continuous lower federal aviation energy, emissions, and
TRANSCRIPT
Federal AviationAdministration
Continuous Lower
Energy, Emissions,
and Noise (CLEEN)
CLEEN Update and
CLEEN II Status
Presented to: ASCENT Advisory Committee Meeting
By: Jim Hileman, Ph.D.
Chief Scientific and Technical Advisor for
Environment and Energy
Federal Aviation Administration
Date: October 14, 2015
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AEE Research OverviewCharacterize the Problem and Assess Risk:
• Improve our scientific understanding of E&E constraints
• Incorporate this scientific knowledge into an integrated tool suite that can characterize the system, assess the risk and inform development of potential mitigation options
Develop mitigation solutions:
• Airframe and engine technologies
• Sustainable alternative jet fuels
• Clean, quiet and energy efficient operational procedures
• Environmental standards and policy measures
Manage system performance:
• Integrated analysis that engages a wide range of stakeholders to understand the current and future state of the aviation system
• Utilize knowledge to provide guidance on system-wide environmental improvements
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Boeing
• Ceramic Matrix
Composite Nozzle
• Adaptive Trailing Edge
• 5 year effort to accelerate technology commercialization
• Reduce aircraft fuel burn, emissions and noise
• Alternative jet fuel testing
• 50% cost share; total FAA budget: ~$125M
Continuous Lower Energy, Emissions and Noise (CLEEN)
General Electric
• Flight Management
System / Air Traffic
Integration
• Flight Management
System / Engine
Integration
• Twin Annual Pre-Swirled
(TAPS) II Low NOx
Combustor
• Open Rotor Engine
Pratt & Whitney
• Ultra-high Bypass
Ratio Geared Turbofan
Rolls-Royce
• Ceramic Matrix Composite
Blade Tracks
• Dual-Walled Turbine Airfoils
Honeywell
• Lighter weight, higher
temp engine
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CLEEN Program Goals
CORNERS OF THE
TRADE SPACE
CLEEN (N+1)
(EIS 2015-18)
N+2
(2020)*
N+3
(2025)*
Noise
(cum below Stage 4)-32 dB -42 dB -71 dB
LTO NOx Emissions
(Below CAEP 6) -60% -75% better than -75%
Aircraft Fuel Burn -33% -50% better than -70%
Ref: B737/CFM56-7B
Develop and demonstrate (TRL 6-7) certifiable aircraft technology
* Technology Readiness Level for key technologies = 4-6
Ref: B777-200/GE-90
Advance use of “drop-in” renewable alternative fuels
Bio feedstock Processing
Jet fuel
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Efforts that support Technology Maturation
Continuous Lower Energy, Emissions and Noise (CLEEN)
• Reduce aircraft fuel burn, emissions and noise through
technology & advance alternative jet fuels
• Public private partnership with 1:1 minimum cost share
requirement – Federal funding at $125M
• Enable industry to expedite introduction of novel
technologies into current and future aircraft and engines
• Maturation from TRL 3-5 concluding in major demonstrations
at TRL 6 or 7 (ground engine or flight test)
Aviation Sustainability Center (ASCENT)
• Center of Excellence for Alternative Jet Fuels & Environment
• Providing independent assessment of environmental benefits
from CLEEN technology introduction
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Boeing CLEEN Technologies
Adaptive Trailing Edge
Up to 2% fuel burn reduction, -1.5dB
cumulative EPNdB noise reduction.
Ceramic Matrix Composite Acoustic Nozzle
Up to 1% fuel burn reduction
Noise attenuation on parity or better than
metallic nozzle.
Photo: Bob Ferguson
Images courtesy of Boeing
2010 2011 2012 2013 2014 2015
Ceramic Matrix
Composite Nozzle
Ground Test (TRL 6)
Adaptive Trailing Edge Flight
Demonstration (TRL 7)
Ceramic Matrix
Composite Nozzle
Flight Test (TRL 7)
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GE CLEEN Technologies (1 of 2)
TAPS II Low NOx CombustorDemonstrated in rig and core engine test > 60% NOx margin to
CAEP/6, exceeding CLEEN goal. – 2016 EIS with ~8000 orders
Open Rotor Fan Blade Development~26% reduction in fuel burn (re: 737-800) and ~15-17EPNdB
cumulative noise margin to Stg. 4
Images courtesy of GE Aviation
2010 2011 2012 2013 2014 2015
Core Test of TAPS II
Combustor (TRL 6)
Open Rotor Wind
Tunnel Tests (TRL 5)
TAPS II 2016 EIS with
~8000 orders
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GE CLEEN Technologies (2 of 2)
FMS/ATM IntegrationBenefits assessment ongoing.
FMS/Engine Control Integration• Adaptive engine control
• Vehicle health management
• Flight-propulsion control
Benefits assessment ongoing.
Ongoing Activities: • Engine and flight testing
Images courtesy of GE Aviation and Aviation Systems
2010 2011 2012 2013 2014 2015
FMS/Engine
Technology Logic
Design CompleteFMS/Engine Effort
Complete Q1 2016
Completed Dynamic
Quiet Climb and
Wind Input
Optimization Tasks
Completed Trajectory
Synchronization
Simulation (TRL 6)
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Honeywell CLEEN Technologies
High
Temperature
Impeller
• Low leakage air-air seals
• Advanced materials
Engine Core Fuel Burn Reduction
Technologies
5% fuel burn reduction as part
of a 15.7% fuel burn reduction
engine package.
Alternative Jet Fuels
• Completed study on impact of
aromatics on materials
• Completed biofuel life cycle
analyses with MIT
Images courtesy of Honeywell
2010 2011 2012 2013 2014 2015
Core Engine Testing
of High T3 Impeller
Final CLEEN Engine
Test (TRL 6) for All
TechnologiesEarly Engine Test
Opportunities (Some
Technologies to TRL 6)
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Pratt & Whitney CLEEN Technologies
Ground Test
Wind Tunnel Tests
Ultra High Bypass Geared Turbofan with
Advanced Fan System
Technologies expand design space
for engine with ~ 20% fuel burn
reduction, 25 EPNdB cumulative
noise margin to Stage 4
Alternative Jet Fuels
• Engine and combustor testing of
alternative jet fuels from multiple
production pathways
Images courtesy of Pratt & Whitney
2010 2011 2012 2013 2014 2015
Ultra High Bypass
Rig Test with
Advanced Fan Exit
Guide Vanes
Integrated Ultra High
Bypass Rig DemoCLEEN Engine
Design Complete
CLEEN Engine
Test Q1 2016
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Rolls-Royce CLEEN Technologies
Dual Wall Turbine Airfoils + CMC Blade Tracks
CMC blade tracks offer > 50% reduction in
cooling and component weight.
Dual Wall turbine airfoils provide > 20%
reduction in cooling and increased operating
temperature capability.
CLEEN technologies provide ~1% fuel burn
reduction
Novel Alternative Fuels Project• Lab, rig, and APU testing complete
Images courtesy of Rolls-Royce
2010 2011 2012 2013 2014 2015
Dual Wall Vane Rig
TestingCMC Blade Tracks
Engine Test 1
Dual Wall Vane
Engine Test Mid-
2016
CMC Blade Tracks
Engine Test 2 (TRL 6)
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Benefits of CLEEN Program:
Demonstrated technologies that reduce noise, emissions and fuel burn
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General Electric
TAPS II Combustor (entering fleet in 2016)
CLEEN 60% margin to CAEP/6 LTO NOx was achieved
FMS/Engine and FMS/ATM Integration
Up to 2% fuel burn reduction from FMS/engine
0.7% fuel burn reduction from trajectory synchronization
Additional benefits being assessed
Open Rotor
~26% reduction in fuel burn (re: 737-800) and
~15-17EPNdB cumulative noise margin to Stage 4
Rolls Royce
Ceramic Matrix Composite Turbine Blade Track
> 50% reduction in cooling and component weight.
Rolls-Royce – Dual Wall Turbine Airfoil
> 20% reduction in cooling and increased operating
temperature capability.
CLEEN tech will provide ~1% fuel burn reduction
Boeing
Adaptive Trailing Edge
~ 2% fuel burn reduction
~ -1.5dB cum in some single and twin aisles
CMC Acoustic Nozzle
~ 1% fuel burn reduction
Parity or better noise reduction compared with
treated metallic hot structure
Honeywell
Fuel Burn Technologies
CLEEN technologies contributed to ~5% fuel
burn reduction as part of a 15.7% fuel burn
reduction engine package
Pratt & Whitney
Geared Turbofan Technologies
CLEEN techs expand design space for engine
with ~ 20% fuel burn reduction, 25 EPNdB
cumulative noise margin to Stage 4 12
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CLEEN II Program Details:• Reducing environmental impacts via aircraft technology and alternative jet fuels
• Five year effort to accelerate technology maturation (2015-2020)
• 50% cost share; total FAA budget: ~$100M
Aircraft Technology Maturation
Continuous Lower Energy, Emissions & Noise II (CLEEN II)
CLEEN II Program Goals:• 32 dB1 cumulative noise reduction
• 70%2 landing/take-off NOx emissions reduction
• 40%1 fuel burn reduction
Conducting ground and/or flight test
demonstrations of certifiable aircraft
technologies with entry into service by
2026
Based on 5-year cost share
agreements with industry Benefits in all goal areas: noise, NOX, & fuel burn
Many planned technologies targeting multiple
areas simultaneously.
1 Common baseline with CLEEN I goals2 70% reduction in landing and take-off NOx relative to the CAEP/8 standard (75% reduction relative to CLEEN I CAEP/6 baseline).
Awardees:• Aurora Flight Sciences
• Boeing
• Delta Tech Ops, America’s Phenix, MDS Coating
Technologies
• General Electric (GE) Aviation§
• Honeywell Aerospace
• Pratt & Whitney
• Rolls-Royce
• Rohr, Inc. / UTC Aerospace Systems
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CLEEN II Program Technologies
Company Technology
Aurora Flight Services D8 Double-Bubble Fuselage
Boeing Structurally Efficient Wing
Delta Tech Ops, America’s
Phenix, MDS Coating
Technologies
Protective Coating on Leading Edge of Gas Turbine Engine Fan Blades
General Electric (GE) Aviation* TAPS III Combustor, More Electric Systems and Technologies for
Aircraft in the Next Generation (MESTANG), Flight Management
System / Engine Integration Technologies, Alternative Jet Fuel Test and
Evaluation
Honeywell Aerospace Compact, Low Emissions Radial In-Flow Combustor (SABER) and
Advanced Turbine Blade Outer Air Seal System
Pratt & Whitney* Compressed Aero-Efficiency Technologies and Turbine Thermal and
Aero-Efficiency Technologies
Rolls-Royce* CSD Low NOx Combustor and Alternative Jet Fuel Test and Evaluation
Rohr, Inc. /
UTC Aerospace Systems
Integrated Thrust Reverser
* Contract terms and conditions are being finalized
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In Summary
• CLEEN* has successfully
accelerated aircraft technology
development to reduce noise,
emissions and fuel burn
• CLEEN has helped and is helping
to accelerate alternative jet fuel
development
• FAA have initiated CLEEN II
* For more information on the CLEEN Program, its benefits, and
accomplishments to date, please see the CLEEN Program Fact Sheet at
http://www.faa.gov/news/fact_sheets/news_story.cfm?newsId=16814