Power Conversion Technologies for Improved System Performance · Power Conversion Technologies for...

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Power Conversion Technologies for Improved System Performance Kaz Furmanczyk Crane Aerospace & Electronics 2009 Join Service Power Expo May 4-7, 2009 – New Orleans, Louisiana

Transcript of Power Conversion Technologies for Improved System Performance · Power Conversion Technologies for...

Page 1: Power Conversion Technologies for Improved System Performance · Power Conversion Technologies for Improved System Performance ... Introduction Background New ... V_Aux.V [V] R_Aux.I

Power Conversion Technologies for Improved System Performance Kaz Furmanczyk Crane Aerospace & Electronics

2009 Join Service Power Expo May 4-7, 2009 – New Orleans, Louisiana

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2©Crane Aerospace and Electronics

Introduction

Background

New Challenges for Power Conversion Equipment on Airplanes

Review of Technology Options for Powering Motors that Meet Aerospace Requirements

Implementing Modeling and Simulations for Design Optimization - Example

Conclusions

Summary of Hardware Performance

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Background

Traditional constant frequency power sources (400 Hz) on airplanes are being replaced by variable frequency generators (typically 360-800 Hz)

Pneumatic and hydraulic systems are being replaced with electrical devices – most of which are using electric motors

More electrical equipment is being added to airplanes – power quality becoming an issue

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Challenges

This creates new challenges, which need to be resolved:

Challenge #1 – Speed of inductive motors varies with frequency solution: replace inductive motors with DC brushless motors• However, direct rectification of AC into DC generates high

current distortion – exceeding acceptable power quality limits

Challenge #2 – Find effective solution for converting AC into DC with good power quality

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Power Quality

Effect of power conversion is reflected back onto the aircraft AC bus

The smoother the current waveform ---> the better the “Power Quality”

18-pulse, 30-pulse and active PFC approaches represent good power quality

~ ~~ =+

-Aircraft

Generator

PowerConverter

ElectronicLoads

AC DC

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Pow

er Q

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y im

prov

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Power Quality

Power quality requirements from leading OEMs (examples):• Boeing: 787B3-0147 • Airbus: AMD-24

Recent, DO-160, Rev. F Document imposed power quality requirements for aerospace products powered from an aircraft AC power systemThe most significant requirement is on restriction of individual harmonics generated by user equipment rated 35 VA or moreThe harmonic limits requirement makes direct rectification obsolete• Practically, all motor drivers, which are using direct rectification need

to be replaced or upgraded• Majority of traditional TRU units can not meet new current limit

requirements – improved designs or larger filters are needed

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DO-160F Current Harmonics Limit

Each current harmonic, up to 40th harmonic has specified limit

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Existing Approach

~ M

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Harmonics

[%] H. Limits

6-p Rect.

Traditionally, 6-pulse rectification provides DC power for motors However, input current harmonics exceeded DO-160F limits New - more advanced technology - is required to convert AC into DC

Current waveform

Harmonics

THD = 30.7%

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Technology Options

The following power conversion technologies are capable of meeting the new power quality requirements: • High frequency switch mode conversion (active

conversion)• Multiphase power conversion (passive conversion)• Other harmonic correction techniques, based on:

• Harmonic injection• Active filter implementation

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High Frequency Switch Mode Conversion

~ M

6-pulse rectifier being replaced by

3-phase switch mode converter

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THD < 5%

Input Current meets power quality

Switch Control

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High Frequency Switch Mode Conversion

Two practical solutions, based on:

Boost Converter

Regulated DC Output Voltage:• 320 Vdc minimum (with 115 Vac input) - for boost converter• 230 Vdc maximum (with 115 Vac input) - for buck converter

Meets Input Current Harmonic LimitsSoft Start AbilityPower Factor: 0.994–0.998Efficiency: 95–97 %

Buck Converter

DC Output

Three-Phase AC Input

DC Output

Three-Phase AC Input

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Multiphase Power Conversion

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Input Current meets power quality

6-pulse rectifier being replaced by ATRU (18-pulse)

THD = 6.4%

CB

A

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Multiphase Power Conversion

3-phase to n-phase autotransformer

3-phase n-phase

Three-PhaseAC Input

DC Output

1 2 n

Output Voltage: 270 Vdc nominal (with 115 Vac input); passive regulationMeets Input Current Harmonic LimitsPower Factor: 0.980-0.990 Efficiency: 96-98%Simplicity: low parts count; no need for energy storage components (C or L)

DesignApproach

Output Voltage Ripple[% p-p]

Input Current THD[%]

6-pulse

14 28-33

12-pulse

3.4 9-14

18-pulse

1.52 6-9

30-pulse

0.55 2.5-3.5

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Design Example - Multiphase Power Converter

Some of available 18-pulse autotransformer options:

It is almost impossible to analyze topology and optimize design without converter modeling and running simulations

A

C

B

A

C

B

A

CB

Option A Option B Option C

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18-pulse autotransformer topology meets new harmonic limits – if designed correctly

Current waveforms in transformer windings become very complex

Autotransformer converts 3-phase input voltage into 9-phase output

voltages (spaced 40 degrees from each other)

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Design Example - Multiphase Power Converter

ATRU Schematic.ssh

®

Simulation properties:Step width maxStep width minSimulation end time 5

NC4

NC1

EA

NC2

NC3

NC5

NC6

NB4

NB1

NB2

NB3

NB5

NB6

NA4

NA1

NA2

NA3

NA5

NA6

EB

EC

D1

D2

D3

D4

D5

D6

D7

D8

D9

D10

D11

D12

D13

D14

D15

D16

D17

D18

R1

R6

R8

R7

R3

R5

R4

R9

R2

18-pulse ATRU Non-Linear Model

ICA:

Input Parameters Control Equations

EQU

RW1:=2.1m*1.5

LPCT:=0.0005*1

N3:=11

Lg:=0.00075*2*2.54

FREQ:=400

RW4:=38.5m*1.5

N6:=15

RW3:=4.5m*1.5

N1:=6

Lmean_length:=18.09

LM:=16m

N2:=13

PHI0:=0

N4:=37

RW5:=4.4m*1.5

Acore:=21.2

RW2:=4.1m*1.5

N5:=13

RW6:=4.7m*1.5

X Y

NL NL NL

I I I

BH Curve 2

NL A NL B NL C

B A

VM1_prim.V

B B

VM2_prim.V

B C

VM3_prim.V

G

B

C

IA

IB

IC

G

B

C

B

G

C

Coil A Coil B Coil C

Magnetic Core

Output Filter

RB

RA

RC

RLOAD

Power Transformer

P_Load:=135*1

C1220u

R100.3

C2220u

R110.3

R1249.9k

R1349.9k

R1449.9k

R1549.9k

Rectifers

R18

C3

R16

C4

R17

C5

C6 R19

L6

RA1

RB1

RC1

L4

L5

C70.33u

R220.03

C80.33u

R230.03

3.3n

3.9

3.3n

3.9

3.3n 3.3n 3.3n 3.3n 3.3n 3.3n 3.3n

3.3n

3.9 3.9 3.9 3.9 3.9 3.9 3.9

3.9 3.9 3.9 3.9 3.9 3.9 3.9 3.9 3.9

3.3n 3.3n 3.3n 3.3n 3.3n 3.3n 3.3n 3.3n

Power Source Input Filter

Load

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Design Example - Multiphase Power Converter

Transformer construction challenges:• Choosing winding material (copper, aluminum) • Selecting conductor shape (round wire, square wire, foil)• Defining and optimizing core geometry and aspect ratio• Optimizing interactions between windings (leakage

inductance, proximity effects)

It is not practical to build and test each considered option

Therefore, design iterations and optimizations need to be performed on computers

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Design Example - Multiphase Power Converter

Define core geometry and winding configuration

Simulate performance

Convert geometry and materials into electrical parameters

Core LossesWinding LossesLeakage InductanceRegulation

Adjust and optimize

Transformer Construction Optimization:

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Design Example - Multiphase Power Converter

A

CB

Simulate converter performance and verify power quality

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First Completed DesignPower Quality not met; several current harmonics exceed limits

Input Current WaveformsAutotransformer Configuration

Optimized DesignAll current harmonics within

specification plus margin

Completed HardwarePerformance correlates very closely with optimized design

Interactive Optimization

Fabrication

Design

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Performance Summary of Existing Hardware

Parameter Design APassive

(12-pulse)

Design BPassive

(18-pulse)

Design CPassive

(30-pulse)

Design DActive(Boost)

Design EActive(Buck)

Output Power 4.5 kW 1.6 kW 8.6 kW 15 kW 5 kW

Input Voltage (nominal) 230 Vac 115 Vac 115 Vac 115 Vac 460 Vac

Output Voltage (nominal)

270 Vdc 270 Vdc 320 Vdc 400 Vdc 460 Vdc

Power QualityMeeting DO-160E

….Current THDCurrent Waveform

Yes11%Picture A

Yes6.4%

Picture B

Yes3.3%

Picture C

Yes3%

Picture D

Yes3%

Picture E

Power Factor 0.986 0.992 0.998 .990 .990

Output Ripple 15 Vp-p 12 Vp-p 7 Vp-p 3 Vp-p 10 Vp-p

Efficiency 95% 96% 97% 97.5 % 96 %

EMI Filter No Yes No Yes Yes

Size 6” x 4.6” x 3” 7” x 2.6” x 2” 9” x 6” x 3.4” 11” x 15” x 3” 13.7” x 3.6” x 4”

Weight 5.5 lb 3.1 lb 10.2 lb 20.8 lb 6.7 lb

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Input Current Waveforms of AC/DC Converters

A) Passive, 12-pulse B) Passive, 18-pulse C) Passive, 30-pulse

D) Active, Boost E) Active, Buck

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Comparison between Active and Passive Approaches

Active Harmonic Reduction (Switch Mode)

Passive Harmonic Reduction (Multi-Phase)

Input Voltages 115 or 230 Vac 115 or 230 Vac

Output Voltages 150 - 230, 320 – 600 Vdc (without use of additional DC/DC converter)

Is regulated over variations in line and load

150 – 600 Vdc (set by adjusting transformer turns ratio)

Varies with line voltage and load

Harmonics THD 3 – 7% THD 3 – 12% (dependent on topology)

Power Factor 0.980- 0.998 0.980 – 0.998

Output Ripple Dependent on output filter Dependent on output filter

Efficiency 95 – 97% 96 – 98%

Soft Start Available with existing design Needs to be added on

Over-current Protection Available with existing design Needs to be added on

Cooling Method Conduction, liquid or air Conduction, liquid or air

Advantages Precise output voltage regulationOutput voltage can be adjustedBuilt in soft-startBuilt in over-current protection/current limitingThe same unit can operate at 400Hz or 60HzSignificantly lower weight at 60 Hz

SimplicityNo need for energy storage devices or controlHigh reliabilityTypical MTBF - 250,000 hoursRobust – accepts high overloadsLower weight at 400 Hz applicationsLower cost

Disadvantages Lower reliabilityHigh energy storage capacitor needed(Aluminum electrolytic)No overload capabilitiesHigher costGap in output voltage setting -Additional DC/DC converter is needed to obtain

Voltage between 230 Vdc and 320 Vdc

No output voltage regulation Input voltage variations are passed to the output, plus

about 4% voltage drop from no load to full loadAdditional DC/DC converter is needed to obtain full

voltage regulationPresence of inrush current - basic designAdditional circuitry is needed to shape input current

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Existing Hardware Examples

4 kW Converter -230Vac/270Vdc

135 kW Converter - 230Vac/540Vdc(Liquid cooled)

5 kW Converter - 230Vac/540Vdc 8 kW Converter - 115Vac/300Vdc(Fan cooled)

15 kW Converter -115Vac/270Vdc

1 kW Converter - 115Vac/270Vdc

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Conclusions

Demands for electrical power on today’s airplane are increasingTraditional, constant frequency power systems are being replaced by variable frequencyDC brushless motor becoming the motor of choice on new airplanes – it requires DC power to operateNew power conversion technologies are needed to fully meet recent power quality requirements – creating new challengesEffective simulation and optimization tools are critical in successful development of new generation aerospace power converters Two groups of technologies, capable of meeting new power quality requirements, are emerging: passive and active approachWhen unregulated DC voltage can be tolerated, multiphase conversion has a good fit in aerospace applications

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More Information

Crane Aerospace & Electronics, Power Solutions, designs, manufactures and supports products and capabilities via our brands: ELDEC, Interpoint and Keltec. We provide both Standard Power Products and Custom Power Products.

• Standard Power Products consist primarily of our DC-DC converter and filter modules sold under the Interpoint brand.

• Custom Power Products consists of our custom and semi-custom low voltage and high voltage power products and subsystems.

• Our Power solutions meet the current and future needs of our customer’s applications:• Power for Electronic Systems – Our full range of standard and custom products delivers

compliant product performance, low cost of ownership and ease of integration thereby providing the lowest risk comprehensive solutions (Ex. Embedded low voltage power supplies)

• Power Distribution – Low weight, high power quality and high efficiency platform power conversion, management and distribution. We can provide significant weight and volume savings through integrated power conversion, bus control and power control. (Ex. TRUs, ATRUs, etc.)

• Electronic Warfare & Radar – Solid-State or traveling wave tube (TWT) based low/high voltage, high power products and subsystems for mission critical defense platform and payload applications (Ex. TWT amplifiers, high power / high voltage power supplies, etc)

• Energy Storage – Delivering safe integration of energy storage devices into electrical systems while providing the longest maintenance interval and service life at the lowest weight. (Ex. Battery systems, battery charger/controller, batteries, etc.)

• Motor Power Conversion and Control – High power quality ac-dc converters as standalone solutions or as part of an integrated electric drive motor package (Ex. ATRUs, active PFC converters, etc.)

Information: www.craneae.comTechnical assistance: Kaz Furmanczyk, Principal Engineer

• Tel. 425-743-8106; e-mail: [email protected]

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25Crane Aerospace and Electronics Proprietary Information

Crane Power SolutionsCrane Power Solutions