Grainger CEME/IEEE Workshop on Technology Roadmap for Large...
Transcript of Grainger CEME/IEEE Workshop on Technology Roadmap for Large...
April 5-6, 2016Urbana, IL
James D. Heidmann, PhDActing Manager, Advanced Air Transport Technology (AATT) Project
NASA Glenn Research Center
Government Panel on Extreme Electrical Machines and Drives -
A NASA Aeronautics View
Grainger CEME/IEEE Workshop on Technology Roadmap for Large Electrical Machines
NASA Aeronautics Research Six Strategic Thrusts
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Safe, Efficient Growth in Global Operations• Enable full NextGen and develop technologies to substantially
reduce aircraft safety risks
Innovation in Commercial Supersonic Aircraft• Achieve a low-boom standard
Ultra-Efficient Commercial Vehicles• Pioneer technologies for big leaps in efficiency and
environmental performance
Transition to Low-Carbon Propulsion• Characterize drop-in alternative fuels and pioneer
low-carbon propulsion technology
Real-Time System-Wide Safety Assurance• Develop an integrated prototype of a real-time safety
monitoring and assurance system
Assured Autonomy for Aviation Transformation• Develop high impact aviation autonomy applications
3Aeronautics Research Mission Directorate
Aeronautics Research Mission Directorate
Advanced Air Transport Technology
(AATT)
Advanced Air Vehicles (AAVP)
Jay Dryer
Airspace OperationsAnd Safety (AOSP)John Cavolowsky
Integrated Aviation Systems (IASP)Ed Waggoner
Transformative AeronauticsConcepts (TACP)
Doug Rohn
Revolutionary VerticalLift Technology
(RVLT)
Commercial SupersonicTechnology
(CST)
Advanced Composites(ACP)
Aeronautics Evaluationand Test Capabilities
(AETC)
Airspace TechnologyDemonstrations
(ATD)
SMART NAS – Testbedfor Safe Trajectory
Operations
Safe AutonomousSystem Operations
(SASO)
EnvironmentallyResponsible
Aviation(ERA)
UAS Integrationin the NAS
Flight Demonstrationand Capabilities
(FDC)
Leading EdgeAeronautics Research
for NASA(LEARN)
Transformational Toolsand Technologies
(TTT)
Convergent AeronauticsSolutions
(CAS)
-------------------------- Mission Programs ----------------------------- Seedling Program
Coming SoonElectric content
CurrentElectric content
NASA Aeronautics Program Structure
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Major Aviation Community “Driver”Reduce Carbon Footprint by 50% by 2050…
…in the face of increasing demand, and while reducing development, manufacturing and operational costs of aircraft & meeting noise and LTO NOx regulations
Near to mid opportunity
“Industry pull”
Mid to far opportunity
“NASA push”
Credit - IATA
Thrust 1
Thrust 3
Thrust 3
Thrust 1,Thrust 3 &Thrust 4
5Analysis based on FAA US operations data provided by Holger Pfaender of Georgia Tech
Fuel Use by Vehicle Class
40% of fuel use is in 150-210 pax large single aisle class87% of fuel use is in small single-aisle and larger classes ( >100 pax)
13% of fuel use is in regional jet and turboprop classes
Focus on small single-aisle and larger vehicle classes for
maximum community impact
Ultimate Focus on Large Aircraft
6Aeronautics Research Mission Directorate
Hybrid Electric AircraftInteragency and Industry Contributions
ElectricalEnergy
Production
ElectricDistribution
EnergyStorage
IntegratedDesigns
SystemTesting&Evaluation
EndUser/Buyer
Certification
DoD ü ü ü
DOE ü ü ü
FAA ü
NASA ü ü
EngineCompanies ü ü
Airframers ü ü
Operators ü
EnergyandTransportIndustry
ü ü ü
Version: 19jan2016
7Aeronautics Research Mission Directorate
Leverage Opportunities
• Leverage early adopter market opportunities to establish new certification criteria and accelerate industry technology investments.
• Leverage efforts in the Energy and Transportation sectors to improve battery and fuel cell energy density. Higher energy density in these devices may enable all electric architectures and enhance hybrid electric architectures.
• Leveraging advances in small core turbine engine technologies being developed by industry would enhance hybrid electric architectures
• Leveraging DoD’s and DARPA’s investment and knowledge in HEP for civilian and military dual use applications will allow NASA to explore a wider range of configurations.
• Leverage lessons learned from electric/hybrid aircraft propulsion efforts by Google, Facebook, and Boeing to learn how to design, build, integrate and operate vehicles
8Aeronautics Research Mission Directorate
HEPTechnologyForecast(TRL6)
Exploration of Alternative Propulsion Systems
Introduction of Alternative Propulsion Systems to
Aircraft of All Sizes
Initial Introduction of Alternative Propulsion Systems
2015
2025
2035
Mature foundation technologies, architect HEP aircraft and Vert Lift vehicles, demonstrate
subsystems and integrated prototypes
Support industry in the development of HEP aircraft and Vert Lift Vehicles
Fly technology demonstrators, prototype subsystems and advanced componentsNASA
Outputs
CommunityOutcomes
CryogenicSC Elec Machines
Proof ofConcept
20hp/lb
25hp/lb
30hp/lb
Non-SCElec Machines
8hp/lb
10hp/lb
12hp/lb
>12hp/lb
Energy Storage 400wh/kg
500wh/kg
600wh/kg
700wh/kg
Fuel CellEnergy Conversion
2kW/kg
4kW/kg
5kW/kg
Power Electronics 2XSOA
5XSOA
10X SOA
Light WeightThermal Mgmt
2X Wt. Reduc
5X Wt. Reduc
10X Wt. Reduc
Leverage
Leverage
Technology Forecast
Version: 19jan2016
9Aeronautics Research Mission Directorate
Timeline of Machine Power With Application to Aircraft Class
SuperconductingNon-cryogenic 100 kW 1 MW 3 MW 10 MW 30 MW
PS–01758–1115
19 Seat2 MW Total Propulsive Power
300 Seat60 MW Total Propulsive Power
9 Seat 0.5 MW Total Propulsive Power
50-250 kW Electric Machines
.1-1 MW Electric Machines
50 Seat Turboprop 3 MW Total Propulsive Power
.3-6 MW Electric Machines
150 Seat22 MW Total Propulsive Power
1-11 MW Electric Machines
3 -30 MW Electric Machines
Largest Electrical Machine on Aircraft
50 Seat Jet12 MW Total Propulsive Power.3-6 MW Electric Machines
Version: 19jan2016
10Aeronautics Research Mission Directorate
Prove Out Transformational PotentialHybrid Electric Propulsion
Increasingly electric aircraft propulsion with minimal change to aircraft outer mold lines
Explore and demonstrate vehicle integration synergies enabled by hybrid electric propulsion
Gain experience through integration and demonstration on
progressively larger platforms
Single Aisle Transport
ModelingExplore Architectures
Test BedsComponent Improvements
Env
iron
men
tal
Ben
efit
+
2040
2030
2020Small Aircraft
Knowledge through Integration & Demonstration +
Image Credit: Joby
Image Credit: Yamaha
11Aeronautics Research Mission Directorate
NASA Aeronautics Ready for Flight
2008-2013 2014/15 2016/17 2018-2026
Accomplishments and Planning
Ready for X-Plane Integration & Demonstration
N+3 Subsonic & Supersonic Concept/Technology Studies
Ground Testing of N+3 configurations and technologies
LBFD PDRCompleted
8 Integrated Tech Demos Completed, Tech transitioned to industry. HWB ready for Flight Dem/Val.
Ready for NextGen TBO Integration & Demonstration
NASA FAA NextGen Research Transition Teams (RTTs) Initiated
Technology Transitions to FAA: MSP, EDA, PDRC, TSAS
ATD-1 Completed and transferred to
FAA
ATD-2, 3 Completed & Transferred to FAA
NASA Aero Vision and Strategy Established
Roadmaps Completed
N+2 Environmentally Responsible Aviation (ERA) Project Initiated
www.nasa.gov
UEST PDRCompleted
12Aeronautics Research Mission Directorate
New Aviation Horizons Flight Demo Plan
Design & Build Flight Test
Design & Build Flight Test
Design & Build Flight Test
Design & Build
FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24 FY25 FY26
PreliminaryDesign
“Purpose-Built” UEST Demonstrators
Hybrid Electric Propulsion Demonstrators
Fully integrated UEST Demonstrator
Design & Build Flight Test
PreliminaryDesign
PreliminaryDesign
Design & Build Flight Test Design & Build
Flight Test
Ground TestRisk Reduction
Ground TestRisk Reduction
PotentialCandidates
Ground Test Risk ReductionFlight TestSmall Scale “Build, Fly, Learn”
Transport Scale PreliminaryDesign
Total Demonstration Cost ROM: $700M
Life Cycle Cost Est: $430M
Life Cycle Early Cost Est: $850M
Life Cycle Cost ROM: $400-500M
Life Cycle Cost ROM: $400-500M
www.nasa.gov
Images Credit: Lockheed Martin
DP
DP
DP
DP
DP
Validated ability for U.S. Industry to Build Transformative Aircraft that use 50% less energy and produce less than half of the perceived noise
Validated HEP Concepts, Technologies And Integration for U.S. Industry to Lead the Clean Propulsion Revolution
Enables Low Boom Regulatory Standard and validated ability for industry to produce and operate commercial low noise supersonic aircraft
Key opportunity for “more electric” aircraft investment
13Advanced Air Transport Technology ProjectAdvanced Air Vehicles Program
NASA Aeronautics President’s FY17 Budget Request
$Millions FY2015EnactedFY2016 FY2017 FY2018 FY2019 FY2020 FY2021 FY2022 FY2023 FY2024 FY2025 FY2026
Aeronautics $642.0 $640.0 $790.4 $846.4 $1,060.1 $1,173.3 $1,286.9 $1,294.2 $1,307.6 $1,218.1 $829.7 $839.5
AirspaceOperationsandSafety 154.0 159.4 159.2 176.2 189.1 221.5 198.7 200.9 193.2 175.5 167.8
AdvancedAirVehicles 240.6 298.6 277.4 308.8 311.6 312.6 321.3 315.0 318.9 317.7 326.7
IntegratedAviationSystems 150.0 210.0 255.4 381.4 493.0 556.7 591.5 612.2 525.0 203.8 210.6
TransformativeAeronautics Concepts 97.4 122.3 154.4 193.8 179.7 196.2 182.8 179.4 181.0 132.7 134.4
Aeronautics budget includes paid-for 10-year mandatory funding from the Administration’s 21st Century Clean Transportation Plan.
MandatoryBudgetAuthority$Millions FY2017 FY2018 FY2019 FY2020 FY2021 Outyears21st Century Clean Transportation Plan 100 200 400 500 600 1900
AirspaceOperationsandSafety 18 20 35 45 75 170AdvancedAirVehicles 30 41 79 80 65 305IntegratedAviationSystems 37 84 196 300 370 1170TransformativeAeronauticsConcepts 15 55 90 75 90 255
Low Boom Flight Demonstrator 56IntegratedAviationSystems 56
www.nasa.gov