Magnetic Optimization of a Fault-Tolerant Linear ...

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Plant weight and size are very large; plant encumbrance is heavily increased by pipes, valves, bulky oil tanks, etc. - Plant complexity and cost is high.
Magnetic Optimization of a Fault-Tolerant Linear Permanent Magnet Modular Actuator for Shipboard Applications M. Bortolozzi(+), C. Bruzzese(*), F. Ferro(*), T. Mazzuca(x), M. Mezzarobba(+), G. Scala(o), A. Tessarolo(+), and D. Zito(*) (+) Dept. of Engineering and Architecture (DIA) University of Trieste - Italy (*) Dept. of Astronautical, Electrical, and Energy Engineering (DIAEE) University of Rome Sapienza - Italy [email protected] (x) Electrical Plants Office Italian Navy's General Staff (MARISTAT) – Italy (o) General Directorate of Naval Armaments Italian Ministry of Defense (NAVARM) - Italy

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Outline of the presentation ● Research about “all electric” ships ● Description of classical oil-powered steering gears ● Mechanical structure of the proposed direct-drive concept ● Magnetic optimization by FEM for force density maximization ● Inverter feeding scheme and winding sizing ● Torque-speed operating area and efficiency ● Laboratory prototype ● Applications: rudders and stabilizing fin drives ● Conclusions

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●“All-electric“ ships are object of growing interest and research ● Electric propulsion (synchronous PM motors, multi-phase or multi-star windings, VSI/CSI converters, azimuth thruster pod drives, etc.) ● Ship electric system (DC transmission, stability, reliability, grid segmentation, harmonic pollution due to converters, coordination of load and generators, high speed turbogenerators, etc.) ● Reasons: more power is needed on modern ships (both commercial and military ships), so propulsion is no more the only relevant load, and a centralized electric power generation becomes convenient (more electrical loads are allowed!) ● A challenging sub-topic concerns the innovation of traditional oil-powered onboard actuators, for steering gears, stabilizing fins, pods, bow-thrusters, launch and lift systems, etc. ● New solutions based on inverter-fed drives are emerging, and also direct-drives (with no reduction gears). 3

Hydraulic steering gear on board ship “Etna“

MANY REDUNDANT OIL SUPPLIES BUT...ONLY ONE MOTOR!

4

induction motor

218 l/min 59bar

i.m.

p.

pilotoperated check valve

two-way electrovalve

75 bar

B

T 26kW

ηim=90%

B1

ηp=81%

75 bar

r.

ηvp=75%

Hydraulic circuit, singlepump rated operation

0.387rpm

Powers and efficiencies are shown

13kW

Overall plant efficiency = 44%

16kW

ηvm=80%

46.2%

44.3%

maximum power operating point rated power operating point

604 STALL

462

v.m.

B2

21kW

Tm(kNm) η(%)

vane motor pressure-relief valve opening

rudder 322kNm

44bar

1750rpm

29kW

pressure-relief valve

vane-motor valve pipes A1 A2 A

P

145Nm

ship grid

pump valve

MAXIMUM TORQUE

Torque-speed curves, with one and two pumps

34Kw

322

RATED TORQUE

26Kw pump pressurerelief valve opening

17Kw

Output powers and efficiencies are shown

13Kw VUOTO

0

0.35 0.39 0.47 SINGLE-PUMP OPERATION

0.7

0.77

TWO-PUMPS OPERATION

0.94

ωm (rpm)

5

Drawbacks of hydrostatic transmissions: - Maintenance is heavy and troublesome. Seals and filters must be routinely checked and replaced (require pump dismounting). Oil refill/replacement is time-consuming and costly. Oil leaks are frequent. - Plant efficiency is low. - Plant weight and size are very large; plant encumbrance is heavily increased by pipes, valves, bulky oil tanks, etc. - Plant complexity and cost is high. - Plant control is slow and sluggish. A continuously running pump is required with relevant no-load losses. - No redundancy for the vane motor. Only the pumps are redundant.

Good features of hydrostatic transmissions: - Very high torques/forces. - Mechanically robust and affordable (with continuous maintenance!) - Simple operating principle 6

PROTECTIVE COVER

PMLSM CONCEPT

ARM

RUDDER STOCK

MOVER HEAD ROTARYPRISMATIC JOINT

BRAKE

STATOR WINDINGS

SLIDER

MOVER WITH MAGNETS

7

8

80

300

310

80

104

9

10

redundant power sources

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INTEGER-SLOT DESIGN

REMOVABLE THREE-PHASE MODULE

the winding end-connections of neighboring modules cannot overlap, so the end connections must be put at least on three orders and they require more space and copper, with higher joule losses.

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FRACTIONAL-SLOT DESIGN

THREE-PHASE MODULE

REMOVABLE SUB-MODULE (TOOTH+COIL)

-Shorter end connections (saving of copper, space, losses) -Smaller air gap force density -The space saved can be used to design a larger module. -Finally, the higher simplicity, modularity and the easier module dismounting, substitution and reparation are the decisive features.

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FEM analysis: Parametric model (integer slot)

+A

-C

+B

-A

+C

-B

F '=

F =B J ' Lx p

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2.05T 1.96T 1.80T 1.47T

2.02T 2.02T 1.93T 1.84T

143kN/m2

150kN/m2

636kN/m3

667kN/m3 +5%

flux density, 5A/mm2(rms) – maximum thrust condition magnet flux and current in quadrature 15

F'(kN/m2)

Force per unit of airgap area vs. parameter 'a'

a(mm) 16

FEM analysis: Parametric model (fractional slot)

F '=

F BJ' = Lx p H H

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QUASI-NEWTON ALGORITHM

SEQUENTIAL NON-LINEAR PROGRAMMING ALGORITHM

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Gradient-based methods may remain trapped in local minima due to FEM numerical noise

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“GEOMETRY STRETCHING” METHOD (GSM)

h

l

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MAX FORCE DENSITY

Force per unit of machine volume (Fv) on the length-height plane (GSM applied to the starting geometry).

Contours of the surface Fv on the length-height plane (values in kN/m 3) (GSM applied to the starting geometry)

(FINAL)

(START)

(FINAL)

(START)

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Force vs Slot current density (integer slots)

157kN/m2

ABOUT +50% MORE THRUST DENSITY THEN IN USUAL COMMERCIAL MOTORS PEAK SHORT-TERM THRUST IN COMMERCIAL MOTORS: 104kN/m2 (TYPE: BALDOR® IRON CORE BRUSHLESS LMIC-71-S-HCO-X) 27

Final drive sizing for rudder application (integer slot) 3 SEPARATE INVERTER

GRID INVERTER1

INVERTER2

INVERTER3

PHASE-COIL

STAR-CENTERS

+ A

C

+ B

A

+ C

B

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Equations for winding sizing ● Nc : Number of turns per coil ● ns, np: Series and parallel coils in a phase current vector

V≈RsI+ωΨm

     

n p ρ lm N c R s = s R coil = np A np  m= n s N c φ m

magnet

V

r Rs m V= F v 3 m r

2

E

I

motor torque

sud I

jXsI RsI

o

S

N

o

90 ψm

electronically-controlled in-quadrature lag VECTOR DIAGRAM

stator current

nord ANALOGOUS ROTARY MACHINE

φm=Fr/3pJA

   

V max r ρl m φ p = F mp m vmp =3.32V  N c / n p  3φ m A r

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ψm

x

   

V max r ρl m φ p = F mp m vmp =3.32V  N c / n p  3φ m A r

F(kN)

v = ω*a

3ΨmV/Rsr

inverter power limit

inverter current limit maximum power operating point (82kW)

inverter voltage limit

137 STALL

160

162

167

182

186

196

MAX FORCE 343 47

65

66

70

82

85

93

27

28

31

39

41

47

16

17

20

449

239

120

0

F=T/ a

15 RATED FORCE

4

HALF RATED FORCE10

10

rated operating point (41kW) 12

0

NO-LOAD

0

0

0

0

0

5 5.5

6.6

9.9

11

13

0

curves of the hydraulic drive

v(cm/s) rV/Ψm

PMLSA working area on the v-F plane. The working area is bounded by the inverter's current and voltage limiting curves (bold lines). The PMLSA input electric power Pe=3VIcosφ is also plotted on the plane.

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F (kN)

F' (kN/m2)

J' = F'/B LINEAR

J' = F'/B+f(B)F'2 343

157 MAX FORCE SATURATED

239

109

0

RATED FORCE

112

200

J'(A/mm)

2.8

5

J(A/mm2)

Resistive power losses P ρ=3 R s I 2=∫ ρ J 2 d = ρ J 2 cu P ρ v , F ≃



2

ρ cu s 2

2

2

  2

2

A B bs hs

F 

2

2 ρ cu s f  B 3

2

2

A B bs hs

Mech. output power

P m v , F =F⋅v

Electr. input power

P e  v , F = P m P ρ= Fvk 1 F k 2 F

Motor efficiency

Pm Pm Fv  PMLSA= ≃ = P e P m P ρ F v ρ J 2 cu

2



3

2

F = k1 F  k2 F

3

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3

CONSTANT EFFICIENCY CURVES

Pm(kW) F (kN)

13

17

26

η(%)

34

0 STALL

14

15

18

25

26

30

343 0 MAX FORCE

26

28

32

42

44

49

44

46

51

61

63

67

449

239

120

0 RATED FORCE

67

76

77

90*

90*

90*

90*

90*

90*

50**

50**

50**

50** 50**

0 HALF RATED FORCE 61

0 NO-LOAD

0

63

rated operating point 81

5 5.5

6.6

9.9

11

50**

v 13 (cm/s)

PMLSA efficiency (4) on the speed-force plane. Dash-dot lines are constant-efficiency loci. Maximum (*) and noload (**) values depend on mechanical friction losses, on stray losses and on additional losses due to inverter feeding, so they have been only approximately evaluated.

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DESIGN AND REALIZATION OF THE PMLSA CONCENTRATED COIL MAGNETS

MODULAR STATOR

MOVER FRAME BEARINGS 34

PROTOTYPED MACHINE

MODULAR STATOR

MAGNETS MOVER

BEARINGS

35

PROTOTYPED MACHINE

MAGNETS LATERAL AXES (FRAME)

MOVER

FOOT

36

PROTOTYPED MACHINE

TOOTH COILS

BACK-IRON

BACK-IRON AND TOOTH ARE INTEGRATED IN A SINGLE PIECE WITH STRUCTURAL FUNCTION

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MEASURED VS PREDICTED FORCE CURRENT AND MAGNET FLUX ARE IN QUADRATURE

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DOUBLE RUDDER (MMI's Ship “Durand de la Penne”) -project under examination by the Italian NavyHYDRAULIC MOTOR TILLER#2

TILLER#1 TRANSMISSION ROD

RUDDER STOCK

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PMLSA

TILLER#2

TILLER#1

THE MOTOR REPLACES THE TRANSMISSION ROD

RUDDER STOCK

Double rudder drive concept

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Stabilizing fin drive concept

41

42

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Conclusions: ●

Oil is really a problem on board ships



Inverter-fed drives are demanded for ships



Direct-drives are preferred for affordability



A PMLSA-based direct drives is proposed



Higher efficiency



Mechanical simplicity

Redundancy and fault tolerance through full modularity (for both inverters and motors) ●

A prototype is under testing for performance verification and fault-tolerant control. ●

THANK YOU FOR YOUR ATTENTION 44

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