrafast mechanical switches for hybrid DC circuit breaker

Medium and high voltage hybrid DC circuit breakers combine electronic switches with mechanical

switches in parallel[18–23]. They consist of four primary components for current conducting, commutation and interruption as shown in Fig. 3.1; an ultrafast mechanical switch (UFMS) or

disconnector, a low voltage solid state switch as the commutating switch (CS), a high voltage solid state

(39)

composed of anti-series IGBTs, denoted as two IGBT symbols with diodes in the diagram. They in fact

represent strings of devices to meet the requirement of the nominal voltage rating. The hybrid solid

state DC circuit breaker scheme that exploits a low voltage commutating switch in series with an

ultrafast mechanical disconnector provides an ultrafast and highly efficient protection solution to

power systems[19, 20]. In normal conduction, the current flows through the nominal path that consists

of UFMS and CS. In order to interrupt a fault current, first the CS turns off in a few microseconds and

commutates current into the MB in a few tens of microseconds. The UFMS opens and forms a gap

between its contacts that can withstand the high voltage that will result from the subsequent turn-off of

MB.

Though this concept was originally proposed to interrupt a DC circuit, it fits AC applications as

well. As a matter of fact, since the interruption operation is finished as fast as in a couple of

milliseconds, it is faster than usual AC periods (at 50 or 60 Hz), such that an AC circuit acts like a DC

circuit as far as the hybrid circuit breaker is concerned. Because of the sub-quarter cycle operation, the

hybrid circuit breaker can therefore also limit the fault current in AC circuits.

The effectiveness of these hybrid AC and DC circuit breakers is predicated on the mechanical

switch opening as fast as possible to obtain a sufficient gap between the open contacts, so that they can

withstand the transient recovery voltage (TRV) following current interruption. This is because the total

interruption time of the hybrid circuit breaker is dominated by the operation speed of the UFMS in

such hybrid circuit breakers[18, 19, 24–27].

(40)

Figure 3.2Diagram of the Thomson coil actuator based fast mechanical switch.

The switches used in this type of circuit breakers are typically based on electromagnetic

repulsion forces with current induced in a conductive copper disc (so-called Thomson coil actuator)

[24, 25, 27]. The switch actually comprises two coils, one for the opening operation and one for the

closing operation, located on either side of the copper disc (above and underneath, Figs. 3.2 and 3.3. To

open the UFMS, the opening coil is energized so that a strong magnetic field is generated which

penetrates into the conductive disc. This time varying magnetic field induces azimuthal eddy currents

in the disc which in turn create an opposing magnetic field. These two fields oppose each other and a

repulsive force is generated between the coil and the disc. Closing is obtained in a similar manner with

the lower coil.

In this paper, an active damping mechanism and its control are proposed for this type of actuator.

The goal is to absorb the kinetic energy at the end of motion, avoiding over-travel, bounce, and the like.

In doing so it becomes possible to actually excite the opening coil to higher levels, resulting in overall

faster operation than would be possible without the active damping. This result will contribute to

achieving ultrafast operation for the switches and therefore the hybrid DC circuit breakers. With this

control, superior performance is achieved. Further, the structure remains simple without adding extra

damping mechanisms. Smaller vacuum interrupters can be used and the size of the overall switch

(41)

on the issue of DC current breaking are facing the same difficulties. Similarly, in[27], the velocity of the

moving part is seen increasing up to the end of motion, reaching a high 5 to 6 ms , with no damping

mechanism included in the design to absorb the corresponding kinetic energy upon end-of-motion

impact. The present paper adds to the literature a comprehensive parametric analysis as well as

experimental investigations. The experimental study provides valuable quantitative results on different

combinations of driving conditions of the opening and damping operations.

The paper includes finite element modeling of the active damping transients and test results

obtained on a 15kV/630A/1ms mechanical switch. The actuator design used in this study is described

in details in[25], and the drive circuits have been discussed in[26]. The content of this study were

originally presented at the 2016 ECCE Conference[25].

(42)

Figure 3.4The ultrafast mechanical switch prototype. The based plate is approximately 30 cm by 30 cm.

3.2 Reclosing issue with passive damping mechanism

The general issue addressed in this paper is the design of effective, reliable damping mechanisms to

absorb the kinetic energy due to fast opening. Mechanical means are effective, but need to be tuned to

the energy imparted to the system during opening. Not enough damping can lead to damage, and too

much generates bounce and long effective travel time. If the bounce is large enough, the system

recloses (opening failure). Therefore, a fixed damping can actually limit the opening energy and

lengthen the travel time, by forcing the designer to use a level of energy below that which will lead to

bounce. This was observed during initial tests of a prototype switch (shown in Fig. 5.4). In order to

illustrate this, Fig. 3.5 shows a successful opening with a capacitor bank that is precharged to 400 V. The

displacement curve is linear, overshoots and finally settles at a steady state open position. When driven

by 420 V however, see Fig. 3.6, the travel is initially faster but at the end of the travel and following the

overshoot the switch does not stay at a steady state open position. Instead it bounces back towards the

(43)

non-linear disc springs (see[4]for a more detailed description of the design). Other mechanisms are

possible[29–31]but all are expected to suffer from the same limitation due to their being set at the design stage, with no feedback control possible. With damping disc springs a few factors can affect the

damping process, such as:

1. The kinetic energy of the moving mass. Most of the energy is to be absorbed by the disc springs.

2. The non-linear load-versus-deflection characteristic of the disc spring (see[25]) and how much

energy the disc spring can absorb. The disc spring provides holding forces both at the open and

closed positions which correspond to different operation points on the load-versus-deflection

curve.

3. The allowable over-travel during opening. Two components limit this over-travel range: the

vacuum interrupter and the disc spring. A longer over-travel results in larger sizes for both

components and therefore the overall size of the switch assembly.

Figure 3.5Successful opening driven by 400 V.

3.3 Proposed active damping for Thomson coil actuated switches

This paper proposes an active damping method that utilizes the Thomson coils of such an actuator and

does not require extra mechanical complexities in structure and design.

When the mechanical switch is to open, a large amount of energy is dumped into the opening

(44)

Figure 3.6Opening driven by 420 V followed by a reclosing.

method, as the fast opening is completed and the required gap is obtained, the closing coil is energized

and used as a damping coil to generate a reverse, braking force which slows down the movement. Then

the disc spring can easily handle the remaining kinetic energy and secure the moving parts in the open

position.

The approach is developed here in the context of repulsion coils. It can be extended, at least in

principle, to any actuator with two (or more) coils acting in opposite directions. Some work in that area

was done, for instance, on actuators with permanent magnets[32–34].

The research was carried out first by comprehensive transient finite element method (FEM)

simulation, complemented by experimental evaluation. The physical equations solved by COMSOL

include Maxwell’s Equations in the opening coil, the closing coil and in the conductive disc, as well as

the mechanical balance of force between the electromagnetic forces as derived from Maxwell’s, spring

forces, gravitational forces and friction losses.

These supporting equations have been published in previous work completed under this project

[20], and similar equations were provided elsewhere[27].

The FEM modeling includes different physics (electromagnetic, mechanical, and thermal), see

Fig. 3.7. The mechanical actuator is designed for a 630 A prototype at medium voltage range (15-50 kV).

The model geometry is shown in Fig. 3.8. Two typical snapshots of the simulated transients are

presented in Figs. 3.9 and 3.10 to illustrate the eddy currents induced in the conductive copper disc

upon the energization of the opening coil and the damping coil, respectively.

(45)

Figure 3.7Multiphyics interaction in the actuator.

Figure 3.83D view of the FEM model.

opening transient when the opening coil is driven by a moderate voltage level of 355 V. The travel

reaches 3 mm at 2 ms and settles to a steady state position of approximately 7-8 mm with 1.5 mm

overshoot. When opening voltage is as high as 415 V (the purple curve), the moving contact overshoots

more than 2 mm and recloses because the excessive kinetic energy is not damped out by the

(46)

Figure 3.9Induced current in the disc, 60µs after energizing the opening coil, simulation in axisymmetric 2D view.

Figure 3.10Induced current in the disc, 440µs after energizing the damping coil, simulation in axisymmetric 2D

view.

Therefore, the active damping method is proved to enable higher speed operation and prevent

(47)

voltage can be even higher, such as 430 V, so that faster opening operation can be achieved.

Figure 3.11Damped and undamped operations.

3.4 Design of the active damping control

The general principle of active damping was presented in Section III. This section addresses how to

design the damping control, or in other words when and by how much the damping coil should be

energized. For a given pulse of the opening coil, there are a few variables in the damping pulse that can

be changed to achieve the best performance for a given design of an UFMS. They correspond to the

timing, magnitude, and shape of the damping pulse, the magnitude and shape being controlled by the

capacitance and voltage of the capacitor bank exciting the damping coil. If the same capacitor bank is

used for both opening and closing operation, as is preferable for simplicity and to minimize cost, it is

also the same for the damping operation. Therefore timing is the most convenient parameter to affect

the damping performance. Voltage and capacitance may be used as additional degrees of freedom, if

their impact on performance justifies the extra complexity.

Figs. 3.12 and 3.13 illustrate the active damping effects, as calculated by transient FEM modeling

(48)

to Fig. 3.12, a negative force accelerates the moving mass, starting at time 0. Then, a positive force later

dampens the movement, starting at time 2 ms or later (several model runs are superimposed on the

same graph, all starting with the same opening pulse). Fig. 3.13 shows the corresponding displacements

(solid traces) and velocities (dashed curves).

Figure 3.12Driving force (from 0 to 2 ms) and damping forces (from 2 to 4 ms), simulation results.

With a capacitor bank of 2 mF pre-charged to 400 V, the actuator is accelerated to 2.6 m/s (Fig.

3.13). At 2 ms, the gap in the switch reaches 4.5 mm which can withstand 60 kV. A sweep of delay times

from 2.0 ms to 3.0 ms is presented in Figs. 3.12 and 3.13, and the following observations can be made:

1. Energizing the braking coil has an immediate effect to dampen the opening movement. Braking

therefore should not be initiated before the specified gap and opening time are reached, 4.5mm

and 2ms, respectively, in this case.

2. The later the damping coil is energized, the closer the copper discs proximity is to the damping

coil at time of actuation, therefore the damping force increases. Conversely, with shorter delays,

the disc may be too far for the damping coil to have any substantial effect, the disc being out of

range, so to speak. The largest peak damping force was obtained with a 3 ms delay. It is 160

(49)

Figure 3.13Speed and displacement curves corresponding to Fig. 3.12 forces, simulation results.

There is therefore an opportunity for optimization, with later pulses being more powerful, but

intervening farther in the travel. Fig. 3.13 shows when the damping force starts to operate, and

also shows the position at which the disc comes to a stop.

3. An earlier damping pulse results in a weaker force and takes a longer time to reduce the kinetic

energy of the moving mass. But the travel is limited to a smaller range (the disc stops at position 6

mm at time 4 ms).

4. A later damping results in a stronger force, takes a shorter time to reduce the kinetic energy of the

moving mass. However, the movable contact tends to travel further (7.7 mm at 4 ms).

3.5 Experimental tests of active damping

Experimental tests were performed on a Thomson coil actuated ultrafast mechanical switch to verify

the approach and the FEM model. These results provide additional validation of both the calculated

parameters of active damping, and the interactions that occur between the repulsion coils and the

(50)

Table 3.1Combinations of opening voltages, damping voltages and damping delays tested.

Opening voltage Damping voltage Damping delay

• 355 V

• 370 V

• 385 V

• 400 V

• 415 V

• 430 V

• 322 V

• 345 V

• 365 V (for selected opening voltage and delay values)

• 2.0 ms

• 2.2 ms

• 2.4 ms

• 2.6 ms

• 2.8 ms

• 3.0 ms

3.5.1 Test Setup

A prototype of a Thomson coil actuated ultrafast mechanical switch and associated driving mechanism

was modified to test the active damping approach in a laboratory setting. More details regarding the

mechanical switch can be found in[25]. The closing coil was used as the damping coil; two capacitor

banks of the same capacitance were independently controlled by two thyristor switches to energize the

opening coil and the damping coil. The physical setup is shown in Fig. 3.14.

The test setup allows incremental variations of the opening coil voltage, damping coil voltage,

and trigger delay between the opening and damping current pulses. Testing has been conducted using

the parameters listed in Tab. 3.1. Figs. 3.15 and 3.16 show which combinations of parameters led to a

successful opening, and which led to reclosure.

3.5.2 Measurement and Control of Test Setup

A high level measurement and control diagram shown in Fig. 3.17 represents the control inputs and

measurement outputs from the prototype test bench. Two programmable DC power sup plies charge

the opening and closing coil capacitor banks, which are then discharged through the Thomson Coils via

power thyristors. The User inputs and control, annotated in green in Fig. 3.17 control the timing delay

and voltage applied which is variable for experimentation. In red, the measurements of the system

(51)

Figure 3.14Test setup of the active damping method.

Figure 3.15Opening operations with varying opening voltages and damping delays with a damping voltage of

(52)

Figure 3.16Opening operations with varying opening voltages and damping delays with a damping voltage of 345 V.

• Current pulse applied to the opening and closing coils via a Rogowski current sensor

• Control signal to the opening coil

• Control signal to the damping coil

• Voltage signal from a linear potentiometer mounted to the shaft of the movable mass

The voltage signal generated by the linear potentiometer on the shaft is mathematically equated

to position, and the derivative of this signal is the movable masses velocity. Together these

measurements are used to track the position, speed, and signals associated with operation with respect

to time. The test bench offers great flexibility in operating the Ultrafast mechanical switch under

variable conditions to systematically test variable operating conditions, as described in the following

sections of this paper.

3.5.3 Comparison of COMSOL simulation with test results

Simulation accuracy is verified through comparison of the COMSOL multiphysics simulation and the

(53)

Figure 3.17Measurement and control diagram of the Thomson coil actuated, actively damped, ultrafast mechanical switch.

Volt opening and 345 Volt damping simulation with experiment. Two cases are shown corresponding to

damping-pulse delays of 2.0 ms and 3.0 ms. The timing, velocity and overall shape of simulated and

test-bench results verify the accuracy of the model after the 1 ms point. Deviation between simulated

and experimental data within the first millisecond are likely due to the following sources of error not

accounted for in modeling:

1. Stiction of the two physical bodies that requires additional force to overcome stationary friction

prior to beginning motion. The simulation did not include stiction.

(54)

characteristic. Although the spring and its non-linearity were modeled, its exact characteric may

have lacked precision over a portion or all of the spring force-displacement curve.

3. Contact slippage or lag of potentiometer position sensor due to the rapid acceleration of the

moving mass.

4. The COMSOL simulation predicts force which is then compared to motion, amplifying any error

in the double integral.

Figure 3.18Comparison of Experimental test-bench results to COMSOL simulated results.

3.5.4 Contribution of opening voltage

The impact of opening voltage for a fixed damping delay (either 2 ms or 3 ms) is shown as displacement

curves in Figs. 3.19 to 3.22. Also shown in the figures, for reference, is one trace corresponding to the

current pulses in the opening and damping coils. The force exerted on the movable mass for opening

and therefore the acceleration of the opening contacts are controlled through the opening voltage

applied to the opening coil. Increasing this opening voltage and therefore the magnitude of the current

Figure

Figure 1.3 A DC microgrid interconnected to the legacy AC grid and a DC microgrid.
Figure 3.9 Induced current in the disc, 60 µs after energizing the opening coil, simulation in axisymmetric 2Dview.
Figure 3.16 Opening operations with varying opening voltages and damping delays with a damping voltage of345 V.
Figure 3.17 Measurement and control diagram of the Thomson coil actuated, actively damped, ultrafastmechanical switch.
+7

References

Related documents