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www.HowFliesTheAlbatross.com Permanent-magnet motor- generator or starter-generator Review & Renew J. Philip Barnes 14 Sept 2015 Any electric motor is a generator and vice versa “Motor-generator” applications: electric vehicles “Starter-gen.” applications: aircraft APUs/engines Assumed herein: “permanent magnet” behavior Classical brushed-DC, or typical 3-phase brushless Introduced herein: “4-constant equivalent DC” model Efficiency Vs. non-dim. speed, voltage, current, torque Predict motor-generator performance at any voltage New, fundamental, previously-unpublished formulas

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Page 1: Www.HowFliesTheAlbatross.com Permanent-magnet motor-generator or starter-generator Review & Renew J. Philip Barnes 14 Sept 2015 Any electric motor is a

www.HowFliesTheAlbatross.com

Permanent-magnet motor-generatoror starter-generator Review & Renew

J. Philip Barnes 14 Sept 2015

• Any electric motor is a generator and vice versa• “Motor-generator” applications: electric vehicles• “Starter-gen.” applications: aircraft APUs/engines

• Assumed herein: “permanent magnet” behavior– Classical brushed-DC, or typical 3-phase brushless

• Introduced herein: “4-constant equivalent DC” model – Efficiency Vs. non-dim. speed, voltage, current, torque– Predict motor-generator performance at any voltage– New, fundamental, previously-unpublished formulas

Page 2: Www.HowFliesTheAlbatross.com Permanent-magnet motor-generator or starter-generator Review & Renew J. Philip Barnes 14 Sept 2015 Any electric motor is a

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e

t

w

E

N turns

Generating

i

vi vq

Fp

Fq

B

iChange to generator mode:Same direction, rotation, wSame sign for EMF, e Sign change of torque, t Sign change of current, i

Electromotive force, e= potential energy / charge= work / charge, (Fp / q) L= 2 N w (D/2) B L e = NDBL w ≡ k w

Torque, t = 2N (D/2) B (dx/dt) dq = 2N (D/2) B (dq/dt) dxt = NDBiL = NDBL i = k i

(+) Charge (q) with velocity, V in magnetic field of strength, B:Force vector, F = q V x B

e

tw

E

N turns

Motoring

B

i

vi vq

Fp

Fqi

L

Brushed-DC motor-generator fundamental characteristics

k =“EMF const.”k = /e w = t/iVolts/(rad/s)or N-m/Amp

Model aircraft: “Kv” RPM/Volt

= 60/(2pk)

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“Equivalent DC” machine

eb

iInverter-Rectifier

= t ki ±l

w

emg

kwR

“Equivalent-DC” brushless machine + inverter/rectifier

BLDC system has same characteristics of classic brushed-DC:• 2-wire interface with the battery (or power source) • Motor-generator EMF proportional to rotation speed, (w)• Torque (t), +/- fixed loss (l), is proportional to current (i)• System resistance (R) incl. batt., cables, & M-G windings• “Battery” can be supercap., other gen., or power supply• “Chopping loss” not included (Inverter at 100% duty cycle)

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Brushless motor with “six-pack” inverter-rectifier

• Inverter converts 2-wire DC to 3-wire "AC“• Alternating transistor “diagonal pairs”• Commutation toggles each phase 0-to-VB

• Relatively low frequency, 100% duty cycle

VB

VB

12

3

1

2

3-7V 15V S

N

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Brushless generator with “six-pack” inverter-rectifier

eB

12

3

• M-G max delta EMF exceeds battery EMF• Six-pack rectifies 3-wire AC into 2-wire DC• Battery recharged through flyback diodes• IGBTs unidirectional: commutation ignored

Snapshote1 - e3 > eB

1

2

3

~ “DC” current

Diodes provide"free" regen!

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i

= t k i - l

w

eb

R emg = kw

Motoring

i

= t k i +l

w

eb

R emg = kw

Generating

Phil Barnes Sept 2015

4-constant “Equivalent-DC” starter/motor-generator model

1. Definitions:EMF ratio, n ≡ emg/eb

Fixed torque loss, lEMF const., k = emg/w = ( +t l)/iSystem resistance, R

2. Simple circuit model:Non-dim current, iR/eb = 1-nSystem efficiency, h = tw/(ebi)

Combine circuit model EQs:“4-const. Equiv. DC” modelmotor: n < 1 - lR/(keb):

Generator: n > 1, h = ebi /(tw):

Model accommodates motor, gen, or motor-genModel predicts M-G performance at any VoltageFixed torque loss (l) ≈ 0.8% of stall torque, keb/RTorque loss and resistance (R) degrade efficiencyNeglecting losses, motor efficiency = EMF ratioNeglecting losses, gen. efficiency = 1 / EMF ratioNext chart: 4-constant model matches test data

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0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6

System efficiency,tw/(ebi)

orebi/(tw)

n ≡ EMF ratio, emg /eb = k w /eb = speed ratio, w / (eb /k)

Starter/motor-generator system efficiency (h)Brushed-DC or Brushless with inverter/rectifier Sys.

"4-const. EqDC" model, sys. resistance (R) & fixed torque loss (l)eb = battery EMF, k = EMF constant, t = torque, w = rotation speed

motor and battery

generator & battery

ideal motor system

ideal generator sys.

test_data

, l N-m ≈ 0.0065 k eb / R

GENERATINGLMCLTD.neteb=48V / 3,600 RPMk = 0.16 N-m/AR = 0.041 Ohm

MOTORINGVisForVoltage.org1-HP Scott motoreb=24V / 15,000 RPMk = 0.070 N-m/AR = 0.054 Ohm

4-constant EqDC model, motor 4-constant EqDC model, generator

, l N-m ≈ 0.010 k eb / R

Phil

Barn

es S

ept 2

015

4-constant “Equivalent-DC” model matches test data

Ideal motorin

g =

h

n Ideal generating = 1/h

n

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-0.3

-0.2

-0.1

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 1.1 1.2 1.3

Torque group, tR/(keb) or

Current group,i R / eb

n ≡ EMF ratio, emg /eb = k w /eb = speed ratio, w / (eb /k)

"4-const. equiv.-DC" model: Starter-genor motor-gen. system efficiency & non-dim. speed, current, & torque

4-constant “Equivalent-DC” model: Torque and Current

Non-dimensional rotation speed: n = w / (eb

/k)Non-dim. torque: t R / (k eb ) ≈ 1-n- l R/(keb ) Non-dim. current: i R/eb = 1-nTorque & current change sign, generator mode

, l N-m ≈ 0.0065 k eb / R

GENERATINGLMCLTD.neteb=48V / 3,600 RPMk = 0.16 N-m/AR = 0.041 Ohm

MOTORINGVisForVoltage.org1-HP Scott motoreb=24V / 15,000 RPMk = 0.070 N-m/AR = 0.054 Ohm , l N-m ≈ 0.010 k eb / R

Current group, i R/eb

Torque group, t R/(keb )

Motor eff., tw/(e b

i)

Gen eff., eb i/(tw)

Lines/curves: modelsymbols: test data

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Brushless machine commutation and speed control

Commutation “accommodates” RPM, matching fields & magnets

TerminalVoltage

Battery

ground

Pulse-width modulation (PWM),superimposed on commutation, indirectly “controls” speed bychopping current, & thus torque

Whether or not the machine is “sensorless,” rotor position or phase EMF is sensed for commutation

• Commutation “accommodates” the existing RPM• Relatively low frequency, order ~100-1000 Hz

• PWM reduces speed via chopping at duty cycle (d)• PWM is applied only to “upper” 6-pack IGBTs• Relatively high frequency, order ~20 kHz• Switching loss prompts alternate architectures• Also, PWM is not well suited for regeneration

| |

dt| t |

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DC boost architecture – increased capability and efficiency

"Evaluation of 2004 Toyota Prius,"Oakridge National Lab, U.S. Dept. of Energy

233 Vdc in

5 10 15 20 kW

Regen

M-G

Motor

PWMiGBT

CL VB

• DC boost architecture enables efficient bi-directional power• Age-old regen problem: reduced motor-gen RPM & EMF < battery• DC boost converter (DCBC) amplifies either battery or MG Voltage• Low-Voltage PWM duty cycle at IGBT gate sets DCBC Voltage gain• Highest system efficiency, with or without interest in regeneration• For starter-gen, DCBC is well suited to adjust torque-speed profile

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System efficiency and current with DC boost converter

ib /Gb

tw

Gb

Rh kw

eb

Rh

ib

a

Motoring

Gm ib

tw

Gm

Rh kw

eb

Rh

ib

a

Generating

ib = [eb Gb2- Gb kw] / [Rh (1+Gb

2)] motoring

ib = [kwGm - eb] / [Rh (1+Gm2)] regeneration

G ≡ DCBC voltage gain

• Get sys. efficiency & battery current for DC boost architecture• With the DCBC, current “gain” is inverse of Voltage gain (G)• Boost battery Voltage to motor ; otherwise boost MG Voltage• Say “half resistance (Rh)” resides up & downstream of DCBC• Solve for Voltage at node “a” to get battery current by mode• Efficiency has trends shown earlier, but Vs. ne ≡ Gmkw/(Gbeb)

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Summary: PM Motor-generator Review & Renew

• Assumed: “permanent-magnet-type” behavior• Review: Classic brushed-DC machine principles • Renew: Brushless + inverter/rectifier “Equiv. DC”• Review: “Six-pack” inverter & rectifier operation• Renew: New formulas for system efficiency• Renew: Non-dimensional speed, torque, current• Renew: New methods validated by test data• Review: “Chop” Vs. “DC boost” speed control• Renew: System efficiency & current with DCBC

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Phil Barnes has a Master’s Degree in Aero Engineering from Cal Poly Pomona and BSME from the University of Arizona. He is a 35-year veteran of air vehicle, propulsion, and subsystems performance analysis at Northrop Grumman. Phil authored a “landmark” study of dynamic soaring, and he is pioneering the science of regenerative electric flight. Author of numerous SAE, AIAA, and other technical papers, he is often invited to present travel-paid lectures at various universities. The charter of his free website is to apply “green aero engineering” to help prevent or delay extinction of the wandering albatross.

About the Author