Innovation Takes Off - Clean · PDF fileo Advanced load control architectures and function ......
Transcript of Innovation Takes Off - Clean · PDF fileo Advanced load control architectures and function ......
Innovation Takes Off
Clean Sky 2 Information Day Large Passenger Aircraft – IADP
presented by
Michel Goulain Airbus
and François Mirville
Snecma
Toulouse, 4 September 2014
From Clean Sky towards Clean Sky 2
CS1 Smart Fixed Wing Aircraft -ITD (SFWA)
Is a unique environment for high TRL integrated Research and Development
Provides the frame for well aligned objective driven R&T covering
development and maturation through numerical simulation,
rig demonstrators, wind tunnel testing, large scale and
flight testing under conditions relevant for operation
TRL6
TRL5
TRL4
CS2 Large Passenger Aircraft IADP (LPA)
Will provide a platform for even more focussed large scale, highly
integrated demonstrators with core partners and partners
Build on down best candidate technologies emerging from
CleanSky 1 other national and EU R&T programs and
additional technologies developed in CS2 ITDs
SFWA key technologies
o NLF – wing for large transport aircraft and
bizjets
o CROR engine integration
o Innovative empennage for next generation
bizjets
o Innovative control surfaces
o Buffet Control Technologies
o Advanced load control architectures and
function
o Advanced Flight Test instrumentation
2 3 4 5 6
Contribute to TRL - Scale
1
TRL3
CS2 LPA-IADP Info day
Setup and Implementation
rr
Platform 1 Advanced Engine and
Aircraft Configuration
Platform 2 Innovative Physical
Integration Cabin-System-
Structure
Platform 3 Next Gen. A/C Systems,
Cockpit Systems &
Avionics
„Mature and validate disruptive
technologies for next generation
Large Passenger Aircraft through
large scale integrated
demonstration“
CS2 LPA-IADP Info day, 4th September 2014
LPA-IADP Work Breakdown Structure
CS2 LPA-IADP Info day, 4th September 2014
WP 0
LPA – IADP
WP 0.1
Technology assessment
WP 0.2
EcoDesign
WP 0.3
ITD - Interfaces
Platform 1 – WP 0
Advanced Engine & Aircraft Configuration
WP 1.1
CROR Demo engine FTD
WP 1.2
Advanced engine integration driven fuselage
WP 1.3
Validation of scaled flight testing
WP 1.4
Hybrid Laminar Flow Control large scale demonstration
WP 1.5
Innovative Flight Operations
WP 1.6
Demonstration of radical aircraft configurations
Platform 2 – WP 0
Innovative Physical Integration Cabin-System-Structure
WP 2.1
Integrated product architecture
WP 2.2
Non-specific design technologies
WP 2.3
Technology validation
Platform 3 – WP 0
Next generation Aircraft, Cockpits Systems & Avionics
WP 3.1
Enhanced flight operations & functions
WP 3.2 Avionic backbone technologies
development, integration & demonstration
WP 3.3
Next generation cockpit functions flight demonstration
WP 3.4
Next generation cockpit ground demonstrator
WP 3.5
Pilot Case Demonstrator
WP 3.6
Maintenance
LPA-IADP WBS – “Platform 1”
Estimated Volume of Activities ~560M€
Next Gen. A/C Systems, Cockpit Systems & Avionics
Advanced Engine and Aircraft Configurations
Innovative Physical Integration Cabin-System-Structure
Large Passenger Aircraft Platform – integration topics
TRL 4-6 Aircraft Level
Airbus with SAAB, Dassault,
SNECMA and Partners
Platform 1 Advanced Engine and Aircraft Configurations
WP 1.1 CROR demo engine FTD
WP 1.2 Advanced engine integration driven rear fuselage
WP 1.3 Validation of scaled flight testing
WP 1.4 Hybrid laminar flow control large scale demonstration • HLFC applied on fin in long-term flight operation
• HLFC wing pre-flight demonstrator
WP 1.5 Innovative Flight operations
WP 1.6 Demonstration of radical aircraft configurations
CS2 LPA-IADP Info day, 4th September 2014
Under Revision
WP1.1 CROR Engine Demonstrator FTD
Top objectives
• Validate the aerodynamic efficiency and noise level for a full size airworthy CROR pusher engine under operational conditions (TRL 6)
• Demonstrate and validate the viability of the chosen propulsion system concept and associated technologies like power gearbox, pitch control, lubrication system, propeller and blade design
• Demonstrate and validate a pylon concept and system integration, addressing loads, vibration, and noise attenuation technologies in real size
• Synthesize available data from Clean Sky with CROR demo-engine flight test data, re-calibrate tools
Timescale: Q3 2014 – Q2 2023
Gross budget: 185M€, including 120M€ for WP1.1.3
SNECMA is leading WP 1.1.3. CROR Demo Engine
WP1.2 Advanced Engine Driven Fuselage
Top objectives
• Design and manufacture of a real size CFRP rear-end (rear mounted engine).
• Validate the overall structure and system integration concept including rear-end fuselage, tail cone, pylon & engine mounts, T-tail and APU, with respect to industrialisation.
• Demonstrate the loads capability of the structural solution and the design characteristic with respect to noise.
• Demonstrate an engine integration solution fully compliant with certification rules, focusing on stability of the structure against uncontained engine debris release or ice shedding and relevant engine failure cases.
• Development of required test capabilities both physical at full scale and virtual.
Gross budget: 77 M€
Timescale: Q3 2014 – Q2 2024
WP1.3 Validation of Scaled Flight Testing
Top objectives
• Assessment of the perimeter and boundaries of scaled flight testing with respect to aerodynamic similarity and performance, structural- and flight dynamics.
• Design of the test environment and the associated development of the required procedures and supporting testing environment .
• Further development and validation of existing test vehicle as baseline configuration.
• Demonstration of new airframe components and technologies with an in-flight context.
Gross budget: 10,8M€
Timescale: Q3 2014 – Q3 2017
WP1.4 HLFC Large Scale Demonstration
Top objectives
• Development and manufacturing of an improved HLFC fin-demonstrator for long-term in-service operational use.
• Definition of certification processes and rules for HLFC based aircraft components together with authorities and operators / airlines.
• HLFC-fin long-term in-service demonstration (~1 year) with a commercial operator.
• Transfer of learning from AFloNext HLFC wing leading edge structure demonstrator.
• Design, build and test of a large-scale pre-flight wing ground demonstrator to bring the HLFC technology applied on wing to TRL5.
Timescale: Applied on fin Q1 2015 – Q2 2019 Applied on wing Q1 2017 – Q2 2023
Gross budget: 137 M€
WP1.5 Innovative Flight Operations
Top objectives
• Flight tests of aircrafts in formation.
• Flight tests to demonstrate integrated advanced flow control means in the wing/pylon junction.
• New take-off and approach procedures and trajectories to lower environmental and community impact designed to make integrated use of already highly matured technologies.
• Flight tests to address specific, to be determined operational issues of the Natural Laminar Flow (NLF) technology applied on airframe at selected operational conditions.
• Scoping the use of test aircraft to perform as a “modular, common platform”.
Timescale: • Formation flight Q3 2014 – Q3 2023 • Advanced technologies demonstration Q2 2017 – Q4 2024 • New environmental flight procedures Q1 2017 – Q2 2024
WP 1.5.1
Demonstration of linked aircraft to aircraft flight,
formation flight
WP 1.5
Innovative Flight Operations
Platform 1 - WP0
Advanced Engine and Aircraft Configuration
WP 1.5.2
Demonstration of advanced green flight
procedures & technologies
WP 1.5.3
Demonstration of separation flow control
technologies
WP 1.5.4
Validation of advanced technologies at in service
operation
Gross budget: 37M€
WP1.6 Demonstration of Radical Aircraft Configurations
Top objectives
• Development of advanced aircraft concepts (airframe, systems architecture, propulsion concept) with an integrated design approach.
• In particular development of hybrid propulsion concepts.
• Testing of developed technologies and airframe components by means of adaptable and rapid test means such as scaled flight testing.
Gross budget: 98M€
Timescale: Q4 2018 – Q3 2024
Advanced Engine and Aircraft Configurations
High-Level Technology Roadmap
2 3 4 5 6
Contribute to TRL - Scale
1
LPA-IADP high level provisional schedule
2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024
Platform 1
CROR demo engine FTD
Adv. engine integrated fuselage ground demo
Dynamically Scaled integrated flight testing
HLFC large scale spec in flight operation
HLFC -wing flight test demonstration
Demo of adv. SMR aircraft configuration
Platform 2
Innov. physical integr. Cabin-System-Structure
Platform 3
Next Gen. A/C Syst., Cockpit Syst. & Avionics
tbd
6 6 5 4
Platform 1
o WP1.1 CROR demo engine FTD
o WP1.2 Advanced engine integration driven
fuselage
o WP1.3 Validation of scaled flight testing
o WP1.4 HLFC large scale demonstration
o applied on VTP
o applied on Wing
o WP1.5 Innovative flight operations &
robustness demonstration
o Formation flight
o Flight procedures
o WP1.6 Demonstration of radical aircraft
configurations
4
4
5 4
6 4 5
5
6
4 5 6
*
**
3
6
* Non-specific TRL ** Specific TRL
4
5 6
4 4
5 5
5
6
CS2 LPA-IADP Info day, 4th September 2014
LPA-IADP WBS – “Platform 2”
CS2 LPA-IADP Info day, 4th September 2014
WP 0
LPA – IADP
WP 0.1
Technology assessement
WP 0.2
EcoDesign
WP 0.3
ITD - Interfaces
Platform 1 – WP 0
Advanced Engine & Aircraft Configuration
WP 1.1
CROR Demo engine FTD
WP 1.2
Advanced engine integration driven fuselage
WP 1.3
Validation of scaled flight testing
WP 1.4
Hybrid Laminar Flow Control large scale demonstration
WP 1.5
Innovative Flight Operations
WP 1.6
Demonstration of radical aircraft configurations
Platform 2 – WP 0
Innovative Physical Integration Cabin-System-Structure
WP 2.1
Integrated product architecture
WP 2.2
Non-specific design technologies
WP 2.3
Technology validation
Platform 3 – WP 0
Next generation Aircraft, Cockpits Systems & Avionics
WP 3.1
Enhanced flight operations & functions
WP 3.2 Avionic backbone technologies
development, integration & demonstration
WP 3.3
Next generation cockpit functions flight demonstration
WP 3.4
Next generation cockpit ground demonstrator
WP 3.5
Pilot Case Demonstrator
WP 3.6
Maintenance
LPA-IADP WBS – “Platform 2”
Next Gen. A/C Systems, Cockpit Systems & Avionics
Advanced Engine and Aircraft Configurations
Innovative Physical Integration Cabin-System-Structure
Large Passenger Aircraft Platform – integration topics
TRL 4-6 Aircraft Level
Airbus with, Liebherr,
Fraunhofer and Partners
Platform 2 Innovative Physical Integration Cabin-System-Structure
WP 2.1 Integrated product architecture
WP 2.2 Non specific design technologies
WP 2.3 Technology validation
WP 2.3.1 Multi purpose demonstrators
• Next generation fuselage, cabin & cargo functional demonstrator
• Next generation cabin & cargo functional demonstrator
• Next generation lower centre fuselage structural demonstrator
WP 2.3.2 Testing
WP 2.3.3 Pre-Production Line Technologies
CS2 LPA-IADP Info day, 20th February 2014 Estimated Volume of Activities ~290M€ CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure Overall Objectives
Objectives
•Demonstrate the benefits of disruptive fuselage architectures which integrate structure, system installation and cabin elements
Enablers
•Multidisciplinary integration methodologies and processes for integrated structural, system, and cabin elements
•Elements and architectures which integrate formerly separated functions from structures, system installation and cabin
•Testing technologies for integrated functional and mechanical demonstrator
Potential partners
•Aero structure manufacturers
•Cabin & Cargo manufacturers
Timescales
•TRL6 in 2023
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.1 Integrated Product Architecture & WP2.3 Technology validation
Objectives
• Reduction in total weight and industrialisation effort
• Reduction of part-count
• Simplified system routing and their attachments
• Increase of additional space
• Better understanding of size and shapes drivers
Enablers
• Study flexibility of Interfaces
• Load Carrying Elements (cabin, cargo and systems)
• Multifunctional solutions
Potential partners
• Aero structure manufacturers
• Cabin & Cargo manufacturers
Fnext Ftoday
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.1 Predictive Virtual Testing & WP2.3.2 Testing
Objectives
• Robust validation of new predictive virtual testing methodologies
• Develop, qualify and apply innovative test and measurement technologies for efficient, high quality testing of integrated demonstrators
Enabling
• Methods with true extrapolation capabilities
• Reduced lead time (and cost) for component validation, leading to earlier entry into service
• Reduced number of individual tests (leaner test pyramid)
• Higher maturity of product at EIS (right first time)
• Improved validation methodology to deliver greater optimisation and earlier/higher maturity leading to improved in-service reliability at EIS
Potential partners
• Universities
• Specialized research centres
• Solution developers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.2 Technologies for elementary parts, sub-components and modules
Objectives
• Validation of structural integration concepts
• Innovative manufacturing processes
Enabling
• Rivetless assembly
• Automation
• Quality assurance
• Net shape manufacturing
• Topology optimisation - Bionic design
Potential partners
• Specialized research centres
• Aerostructure manufacturers
• Cabin & Cargo manufacturers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.3 Technologies for Future of Aircraft Factory & Pre-production lines
Objectives
• Validate a true TRL6 maturity level in a close to real environment
Enabling
• Automation
• Smart production
• Virtual Manufacturing System
• High precision handling and logistic
• Structure mounted system
• Operator booster, Generic and universal robotic worker
• Standard robot and Collaborative robots (Cobot)
• Agile Speed shop
• Intelligent production
Potential partners
• Specialized research centres
• Industrial suppliers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.4 Interface Technologies
Objectives
• Simplify the integration of systems either by reducing part counts, reducing labour time or improving systems’ specific efficiency
Enabling
• Advanced data and power distribution
• Innovations in Systems Integration
• Wireless connectivity
• Contact less connectivity
• Easy electrical bounding connections
• Local power generation & supply
• Maintenance free energy sources
• Smart grid power distribution
Potential partners
• Specialized research centres
• System suppliers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.5 Customisation Technologies
Objectives
• Novel cabin and system architecture serving future airline and passenger’s needs, whilst enabling the aircraft manufacturer to benefit from reduced customization efforts
By means of
• Definition of a Cabin & Cargo Platform Concept that reduces the customization effort extensively. The platform concept ensures increased revenue by limiting non recurring and recurring costs whilst ensuring ramp-up and a reduction of development risks at similar customization level
Potential partners
• Specialized research centres
• Cabin and Cargo manufacturers
• System suppliers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.2.6 Airframe and Cabin & Cargo operation
Objectives
• Address the operation of an airframe with highly integrated structures, systems and cabin in order to deliver a viable product
Enabling
• Maintenance procedures
• Culture specific cabin architecture
• Virtual outside view and passenger guidance
• Crew workload
• Innovative operations
Potential partners
• Specialized research centres
• Cabin and Cargo manufacturers
• System suppliers
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.3 Technology validation: Multipurpose demonstrators & Testing
Objectives
• Integrate new technologies into the following large scale, ground based multipurpose demonstrators in order to validate a true TRL6 maturity level:
• Next generation fuselage, cabin and systems integrated demonstrator
• Next generation Cabin & Cargo functional demonstrator
• Next generation lower centre fuselage demonstrator
Enablers
• Integrated architectures and concepts
• Multifunctional technologies
• Effective multipurpose testing methods and tools
Potential partners
• Aero structure manufacturers
• Cabin & Cargo manufacturers
• Advanced testing facilities
CS2 LPA-IADP Info day, 4th September 2014
Innovative Physical Integration Cabin-System-Structure WP2.3 Technology validation: Pre-Production lines
Objectives
• Develop and demonstrate the critical differentiating process elements in both assembly and manufacturing
• Application of compliance with Eco Design principles, related use of materials, resources, deployment of processes
• Complete the industrial V&V
• Key supply chain elements validation
Enablers
• Combination of key physical and simulated assembly and manufacturing processes to manufacture and assemble the next generation aircraft integrated fuselage
Potential partners
• Aero structure manufacturers
• Cabin & Cargo manufacturers
• Industrial engineering
• Automation
• Logistics
CS2 LPA-IADP Info day, 4th September 2014
WP 0
LPA – IADP
WP 0.1
Technology assessement
WP 0.2
EcoDesign
WP 0.3
ITD - Interfaces
Platform 1 – WP 0
Advanced Engine & Aircraft Configuration
WP 1.1
CROR Demo engine FTD
WP 1.2
Advanced engine integration driven fuselage
WP 1.3
Validation of scaled flight testing
WP 1.4
Hybrid Laminar Flow Control large scale demonstration
WP 1.5
Innovative Flight Operations
WP 1.6
Demonstration of radical aircraft configurations
Platform 2 – WP 0
Innovative Physical Integration Cabin-System-Structure
WP 2.1
Integrated product architecture
WP 2.2
Non-specific design technologies
WP 2.3
Technology validation
Platform 3 – WP 0
Next generation Aircraft, Cockpits Systems & Avionics
WP 3.1
Enhanced flight operations & functions
WP 3.2 Avionic backbone technologies
development, integration & demonstration
WP 3.3
Next generation cockpit functions flight demonstration
WP 3.4
Next generation cockpit ground demonstrator
WP 3.5
Pilot Case Demonstrator
WP 3.6
Maintenance
LPA-IADP WBS – “Platform 3”
CS2 LPA-IADP Info day, 4th September 2014
Setup and Implementation LPA Platform 3
Estimated Volume of Activities ~222M€
Next Gen. A/C Systems, Cockpit & Avionics
Advanced Engine and Aircraft Configurations
Innovative Physical Integration Cabin-System-Structure
Large Passenger Aircraft Platform – integration topics TRL 4-6 Aircraft Level
Airbus with Thales, Liebherr,
SAFRAN and Partners
Platform 3 Next Gen. Aircraft A/C Systems, Cockpits & Avionics
WP 3.1 Enhanced flight operations and functions
WP 3.2 Avionic backbone technologies development, integration and demonstration
WP 3.3 Next generation cockpit functions flight demonstration
WP 3.4 Next generation cockpit ground demonstrator
WP 3.5 Pilot case” demonstrator
WP 3.6 Maintenance
Cockpit of the future (Fenics)
CS2 LPA-IADP Info day, 4th September 2014
CS2 LPA-IADP Info day, 4th September 2014
LPA Platform 3: Historical context and ambition
1970 1980 1990 2000 2010 2020 2030 2040
Innovation in
Operations
Crew standpoint
A300
A300FFCC
A310
A320
A330
A340
A350
NEXT NEXT+1
STEP CHANGE
STEP CHANGE
STEP CHANGE ?
EIS dates
SESAR deployment
A380
CS2 LPA-IADP Info day, 4th September 2014
LPA Platform 3: Historical context and ambition
1970 1980 1990 2000 2010 2020 2030 2040
Innovation in
Operations
Crew standpoint
A300
A300FFCC
A310
A320
A330
A340
A350
NEXT NEXT+1
STEP CHANGE
STEP CHANGE
STEP CHANGE ?
EIS dates
SESAR deployment
A380
CS2 LPA-IADP Info day, 4th September 2014
LPA Platform 3: Historical context and ambition
1970 1980 1990 2000 2010 2020 2030 2040
Innovation in
Operations
Crew standpoint
A300
A300FFCC
A310
A320
A330
A340
A350
NEXT NEXT+1
STEP CHANGE
STEP CHANGE
STEP CHANGE ?
EIS dates
SESAR deployment
A380
ENABLING DEMONSTRATOR
A300 MSN3 with side stick
ENABLING DEMONSTRATOR(S)
CS2 / IADP LPA WP3
CS2 LPA-IADP Info day, 4th September 2014
From technologies to operations and benefits
One « dummy » example (1/2)
Head Up Vision,
Immersive Vision,
Permanent Autopilot
State of the art Technology development (Various
frameworks, including CS2 ITD systems)
Commercial HUD
Military « helmets »
Google glasses
Airbus «standard »
Flight Control laws and
Autopilot modes
Standard procedure
+ ATM (SESAR) proposals
Integrated concept:
Operations + Functions +
Technical resources
Benefits
Safety improvement Easier handling Crew workload Crew training needs
Weather resilience Less operational
disruption Smoother traffic
management
Sustainable competitive advantage New Approach &
Landing guidance and control modes
(& procedures) Coherent onboard
avionics architecture
CS2 LPA-IADP Info day, 4th September 2014
From technologies to operations and benefits
One « dummy » example (2/2)
Head Up Vision,
Immersive Vision,
Permanent Autopilot
New Approach & Landing guidance
and control modes (& procedures)
State of the art Technology
development
Commercial HUD
Military « helmets »
Google glasses
Airbus «standard »
Flight Control laws and
Autopilot modes
Standard procedures
+ ATM (SESAR) proposals
Integrated concept:
Operations + Functions +
Technical resources
Demonstration
principles
Coherent onboard
avionics architecture
Highly representative
simulator
Demonstration of Full concept integration
Flight test
Demonstration of key features (functions +
equipment) in real environment
WP 3.1 Enhanced flight operations and functions
Objectives
• Definition and validation of novel functions to facilitate intuitive operation of LPA in the next generation cockpit
• These functions are based on concepts prepared in other EU funded programmes
Output for benefit evaluation
• Quantified operational benefit by function (fuel, time…)
Potential partners
• CP: Medium and large Nav-systems, equipment industry
• CfP: System suppliers (if not CP), means / part suppliers
Timescales
• From Q3-2015 up to Q4-2018
Gross budget provisions
• 45.8 M€
CS2 LPA-IADP Info day, 4th September 2014
WP 3.2 Avionic backbone technologies development, integration
and demonstration
Objectives • Definition and development of avionics components
(complementary to ITD system WP1 and WP2) to provide a flexible and compact avionics platform to implement and integrate the novel functions developed in WP3.1
• Adapt demonstration platform with the outcome of WP3.1 and WP3.2
• Define and develop additional avionics technologies for implementation of advanced functions
Output for benefit evaluation • Quantified benefit at aircraft level (weight, cost…)
• Feasibility + maturity assessment new standards
Potential partners • CP: Medium and large Nav-systems, equipment industry
• CfP: System suppliers (if not CP), means / part suppliers
Timescales
• From Q3-2015 up to Q4-2018
Gross budget provisions • 30.4 M€
CS2 LPA-IADP Info day, 4th September 2014
WP 3.3 Next generation cockpit functions flight demonstration
Objectives
• In-flight testing of specific functions defined in WP3.1 where flight environment is of paramount importance (e.g. approach and landing)
Output for benefit evaluation
• Critical phases evaluation in flight
Potential partners
• CP: Medium and large Nav-systems, equipment industry
• CfP: System suppliers (if not CP), means / part suppliers
Timescales
• From Q1-2018 up to Q4-2020
Gross budget provisions
• 37.6 M€
CS2 LPA-IADP Info day, 4th September 2014
WP 3.4 Next generation cockpit ground demonstrator
Objectives
• Build a highly representative ground demonstrator of the future LPA cockpit, embedding all the novel functions and avionics technology bricks
• Demonstrate enhanced flight operations in a realistic (simulated) environment
• Validate the concepts and novel type of operations
Output for benefit evaluation
• Overall functional integration
• Crew evaluation and buy-in
Potential partners
• CP: Medium and large Nav-systems, equipment industry
• CfP: System suppliers (if not CP), means / part suppliers
Timescales
• From Q1-2020 up to Q4-2023
Gross budget provisions
• 67.6 M€
CS2 LPA-IADP Info day, 4th September 2014
WP 3.5 “Pilot case” demonstrators
Objectives
• Specific testing of devices not implemented in WP3.3 and WP3.4
Output for benefit evaluation
• Case by case focus (performance demonstration)
Potential partners
• CP: Large system industry
• CfP: System suppliers (if not CP), means / part suppliers
Timescales
• From Q1-2020 (TBC) up to Q4-2023 (TBC)
• Planning definition will be done on a case-by-case basis
Gross budget provisions
• 10.6 M€
Example: AVOID (Airborne Volcanic Object Identifier
and Detector) Technology
CS2 LPA-IADP Info day, 4th September 2014
WP 3.6 Maintenance
Objectives
• Focus on legacy fleet to meet 4 years project timeframe
• Integration and use of technologies which will provide: • Reduction of operational disruption caused by unscheduled
maintenance on the legacy fleet
• Maximization of airline & maintenance asset utilization
• Improvement of the value chain through services.
• Exploration of the impact of new services on the way of working for maintenance actors
• Improvement of maintenance economics
Output for benefit evaluation
• Benefits in maintenance operation: reduction of cost, time, etc…
Potential partners
• CfPs: consortium (airlines + SMEs, RE’s), System suppliers
Timescales
• From Q3-2014 up to Q1-2019
Gross budget provisions
• 30 M€ CS2 LPA-IADP Info day, 4th September 2014
Core partner topics 1st wave
Identification Title Value (Funding in M€)
JTI-CS2-2014-CPW01-LPA
Advanced Engine and Aircraft Configurations - Strategic Complementary Research to Prepare, Develop and Conduct Large-Scale Demonstration
15
JTI-CS2-2014-CPW01-LPA-01-02
Integrated Flow Control Applied to large Civil Aircraft
4
JTI-CS2-2014-CPW01-LPA-01-03
Advanced HLFC fin design work: Structural design and manufacturing of operational HLFC fin
5
JTI-CS2-2014-CPW01-LPA-01-04
Integrated Engine Mounted Rear End Demonstrator: Component Design, Manufacturing and Test
7,5
JTI-CS2-2014-CPW01-LPA-01-05
Power Turbine of the Flight Demonstrator Contra Rotative Open Rotor (CROR) Engine
5
JTI-CS2-2014-CPW01-LPA-01-06
Rotating Frames of the Flight Demonstrator Contra Rotating Open Rotor (CROR) Engine
5
JTI-CS2-CPW01-LPA-02-01
Airframe Cabin and Cargo and System integration Architecture 5
JTI-CS2-CPW01-LPA-02-02
Cabin & Cargo Functional System and Operations
6,5
CS2 LPA-IADP Info day, 4th September 2014
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (1/8)
Title
Advanced Engine and Aircraft Configurations
Strategic Complementary Research to Prepare, Develop and Conduct Large-Scale Demonstration
Topic Number JTI-CS2-2014-CPW01-LPA-01-01
Indicative Topic Funding Value 15 M€
Duration 9 years
Start Date 1st April 2015
Partners requested Research Establishment
Short description :
Aerodynamic design and characterization of advanced powerplant system (CROR, Turbofan for short-to-mid haul aircraft) integrated to the
airframe based on CFRP structural components.
Conceptual and detailed design and analysis of advanced powerplant solutions (UHBR, long-haul aircraft).
Conceptual design of advanced powerplant solutions (hybrid energy powerplant systems).
Definition and design of radical aircraft concepts.
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (2/8)
Title
Integrated Flow Control Applied to large Civil Aircraft
Advanced HLFC Fin Aerodynamic Design Work
Topic Number JTI-CS2-2014-CPW01-LPA-01-02
Indicative Topic Funding Value 4 M€
Duration 9 years
Start Date 1st April 2015
Partners requested Research Establishment
Short description :
Hybrid Laminar Flow Control Large Scale Demonstration.
Aerodynamic design of a fin equipped with HLFC technology
Support to definition of route towards certification.
Analysis of achieved long-term flight-test data and assessment of net benefit of the HLFC technology
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (3/8)
Title
Advanced HLFC fin design work
Structural design and manufacturing of operational HLFC fin
Topic Number JTI-CS2-2014-CPW01-LPA-01-03
Indicative Topic Funding Value 5 M€
Duration 5 years
Start Date 1st April 2015
Partners requested Ind.
Short description :
Hybrid Laminar Flow Control Large Scale Demonstration.
Structure design of a fin equipped with HLFC technology.
Development of all necessary tests, reports, means of compliance to accomplish an HLFC fin airworthy and mature for long term testing in
operational flight.
Development of the complete manufacturing process suitable for pre-serial production of the HLFC fin.
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (4/8)
Title
Integrated Engine Mounted Rear End Demonstrator
Component Design, Manufacturing and Test
Topic Number JTI-CS2-2014-CPW01-LPA-01-04
Indicative Topic Funding Value 7.5 M€
Duration 9 years
Start Date 1st April 2015
Partners requested Ind.
Short description :
Design, manufacturing, testing and complementary simulation of components for the rear mounted advanced propulsion system (CROR engine).
Design and manufacturing of components for flight demonstration of the integrated CROR engine
Design, manufacturing, testing and simulation of components for the alternative advanced powerplant system (UHBR for short to mid-haul
aircraft).
LPA topics of 1st call (5/8 & 6/8)
• These Engine Topics 5/8 and 6/8 refer to the Joint Technical Proposal (JTP), and are part of WP1.1.3. CROR demo engine (Snecma Lead) of IADP_LPA: Platform 1 - Advanced Engine and Aircraft Configuration
• The large scale demonstration will include extensive flight testing with a full size demo engine mounted on the Airbus A340-600 test aircraft.
• A second version of a Geared Open Rotor demonstrator carrying on Clean Sky SAGE 2 achievements with the aim to validate TRL 6 will be tested on ground and then on the Airbus A340 flying test bed
• From initial SAGE 2 demonstrator some engine modifications introducing various improvements will be necessary in order to obtain a flight able demonstrator(Flight Test Demo-FTD) and particularly : -a demonstrator having compatible interfaces with the Airbus A340 flying test bed and its systems -a demonstrator whose parts are flight able parts
• Topics 5/8 and 6/8 are targeting respectively the Power Turbine and the Rotating Frames of the CROR demo engine
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (5/8 & 6/8)
CS2 LPA-IADP Info day, 4th September 2014
Schedule of WP1.1.3 - CROR demo engine (Snecma lead)
3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4 1 2 3 4
Demonstrator ground test M0: 1st run ▼ ▼ D0: Results, GT Inspection
(Clean Sky SAGE 2)
Analysis of Gap between GT and FTD specifications
▼ M1: F-PDR
Preliminary design phase
▼ M2: F-CDR
Detailed Design
Rawparts ▼ M3: Pylon/mounts delivery
Manufacturing
▼
Instrumentation Build 2 (start of assembly flight engine)
Rig tests for permit to fly
Design, manufacturing & assembly of test bench ▼ D1: Engine & bench ready for ground test
adaptation
▼ M4: Flight test demo - 1st run on ground
Pass-off test
M5: Engine FRR ▼ ▼ M6: First Test in Flight
Flight Test Demo - First Test D2: Engine delivery ▼
▼ D3: Report on
Flight Test Result analysis flight test results
TRL Progresses 4 5 6
2020 2021 20222014 2015 2016 2017 2018 2019
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (5/8)
Title
Power Turbine of the Flight Demonstrator Contra Rotative Open Rotor (CROR) Engine
Topic Number JTI-CS2-2014-CPW01-LPA-01-05
Indicative Topic Funding Value 5 M€
Leading Company SAFRAN/Snecma
Duration 9 years
Start Date 1st April 2015
Partners requested Ind.
Short description :
Power Turbine of the flight demonstrator Contra Rotating Open Rotor engine design adaptation or re-design of the power Turbine (PWT) for the
Flight Test Demonstrator FTD CROR Engine
Manufacturing, Assembly/instrumentation of this PWT module, test to check the ability to fly, for example material or process tests on samples.
Design, manufacturing, Assembly/instrumentation and aero cold test of a typical "product" PWT module, test to check the ability to fly, for
example material or process tests on samples and Forward and Aft RF modules for scale 1 component tests.
PWT
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (6/8)
Title
Rotating Frames of the Flight Demonstrator
Contra Rotating Open Rotor (CROR) Engine
Topic Number JTI-CS2-2014-CPW01-LPA-01-06
Indicative Topic Funding Value 5 M€
Leading Company SAFRAN/Snecma
Duration 9 years
Start Date 1st April 2015
Partners requested Ind.
Short description :
Rotating Frames of the flight demonstrator Contra Rotating Open Rotor Engine Design adaptation or re-design of the Forward and Aft Rotating
Frame (RF) for the Flight Test Demonstrator (FTD) CROR Engine.
Manufacturing, Assembly/instrumentation of these Forward and Aft RF demo modules, test to check the ability to fly, for example material or
process tests on samples and Forward and Aft modules for scale 1 component tests.
FWD RF AFT RF
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (7/8)
Title
Airframe Cabin/Cargo and System integration Architecture
Topic Number JTI-CS2-CPW01-LPA-02-01
Indicative Topic Funding Value 5 M€
Duration 9 years
Start Date 1st April 2015
Partners requested
Short description :
Definition of functional & operational requirements of a next generation integrated Airframe-Cabin-Cargo-System architecture based on state-of-
the-art requirements as starting point.
Development of innovative overall fuselage airframe architecture with new integration approaches.
Proposal of new material options for fuselage the structure, including integrated multi-functionalities. For the integrated approach, the concepts
for advanced manufacturing shall focus to optimize production rates, manufacturing cost, installation efforts and the weight of the resulted
integrated components and structures.
Development of a Verification & Validation plan and close-to-reality testing for the final concept.
Fnext Ftoday
CS2 LPA-IADP Info day, 4th September 2014
LPA topics of 1st call (8/8)
Title
Cabin & Cargo Functional System and Operations
Topic Number JTI-CS2-CPW01-LPA-02-02
Indicative Topic Funding Value 6.5 M€
Duration 8 years
Start Date 1st April 2015
Partners requested Ind.
Short description :
Design, development and manufacturing of a linearly moveable and fully integrated Passenger Service Unit (PSU), development of the
associated electronic equipment.
Research and development for a decentralized power supply system based on the fuel cell technology with focus for an autonomous galley.
Research, development and demonstration of an On-board insert Gas Generation System (OBIGGS) able to perpetuate nitrogen enriched air as
part of a halon-free, environmentally friendly cargo fire suppression system.
Fuel Cell in Galley
Environm. Friendly Fire Suppression
(water mist + OBIGGS)
Customizable Passenger Service Unit
Hydrogen
Oxygen
from air
Elec-
tricity Water
Oxygen Depleted
Air
Heat
CS2 CfP Wave 1
• “Maintenance” part (WP 3.6): preparation of the CfP wave 1
Topic ID Topic subject Airbus
Funding (M€)
Duration (years)
Leader(s) participants
CfP_Wave 1
1
Activities related to maintenance planning and performance optimisation through fleet data managament capabilities: * Collaborative environment incl. data mining * Maintenance task planning taking into account flight schedules and available resources Activities related to maintenance execution enhancement by remote support functionalities and intergation of mobile tool solutions Activities related to "conditions based maintenance" enabling capabilities and technologies such as Integrated Health Monitoring and Management (IHMM)
7.5 4 Airbus, Thales?
2 Maintenance SHM 2.4 4 Airbus
3 Architecture_PMT-SHM and demonstration 1.75 4 Airbus
Communication approach
For general information requests regarding Large Passenger Aircraft (LPA) IADP,
please refer to [email protected]
For the submission of technical proposals please choose one of the contacts below according to your proposed contribution:
(For detailed information, please see Application Guideline)
Area of proposed contribution Contact details
Platform 1 [email protected];
Platform 2 [email protected];
Platform 3 [email protected];
Platform 1 + ITD Airframe [email protected];
clean‐sky2‐airframe@dassault‐aviation.com
Platform 2 + ITD Airframe [email protected];
clean‐sky2‐airframe@dassault‐aviation.com
Platform 3 + ITD Systems [email protected];
Q&A
Thanks for listening
CS2 LPA-IADP Info day, 4th September 2014