Electric Ship Power and Energy System Architecturesdoerry.org/norbert/papers/20170609 Electric Ship...

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Electric Ship Power and Energy System Architectures Dr. Norbert Doerry Dr. John Amy Jr. IEEE ESTS 2017 August Approved for Public Release 1 6/1/2017

Transcript of Electric Ship Power and Energy System Architecturesdoerry.org/norbert/papers/20170609 Electric Ship...

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Electric Ship Power and Energy System Architectures

Dr. Norbert Doerry Dr. John Amy Jr. IEEE ESTS 2017

August

Approved for Public Release 1 6/1/2017

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Agenda

• Naval Power (and Energy Systems

• Existing Ships

• MVAC Architectures

• MVDC Architectures

Dec 8, 2016: DDG 1000 and LCS 2 (US Navy Photo by Ace Rheaume)

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MVAC Architectures

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Integrated Power System (IPS)

IPS consists of an architecture and a set of modules which together provide the basis for designing, procuring, and supporting marine power systems applicable over a broad range of ship types:

– Power Generation Module (PGM)

– Propulsion Motor Module (PMM)

– Power Distribution Module (PDM)

– Power Conversion Module (PCM)

– Power Control (PCON)

– Energy Storage Module (ESM)

– Load (PLM)

March 2009

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IPS Design Opportunities • Support High Power

Mission Systems

• Reduce Number of Prime Movers

• Improve System Efficiency

• Provide General Arrangements Flexibility

• Improve Ship Producibility

• Support Zonal Survivability

• Improve Quality of Service

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161208-N-MB306-079 USS Zumwalt DDG 1000 (US Navy Photo by Zachary Bell)

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Reduce Number of Prime Movers

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Ship’s Power Propulsion

Traditional

Electric

Drive

with

Integrated

Power

GEN

GEN

GEN

GEN

Mtr MD

Mtr MD

GEN

GEN

Power Conversion

and Distribution

Reduction

Gear

Power Conversion

and Distribution

Reduction

Gear

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Improve System Efficiency

• A generator, motor drive and

motor will generally be less

efficient than a reduction

gear ….

• But electric drive enables the

prime mover and propulsor

to be more efficient, as well

as reducing drag.

Mechanical

Drive

Electric

Drive

Gas Turbine 30% 35%

Reduction Gear 99%

Generator 96%

Drive 95%

Motor 98%

Propeller 70% 75%

Relative Drag Coefficient 100% 97%

Total 21% 24%

Ratio 116%

Representative values: not universally true

TRADE TRANSMISSION EFFICIENCY TO REDUCE DRAG

AND IMPROVE PRIME MOVER AND PROPELLER EFFICIENCY

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Improve System Efficiency: Contra-Rotating Propellers

• Increased Efficiency

– Recover Swirl Flow

– 10 – 15% improvement

• Requires special bearings for inner shaft if using common shaft line

• Recent examples feature Pod for aft propeller

http://www.mhi.co.jp/ship/english/htm/crp01.htm

Anders Backlund and Jukka Kuuskoski,

“The Contra Rotating Propeller (CRP)

Concept with a Podded Drive”

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General Arrangements Flexibility Improve Ship Producibility

• Vertical Stacking of Propulsion Components

• Pods • Athwart ship Engine

Mounting • Horizontal Engine

Foundation • Engines in

Superstructure • Distributed

Propulsion • Small Engineering

Spaces

Integrated Power System

Propulsion / Elec tri cal PowerMachinery Space

Intakes/Uptakes

Zones Without Propulsi on / Electr ical Power Spaces

Shaft Lin e

Diesel Mechanical System

12APR94G.CDRNH D: S EA 03R 2Rev 1 28 MAR 95

March 2009 Approved for Public Release

9

9

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Topics • Propulsion

– Motor Types

– Options

• Power Generation

• Power Distribution

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Propulsion Motors: General Observations

• Propulsion Motors are typically custom designed for the application based on standard “Frame Sizes”.

– Frame size determines rotor diameter. – Variables are length and shaft speed.

• The Motor Drive has a large impact on both the Propulsion Motor and the Medium Voltage Distribution System.

– Harmonics and Power Quality – Part Load Efficiency – Number of Motor Phases – Need for Propulsion Transformer

• Motor Designs have changed significantly in past 15 years to take advantage of new high voltage and current power electronics.

– Permanent Magnet (PM) and Advanced Induction Motors (AIM) have largely displaced DC and Synchronous Motors for high power applications.

– Homopolar Motors and Superconducting Motors are still being developed. • High Efficiency at very Low Power levels challenging

– 10% shaft power achieves about 35 - 45% speed – Consider powering only portions of the motor (Motor Drive integration)

• Will likely reduce acoustic performance – Consider mounting two motors on same shaft (Do not need to be the same rating)

• Smallest motor must be large enough to achieve “break-away” torque • Can help with shaft rake • Can reduce torque pulsations on propulsor

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Motors: Basic Scaling Law

HP D2 · L · A · B · RPM

HP Power Rating D Rotor Diameter L Rotor Active Length A Surface Current Density

(Cooling Method) B Rotor Flux Density

(Saturation of Magnetic Material) RPM Shaft Speed

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Propulsion Motor Thumb rules • For a given technology, cost is roughly proportional to

Torque. • As the rated speed of a motor increases, the peak

efficiency occurs at a lower diameter. • Higher rated speeds generally translate into smaller and

more efficient motors. • Maximum Rotor Diameter is limited by shaft rake

considerations, manufacturability, and transportability. • Motor efficiencies at design speed can typically fall in

range of 90-98%. • The efficiency of a conventional motor is relatively flat

above about 25-35% rated speed. Below about 25-35% rated speed, the efficiency drops rapidly.

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• Motor and Motor Drive efficiencies generally high at high power levels.

• At very low power levels, losses are fairly constant at ~1-4% of full power rating – Causes rapid drop off of efficiency below 10% power levels

– This constant level for losses can be approximated by the power delivered to the propeller when the efficiency is 50%.

• Poor efficiency at low power levels for main propulsion make low power auxiliary propulsion units (at about 10-20% of main propulsion rating) attractive.

Motor and Drive Efficiency

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Propulsion Motor Efficiencies

http://www.amsuper.com/products/library/HTS_efficiency_advantage.pdf

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PM motor Efficiency

90

92

94

96

98

100

102

0 10 20 30 40 50

Power (MW)

Eff

icie

nc

y %

PM motor eff

Drive Eff

Interface Eff

Rectifier Eff

Transformer Eff

Overall Eff

PM motor efficiency

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DC Motors

• Pros

– Proven Technology

– Simple Drives

• Cons

– Maintenance Intensive (Brushes)

http://www.tecowestinghouse.com/Products/Custom_Engineered/DC.html

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AC Synchronous Motors

• Pros

– Proven Technology

– Simple Drive Systems

– High Efficiencies

• Cons

– Large and Heavy

– More expensive and complex than Induction Motors

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Advanced Induction Motors

• Pros – Proven Technology

– Modern Drives enable higher efficiencies

• Cons – Large and Heavy

– Efficiencies still not as high as other motor types

http://www.powerconv.alstom.com/home/

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Permanent Magnet Motors

• Pros – Low Weight

– Quieter

– Better part load efficiency

• Cons – Developmental

– Cost

Removable

Permanent

Magnet

Rotor

Removable

Stator

Segment

Housing http://www.drs.com

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Homopolar Motors

• Pros – True DC Motor

– Low Noise

– Low torque pulsations

– Low Weight

– Small Size

• Cons – Developmental

– Low Voltage, High Current

– High-Current Brushes

http://www.ga.com/atg/homo.php

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Superconducting Motors

• Generally either Synchronous Machines or Homopolar

• Can achieve significantly higher magnetic flux densities

• Promises to significantly reduce the size and weight of Propulsion Motors

Cooler Module

Housing

Back Iron

Stator Windings

Brushless Exciter

Composite Support Tube

Rotor Assembly

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Propulsion Options

• Conventional

• Pods

• Contra-Rotating

• Waterjets

• Distributed

• Hybrid

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Conventional

• Shafts arranged similar to mechanical drive.

• Electric Drive enables – Shorter Shafts

– Eliminate rake on prime movers

• Simplify foundations

• Can Lower Center of Gravity of Prime Mover

Single Shaft Commercial Electric Drive

1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0

AP FP

0 20 40 60 MSCALE

ASSET/MONOSC V4.4.0 - MACHINERY MODULE - 4/ 6/1999 7:44.54DATABANK-RAILGUN_V44.BNK SHIP-IPS PULSE LM2500GRAPHIC DISPLAY NO. 1 - SHIP MACHINERY LAYOUT

Twin Shaft Military IPS Concept

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Pods / Azimuth Thruster

• Increase propulsor efficiency

• Eliminates Shaft Alignment issues

• Maintainability an issue.

• Commonly found on Cruise Ships – Commercially available up to

the 25,000 HP range

• Pods are not currently used for main propulsion on Naval Warships

Approved for Public Release

Siemens AG

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Contra-Rotating

• Increased Efficiency

– Recover Swirl Flow

– 10 – 15% improvement

• Requires special bearings for inner shaft if using common shaft line

• Potential Acoustic Issues

• Recent examples feature Pod for aft propeller

http://www.mhi.co.jp/ship/english/htm/crp01.htm

Anders Backlund and Jukka Kuuskoski,

“The Contra Rotating Propeller (CRP)

Concept with a Podded Drive”

6/1/2017

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Waterjets

Generally axial flow pumps - direct drive or geared from high-speed diesels or gas turbines

Typically with inlet in the bottom; jet from the transom

Thrust can be obtained from the Momentum Equation

T = m(Vout – Vin)

Competitive with propellers above 35-40 knots

Used in high speed ferries, yachts, and naval vessels

Design matching is done on

thrust/resistance rather than power

Alexander’s modified PC

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Distributed Propulsion

• Apply Zonal Design concept to Propulsion – Weapons effects can

damage both shafts in a conventional twin shaft ship

• Forward Propulsors can interfere with bow mounted sonar performance

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Hybrid Propulsion

• Combines Mechanical Drive and Electric Drive on same Shaft

• Ideal for ships that spend most of their time loitering, but have a high maximum speed requirement

Gas Turbine Mechanical

Drive with Auxiliary

Propulsion Motor

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Power Generation Topology and Ratings Guidance

• Choose Efficient Power Generation Modules for the Endurance Condition

– Typically requires 2 PGMs online or 1 PGM and an ESM for QOS

– Diesels often attractive for this condition

• For other than emergency PGMs, the minimum rating of a PGM should be the worst case condition sum of all un-interruptible and short term interruptible loads (less 5 minute rating of ESM)

• Consider Gas Turbines for achieving Maximum / Sustained Speed Requirements

– Lower Weight and Volume

• Power Generation Modules should be longitudinally distributed such that loss of two adjacent zones will leave undamaged zones with sufficient power to service all surviving loads.

• Have at least 2 PGMs that are self starting – Locate as far apart as possible for survivability

considerations – Serve as Emergency Generators – Each should be rated to at serve all emergency loads

plus have ability to start all other PGMs in sequence. • Emergency loads are a subset of “vital” loads

1.0 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0.0

AP FP

0 20 40 60 MSCALE

ASSET/MONOSC V4.4.0 - MACHINERY MODULE - 4/ 6/1999 7:44.54DATABANK-RAILGUN_V44.BNK SHIP-IPS PULSE LM2500GRAPHIC DISPLAY NO. 1 - SHIP MACHINERY LAYOUT

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Commercial IPS Example

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MVAC Zonal Example

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Power Generation Considerations • Past Studies have shown that 4 to 6 prime movers typically provide the best trade-off

of cost, weight, survivability, and Quality of Service • For QOS, must always have at least two sources of power on-line (one may be energy

storage module) – The rating of the smaller source should be greater than the sum of the un-interruptible and

short-term interrupt loads.

• For the Endurance conditions, the on-line power generation modules should be operating in the flat tail of the SFC curve

– Each type of prime mover has a minimum load for efficient operation (can range from 25% to 80%)

• Prime Movers paralleled via ac power (and not providing propulsion power) should not be loaded more than 95% to account for dynamics in load sharing and variance of the instantaneous ship service power around its average value

– The percentage for sharing via dc power has not yet been determined but will likely not be below 95%.

– With suitable controls, a propulsion motor module can provide the needed flexibility to deal with ship service power variance.

• For Survivability, Sufficient separation of prime movers should be provided such that the loss of generation in any two adjacent zones should leave enough generation capacity to service all remaining non-propulsion loads in the remaining undamaged zones.

– Some Propulsion capability should remain.

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Diesel vs Gas Turbine

Diesels: • Fast Starting • Fuel Efficient • Smaller intakes • Smaller uptakes • Greater Variety

Gas Turbines: • Power Dense

•Weight •Volume

• Lower emissions

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IPS Propulsion Generator

• 21 MW - 26.25 MVA

• 4160 V - 3 Phase

• 60 HZ - .8 Pwr Fctr

• 2 Pole - 3600 RPM

• 97 % Efficiency

• 50,050 KG

• 3.4m(H) x 4.7m(L) x 4m(W)

• Mfd. by: Brush Electric Machines Company (UK)

Courtesy of Timothy J. McCoy © 2003

Approved for Public Release

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Generation Requirements

Speed-Power

(knots - SHP)

Curve

Generation Requirements

• Maximum Margined Load

• Un-interruptible, Short Term

Interrupt, and Long Term

Interrupt Power Requirements

per operating condition

• Endurance Power

requirements

Motor / Motor Drive

Efficiency Curve

Total Load Estimate

Speed –

Propulsion Power

(Electrical)

Curve

Endurance Information • Endurance Speed and Range

or

• Speed -Time Profile &

Endurance Time

Margin and

Service Life Policy

Prime Mover

Specific Fuel

Consumption

Curves

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Speed – Power Curve

• How to calculate – Bare Hull Drag

• Synthesis and specialized computer Tools

• Standard Series • Scaling from existing ships

– Propeller Characteristics – Power Margin Factor – Ship Propeller interaction – Bearing and Shafting Efficiencies

• Standard Assumptions – Clean Bottom – Calm Seas – Deep Water – Full Load Displacement

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Motor and Motor Drive Efficiency Curves

• Where to Find

– Manufacturer’s Data

– Generalized estimates

• A healthy skepticism with respect to data is always good.

0

10

20

30

40

50

60

70

80

90

100

0 20 40 60 80 100

Power (% of full load)

Eff

icie

nc

y (

%)

IPS PWM

Notional LCI

Courtesy of Timothy J. McCoy © 2003

Motor Drive Efficiency

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http://www.amsuper.com/products/library/HTS_efficiency_advantage.pdf

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Prime Mover Specific Fuel Consumption

Courtesy of Timothy J. McCoy © 2003

0

100

200

300

400

500

600

700

0 10 20 30 40 50 60 70 80 90 100

Power Output (%)

SF

C (

g/k

W-h

r)

GT (ICR)

GT (simple)

Diesel(low spd)

Diesel(med spd)

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How do you Estimate the Total Ship Service Load?

• Analogy & Parametric – Scale from other ships

• Synthesis Tool – Let embedded routines do the estimate

• EPLA – Load Factors (See DDS 310-1) – “Works” only if you have a large number of relatively small loads. – Must account for “Large Loads”, starting large motors, and inrush current. – Appropriate for large ships power generation sizing – Appropriate for early stage design of in-zone components

• EPLA – Stochastic Method (See DDS 310-1) – Calculate probability of power load for different operating conditions. – Determine required generation capability to achieve an acceptable

probability for meeting demand based on Quality of Service

• EPLA – Modeling and Simulation (See DDS 310-1) – Quasi-static modeling of loads and controls

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Margin and Service Life Allowance

Includes Service Life Allowance

Allowance

NAVSEA T9300-AF-PRO-020

NOTE: SLA does not apply to

- Propulsion plant

- Steering systems

- Replenishment systems

- Mechanical handling systems

- Deballasting systems

NOTE: Margins and

SLA only apply to

Ship Service Loads

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Endurance

• Desire for Power Generation Modules and Propulsion Motor Modules to be efficient for endurance conditions – Endurance calculations size the fuel

tanks and have a major impact on Full Load Displacement’

• DDS 200-1 Rev 1 Defines three possible endurance conditions – Economical Transit

– Surge to Theater

– Operational Presence

160222-N-MD297-180: DDG 82 and T-AO 200 (USN Phot by Huey D. Younger Jr.)

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Growth of Mission System Loads

• Future non-mobility Mission Systems will likely drive fuel requirements more than propulsion

• Endurance Range and Speed may no longer be appropriate for sizing fuel tanks

0

5

10

15

20

25

30

35

DD-963 DDG-51 Flt

IIA

DDG-1000 AP Study

Medium

Combatant

Ele

ctr

ic L

oad

, M

W

Alternate

Propulsion

Study

Medium

Combatant

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Calculating Total Power Generation Required

• Maximum Propulsion Power – Calculate the Shaft Power for the Sustained Speed (include Power

Margin Factor)

– Multiply by 1.25 (definition of sustained speed)

– Divide by the efficiency of the Propulsion Motor Module. (convert to electrical power)

• Calculate Propulsion Power at other condition speeds – Include Power Margin Factor and correct for PMM efficiency

• For each operational condition, add the maximum ship service electrical load to the appropriate propulsion power – Include margin and service life allowance in the ship service

electrical load

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Power Generation Sizing vs. Energy Storage

Un-interruptible

Short

Term

Interrupt

Long

Term

Interrupt

Large

Generator

Set

(Online)

Large

Generator

Set

(Standby)

Small

Generator

Set

(Online)

Energy

Storage Energy

Storage Po

wer

Load Option A Option C Option B

Small

Generator

Set

(Standby)

Small

Generator

Set

(Online)

Large

Generator

Set

(Standby)

Large

Generator

Set

(Online)

Small

Gen Set

(Online)

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Power Generation Fuel Consumption

• Ship Fuel consumption rate depends on plant line-up and PGM efficiencies

1 WR-21 + 1 501-K34

2 WR-21

2 WR-21 + 2 501-K34

•Plant line-up must consider QOS, fault current, and survivability •Usually requires at least 2 prime movers on line (unless sufficient Energy Storage is available)

1 WR-21 + 1 Diesel

2 Diesel

2 WR-21

2 WR-21 + 2 Diesel

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Power Management

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Load Shed Strategy

• QOS Load Shedding – Shed long-term interrupt loads first – regardless of

mission priority. – Bring stand-by generator online and restore long-term

interrupt loads before 5 minutes

• Mission Priority Load Shedding – If unable to restore long-term interrupt loads within 5

minutes, or if shedding long-term interrupt loads is not sufficient

• Shed the lowest mission priority loads regardless of QOS category (typically propulsion allocated power)

• At five minutes, restore those long-term interrupt loads with a higher mission priority by shedding other lower mission priority loads.

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Mission Prioritization Load Shedding

Restricted Maneuverability

Normal Ops

GQ - AAW

Transit

Anchor

Operational Scenarios Load Priorities Prior ity Load Item

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Com bat System

Com m unications

Active Sonar

Zone N Hotel

Priority Load Item

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Com bat System

Com m unications

Active Sonar

Zone N Hotel

Prior ity Load Item

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Com bat System

Com m unications

Active Sonar

Zone N Hotel

Priority Load Item

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Com bat System

Com m unications

Active Sonar

Zone N Hotel

Prior ity Load Item

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Com bat System

Com m unications

Active Sonar

Zone N Hotel

Priority Load Ite m

1

2

3

4

5

6

N

Propulsion Increment

Propulsion Increment

Propulsion Increment

Combat System

Communications

Active Sonar

Zone N Hotel

Load ItemAllocated

Pwr (KW)

Allocated

Pwr (KVAR)

Allocated

Pwr (KVAR)

Allocated

Pwr (KW)

Level of

Control Location

Steady State Startup

Combat Sys

Comms

Active Sonar

Zone 1 Hotel

Zone 2 Hotel

Zone N Hotel

PMM-1 (A)

150

100

200

50

75

25

1000

N/A

N/A

N/A

N/A

N/A

N/A

500

N/A

N/A

N/A

N/A

N/A

N/A

100

150

100

200

50

75

25

1000

Open / Close

Open / Close

Open only

Open only

Open / Close

Open only

N/A

Zone X/PCM2/ID4

etc

Load Characteristics Definition

• Propulsion power broken down into incremental discrete loads.

• Equipment which is off-line is allocated no power. • Operational Scenario Descriptions (OSDs) do not

include PGM line up. Courtesy of Timothy J. McCoy © 2003

6/1/2017

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Approved for Public Release 50

Example: Loss of First Generator

Un-interruptible

Short

Term

Interrupt

Long

Term

Interrupt

Generator

Set A

(Online) Po

wer

Load Supply

Initial Configuration

Generator

Set C

(Standby)

Generator

Set B

(Online)

Un-interruptible

Short

Term

Interrupt

QOS

Shed

Loads

Generator

Set A

(Online)

Generator

Set C

(Standby)

Generator

Set B

(Offline)

Load Supply

QOS Shedding

Un-interruptible

Short

Term

Interrupt

Generator

Set A

(Online)

Generator

Set C

(Online)

Generator

Set B

(Offline)

Load Supply

Service Restored

Long

Term

Interrupt

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Approved for Public Release 51

Example: Loss of Second Generator

Un-interruptible

Short

Term

Interrupt

Long

Term

Interrupt

Generator

Set A

(Online) Po

wer

Load Supply

Initial Configuration

Generator

Set B

(Offline)

Generator

Set C

(Online)

Un-interruptible

Short

Term

Interrupt

QOS

Shed

Loads

Generator

Set A

(Online)

Generator

Set B

(Offline)

Generator

Set C

(Offline)

Load Supply

QOS Shedding

Long

Term

Interrupt Generator

Set A

(Online)

Generator

Set C

(Offline)

Generator

Set B

(Offline)

Load Supply

Mission Priority Load Shed

Mission

Priority

Shed

Loads

Short

Term

6/1/2017

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MVDC Architectures

Approved for Public Release 52 6/1/2017

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Why Medium Voltage DC? • Decouple prime mover speed from power quality

– Minimize energy storage

• Power conversion can operate at high frequency – Improve power density

• Potentially less aggregate power electronics – Share rectification stages

• Cable ampacity does not depend on power factor or skin effect

• Power Electronics can control fault currents – Use disconnects instead of circuit breakers

• Acoustic Signature improvements • Easier and faster paralleling of generators

– May reduce energy storage requirements

• Ability to use high speed power turbines on gas turbines

Approved for Public Release 53

Affordably meet electrical power demands of future destroyer

An AC Integrated Power System would likely require future

destroyer to displace greater than 10,000 mt

6/1/2017

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MVDC Reference Architecture

Approved for Public Release 54 6/1/2017

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Alternate MVDC Architecture

Approved for Public Release 55 6/1/2017

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MVDC Voltage Standards

• MVDC nominal voltages based on IEEE 1709 – 6000 VDC – 12000 VDC – 18000 VDC

• Current levels and Power Electronic Devices constrain voltage selection – 4000 amps is practical limit for mechanical switches – Power electronic device voltages increasing with time (SiC

will lead to great increase)

• For now, 12000 VDC appears a good target … • Power Quality requirements TBD

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Bus Nodes

• Segment MVDC Bus – Disconnects

• Isolate loads – Disconnects

• Isolate sources – Breaker – Disconnect if Breaker

functionality in source

• Establishes Ground Reference for MVDC Bus – If functionality not

provided in source

Next Zone

Next Zone

PC

M 1

A

MV

DC

Lo

ad

PG

M

Ground Reference Device

Possibly integrated with PCM 1A and PGM

Disconnect if Functionality

integrated with PCM 1A and

PGM

Multi-Function Monitor (MFM)

If needed for fault

management

Approved for Public Release 57 6/1/2017

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Power Generation Modules

• Split Windings – Reduced Impact on

prime mover due to fault on one MVDC bus

– Simplifies “odd number of generators” dilemma

• May enable reducing ampacity of MVDC bus

• Consider Fuel Cells in the future

PM Gen

Rectifier

Rectifier

To Bus Node

To Bus Node

Generator has 2 independent sets of windings

Approved for Public Release 58

Normally open

6/1/2017

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Propulsion Motor Modules

• Typically two motors for reliability – May share housing

• Normally powered by both MVDC busses

• Requires control interface for load management

• Consider contra-rotating propellers for fuel efficiency and minimizing installed electrical power generation capacity

Motor

Drive

Drive

To Bus Node

To Bus Node

Motor

Approved for Public Release 59

Normally open

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PCM-1A / Energy

• Protects the MVDC bus from in-zone faults • Provides hold up power while clearing faults on the MVDC Bus • If desired, provides hold up power while standby generator starts • If desired, contributes to energy storage for pulse power loads • Provides conditioned power to loads • Provides power to loads up to several MW (Lasers, Radars, Electronic Warfare) • Provides power to “down-stream” power conversion (IPNC) • Near term applications could use I-modules with AC inputs in “Energy Magazine”

configuration

Approved for Public Release 60

ESM

Bus Node

I-module

O-module

O-module

O-module

IPNC

loads

PCM-1A

Internal DC Bus

I-module

ESM = Energy Storage Module IPNC = Integrated Power Node Center I-module = Input Module O-module = Output Module

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Integrated Power Node Center (IPNC)

• Update MIL-PRF-32272 – Include 1000 VDC input modules – Include provision for energy

storage for ~1 second • allow 450 VAC LCs in zone and in

adjacent zone to reconfigure.

• Zone may have multiple IPNCs • Supply

– Un-interruptible loads – Supply loads with special power

needs. • 400 Hz. • VSD motor loads • Perhaps Low voltage DC Loads

Approved for Public Release 61 6/1/2017

Courtesy L3

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Notional Electromagnetic Railgun

• PCM-1B = Modular Power Conversion – 10’s of MW – Powers Mount equipment

in addition to Pulse Forming Networks (PFN)

• Normally powered by both MVDC busses

• Requires control interface for load management

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Issues needing resolution

• Power Management • Energy Storage / Energy Management • System Stability • Bus Regulation • Prime Mover Regulation • Fault Detection, Localization and Isolation • System Grounding • Magnetic Signature • Affordability

Approved for Public Release 63

Need resolution by 2025 to support 2030 Lead Ship Contract Award

6/1/2017

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Summary

• Power and energy density needs of a future destroyer with large pulse loads suggest a preference for MVDC

• An MVDC system must be affordable

• A number of technical issues need to be resolved in the next decade

Approved for Public Release 64 6/1/2017