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


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


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


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


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


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




WP 0

LPA – IADP

WP 0.1

Technology assessement

WP 0.2

EcoDesign

WP 0.3

ITD - Interfaces

Platform 1 – WP 0


WP 1.1


WP 1.2


WP 1.3


WP 1.4


WP 1.5


WP 1.6


Platform 2 – WP 0


WP 2.1


WP 2.2


WP 2.3


Platform 3 – WP 0


WP 3.1




WP 3.3


WP 3.4


WP 3.5


WP 3.6

Maintenance


Next Gen. A/C Systems, Cockpit Systems & Avionics



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


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


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


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


• Aerostructure manufacturers



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


• Industrial suppliers


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


• System suppliers


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


• Cabin and Cargo manufacturers



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


• Cabin and Cargo manufacturers



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



• Advanced testing facilities


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



• Industrial engineering

• Automation

• Logistics


WP 0

LPA – IADP

WP 0.1

Technology assessement

WP 0.2

EcoDesign

WP 0.3

ITD - Interfaces

Platform 1 – WP 0


WP 1.1


WP 1.2


WP 1.3


WP 1.4


WP 1.5


WP 1.6


Platform 2 – WP 0


WP 2.1


WP 2.2


WP 2.3


Platform 3 – WP 0


WP 3.1




WP 3.3


WP 3.4


WP 3.5


WP 3.6

Maintenance



Setup and Implementation LPA Platform 3

Estimated Volume of Activities ~222M€

Next Gen. A/C Systems, Cockpit & Avionics



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)



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



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



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


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


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€


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


Timescales

• From Q3-2015 up to Q4-2018

Gross budget provisions • 30.4 M€


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)


• Critical phases evaluation in flight

Potential partners



Timescales

• From Q1-2018 up to Q4-2020


• 37.6 M€


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


• Overall functional integration

• Crew evaluation and buy-in

Potential partners



Timescales

• From Q1-2020 up to Q4-2023


• 67.6 M€


WP 3.5 “Pilot case” demonstrators

Objectives

• Specific testing of devices not implemented in WP3.3 and WP3.4


• Case by case focus (performance demonstration)

Potential partners

• CP: Large system industry


Timescales

• From Q1-2020 (TBC) up to Q4-2023 (TBC)

• Planning definition will be done on a case-by-case basis


• 10.6 M€

Example: AVOID (Airborne Volcanic Object Identifier

and Detector) Technology


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


• 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


• 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



LPA topics of 1st call (1/8)

Title


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.



Title

Integrated Flow Control Applied to large Civil Aircraft

Advanced HLFC Fin Aerodynamic Design Work



Duration 9 years


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



Title

Advanced HLFC fin design work

Structural design and manufacturing of operational HLFC fin



Duration 5 years


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.



Title

Integrated Engine Mounted Rear End Demonstrator

Component Design, Manufacturing and Test


Indicative Topic Funding Value 7.5 M€

Duration 9 years



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


LPA topics of 1st call (5/8 & 6/8)


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



Title

Power Turbine of the Flight Demonstrator Contra Rotative Open Rotor (CROR) Engine



Leading Company SAFRAN/Snecma

Duration 9 years



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



Title

Rotating Frames of the Flight Demonstrator

Contra Rotating Open Rotor (CROR) Engine



Leading Company SAFRAN/Snecma

Duration 9 years



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



Title

Airframe Cabin/Cargo and System integration Architecture

Topic Number JTI-CS2-CPW01-LPA-02-01


Duration 9 years


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



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



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]

[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];

[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];

[email protected]

mailto:–[email protected]

mailto:[email protected]



























mailto:clean‐sky2‐airframe@dassault‐aviation.com






mailto:clean‐sky2‐airframe@dassault‐aviation.com









Q&A

Thanks for listening


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