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Underwater Thermoelectric Generator P14254 10/8/2013 Rochester Institute of Technology

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Underwater Thermoelectric Generator P14254. Agenda. Background Problem Statement Customer Requirements Engineering Requirements House of Quality System Analysis Functional Decomposition Concept & Architecture Development Engineering Analysis Risk Assessment Test Plan Project Plan. - PowerPoint PPT Presentation

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Page 1: Underwater Thermoelectric Generator P14254

Underwater Thermoelectric GeneratorP14254

10/8/2013 Rochester Institute of Technology

Page 2: Underwater Thermoelectric Generator P14254

Rochester Institute of Technology

Agenda

◼ Background◼ Problem Statement◼ Customer Requirements◼ Engineering Requirements◼ House of Quality

◼ System Analysis◼ Functional Decomposition◼ Concept & Architecture Development

◼ Engineering Analysis◼ Risk Assessment◼ Test Plan◼ Project Plan

10/8/2013

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Rochester Institute of Technology

Discussion Points

● Heat Sinking● Materials● External vs. System Electronics Power Source

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Rochester Institute of Technology

Background

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Background Information

BOEING’S UUV, ECHO RANGER

▪ Developed in 2001 for seafloor mapping for oil/gas industry

▪ Currently testing the idea for potential military applications▪ ISR▪ Harbor security

▪ Current run time ▪ ~28 hours

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Rochester Institute of Technology

Background Information

• Boeing wants to extend the mission time of their submarine

• They are interested in thermoelectrics

• Our Task: Prepare a proof-of-concept underwater thermoelectric generator that charges a battery.

10/8/2013

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Project Updates

Since last time...

◼ Battery voltage: 12V◼ Battery capacity: 750mAhr◼ Battery type: Li-ion◼ Emphasis on thermoelectric

and total system efficiency

❏ Was undecided❏ Was undecided❏ Was Li-Poly❏ We will not put much

emphasis on specific heat source

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Rochester Institute of Technology

Customer Requirements

◼ Continuously generate power◼ Operate efficiently◼ Charge a battery◼ Operate underwater◼ Heat source provides a constant source of

heat◼ System can withstand interior enclosure

temperature◼ Utilize passive safety features

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Engineering Requirements

◼ Power Output: 20W◼ Heat Source Power Input: 500W◼ Upper Ambient Operating Temperature: 30°C◼Thermal Overload Protection: 10% of max T◼Operates Without User Input: 0 interactions◼ Heat Source Temperature: Ideally 300°C

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Rochester Institute of Technology

House of Quality

10/8/2013

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Rochester Institute of Technology

System Analysis

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Rochester Institute of Technology

Functional Decomposition

Generate Electrical

Power

Protect System

Resist Operating

Temperature

Operate Under Water

Resist Corrosion

Resist Pressure

Resist H20 Ingress

Generate Heat

Use Electric Heater

Transfer Heat

Spread Heat Reject Heat

Generate Electricity

Utilize Temperature Difference

Store Energy

Charge Battery

Transfer Electricity

Monitor Systems

Measure Power

(Power input and output)

Measure Ambient Conditions

(Temperature, humidity,

moisture content, pressure)

Resist Operating

Temperature

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Rochester Institute of Technology

Mechanical System Level View

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Rochester Institute of Technology

Thermal System Level View

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Red arrows are lost heat.

Main heat path: Source TEG Sink Water

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Electrical System Level 0

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Electrical System Level 1

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Rochester Institute of Technology

vv

Instrumentation System Level View

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Rochester Institute of Technology

Morphological Chart

*Ideas in red have proven to be not feasible

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  Functions

Means Generate Heat

Spread Heat

Monitor Systems

Reject Heat

Enclosure Material

Enclosure Shape

Thermo-electrics Seal

1Cartridge Electric Heater

Air Embedded Microcontrollers Pump

Non-corrosive metal

enclusure

Rectangular Prism stacked Vacuum

2 Film Electric Heater Oil External

Computer Fan Ceramic Sphere single duct tape

3Resistor Electric Heater

Water Tactile Metallic Fins Plastic Cylinder top/bottom electrical

tape

4 Burning Copper   Insulator Rubber Dumbbell all sides gasket

5 Friction Wheel Aluminum     Rigid metals Hexagonal

Prism   o-rings

6   Steel     Polycarbonate Octagon   weld

7         Polycarbonate/Metal Hybrid     epoxy

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Rochester Institute of Technology10/8/2013

Criteria Solution 1 Solution 3 Solution 7 Solution 8 Solution 9Allowable Enclosure Temp 0 + 0 - 0Electronics temp 0 + 0 + +Autonomous 0 - 0 0 0Compact 0 - - 0 -Cost 0 - - - -

Easy of Assembly/Disassembly 0 + 0 - -Ease of Waterproofing 0 - 0 - -Easy to Troubleshoot 0 - - - +Efficiency of Thermoelectrics 0 0 + 0 0Cold Side Temperature 0 + + 0 0Manufacturability 0 - 0 - -Number of Gerbils 0 0 0 0 0Safe 0 + 0 0 0Weight 0 0 0 + 0

DATUM+ 5 2 2 2- 6 3 6 5

Function Solution 1 Solution 3 Solution 7 Solution 8 Solution 9Generate Heat Cartridge Cartridge Cartridge Cartridge CartridgeSpread Heat Copper Copper Copper Copper CopperMonitor Microcontrollers Ext Comp Microcontroller Microcontrollers MicrocontrollerReject Heat Fins Fins Fins Fins Fins

Enclosure Material Non Corrosive Metal Ceramic Non Corrosive Metal

Polycarbonate/Metal Hybrid Non Corrosive Metal

Enclosure Shape Rectangular Prism Dumbbell Rectangular Prism Rectangular Prism Dumbbell

Thermoelectrics Electrical Configuration Series Series Series Series Series

Thermoelectrics Mechanical Configuration All Sides All Sides All Sides - Double

Stacked TE's All Sides All Sides

Seal/Protect Gasket Gasket Gasket Gasket Gasket

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Pugh Conclusions

• Shapes: The simple rectangular prism won.• No External Control: We are going to have a

microcontroller anyway• Enclosure Material: Thermoelectric side will

need non-corrosive metal, electronics side can be plastic.

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Engineering Analysis

• Battery Capacity• Leakage• Heat Sinking• TEM efficiency

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Batteries

Li-Ion instead of Li-Poly

● Li-Ion are more readily available and cost less than Li-Poly.Li-Poly’s higher energy density does not outweigh its cost, and it’s shape characteristics are not an added benefit to the project.

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Batteries

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Battery Voltage: 12 V

Battery Capacity:(20 W*95% efficiency )/12V = 1.58A

1.58A*0.5 hr charge time = 754mAhr

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Rochester Institute of Technology

Leakage

• At 2 feet test depth:• P = ρgh• P = 999 kg/m^3 * 9.81m/s^2 * 0.61m• P = 6 kPa or 0.87 psi• Test Spec IP68 met by a number of cheap

enclosures by Integra Enclosures

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Thermal Circuit Analysis

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Thermoelectrics

● 20% heat loss● 95% efficient charging

system● Constant Thermoelectric

Properties● Heat Sink is flat, isothermal

vertical plate.

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Heat Sink

10/8/2013

Length (cm) Resistance (K/W)9.7 0.199

5.6 0.500

3.8 1.00

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Rochester Institute of Technology

Budget

• Thermoelectrics – $40/ea• Enclosure – $200• Electronics (Including cabling, microcontroller, and

battery) – $250• Testing – $100

Rough Total - ~$550 + 40n

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Thermoelectrics

• Power strongly dependent on Heat Sink.

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Dumbbell Enclosure

• If heat sink has 0.5K/W or greater resistance, the “cold” side will be very hot

• We need to protect our electronics from damage

• Dumbbell shape best mitigates risk to electronics

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Risk Assessment

10/8/2013

Category Risk Item Effect Cause Likelihood Severity Importance Action to Minimize Risk

OverheatLocal system overheat of Thermoelectric device

Component degradation or loss. Replacing component delays testing.

Poor heat sinking, rapid removal from water

1 2 2

Heat sinking testing without component, follow test protocol for removing device from water

EnclosurePressure vessel breach due to failure of seals

Equipment degradation, possible partial or complete system loss. This is potentially a large time draw as multiple components would require replacing before resuming testing.

Deflection due to thermal or mechanical stress, improper assembly

2 3 6

Heat sinking and pressure testing without electronics, follow testing procedure for assembly

ElectricalElectrical failure of PCB / microcontroller

Possible component failure. Possible long lead time item requires replacing, delaying testing.

Short circuit 1 3 3Thorough subsystem testing and CAD simulation

ProjectLack of guidance / late guidance from Boeing

Design criteria left open-ended, design without Boeing input, last minute changes put project behind schedule

Boeing contact is busy, does not respond in a timely manner

3 1 3

Provide ultimatum proposal to Boeing, rely on benchmarking competitors where detailed technical information is needed.

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Test Plan

Test waterproofing without heat

Test thermoelectric, sensors, charging and max power point circuits

Test waterproofing with heat

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Test Plan◼ Test heat sink

◼ Integrate and test full system.

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1: Heat Sink2: Thermoelectric Array3: Heat Source4: Instrumentation5: Microcontroller & Charging circuit6: Battery

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Project Plan◼ We only have 2 weeks◼ This is how we do it

▪ 5 days --- integrate --- 5 days◼ Update EDGE & Risk Assesment

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Issues on the Horizon

● Thermoelectric clamping (300kPa min - recommend 1.2MPa)

● External vs system powered electronics (sensors, microcontrollers, etc)

● Heat sinking

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Clamping Configurations

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Questions

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Problem Statement◼ Current State

▪ Boeing’s current UUV, the Echo Ranger has a maximum mission time of 28 hours. Boeing would like to significantly extend this mission time.

◼ Desired State▪ Boeing would like to utilize a thermoelectric system to significantly extend

mission time of their UUVs.◼ Project Goals

▪ Demonstrate proof of concept of thermoelectric system▪ Use a temperature differential to charge a battery▪ Achieve maximum thermoelectric efficiency over a range of temperatures▪ Establish a UUV-based research partnership between Boeing and RIT

◼ Constraints▪ System must operate underwater▪ System must utilize a thermoelectric device▪ System must operate autonomously

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Customer Requirements

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Engineering Requirements

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