Innovation Takes Off C lean Sky 2 Information Day dedicated to the 4 - - PowerPoint PPT Presentation

Innovation Takes Off

Innovation Takes Off

LPA – IADP

Presented by Ralf Herrmann, Airbus Operations GmbH

Brussels, 30th of November 2016

Clean Sky 2 Information Day dedicated to the 4th Call for Core Partners (CPW04)

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

• NLF – wing for large transport aircraft and

bizjets

• CROR engine integration
• Innovative empennage for next generation

bizjets

• Innovative control surfaces
• Buffet Control Technologies
• Advanced load control architectures and

function

• Advanced Flight Test instrumentation

2 3 4 5 6

Contribute to TRL - Scale

1

TRL3

CS2 Info Day CPW04, Brussels 30/11/2016

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 Info Day CPW04, Brussels 30/11/2016

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

LPA-IADP Work Breakdown Structure

Overview of the LPA-CPW04 topics

Platform 1 Platform 3

CS2 Info Day CPW04, Brussels 30/11/2016

Platform 2

3 topics / 23,65 M€

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

LPA-IADP WBS – “Platform 1”

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations

CS2 Info Day CPW04, Brussels 30/11/2016

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

LPA-IADP WBS – “Platform 2”

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 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross function

CS2 Info Day CPW04, Brussels 30/11/2016 Estimated Volume of Activities ~290M€

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

LPA-IADP WBS – “Platform 3”

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 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstrator WP 3.5 Disruptive cockpit demonstration WP 3.6 Maintenance

Cockpit of the future (Fenics)

CS2 Info Day CPW04, Brussels 30/11/2016

Overview of the LPA-CPW04 topics

Platform 1 Platform 3

CS2 Info Day CPW04, Brussels 30/11/2016

Platform 2

3 topics / 23,65 M€

2 Topics Total funding 13,65 M€

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

Assignment of the LPA-CPW04 topics to the LPA-IADP WBS

LPA 01-11 LPA 01-12

LPA-PL1-CPW04 HLFC on Wing Strategic Topic Description Core Partners Call

Innovation Takes Off

http://www.cleansky.eu/content/homepage/about-clean-sky-2

LPA – PL1

Presented by Simona Di Credico - AIRBUS

Brussels, 30th of November 2016

CPW04 - WP1.4.4 HLFC Wing - ‘Topic Description ’

• Background
• Objectives
• Scope of Work
• Deliverables
• Milestones
• Skill and Capabilities

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04-LPA-01-01 - ‘Design of a Wing with HLFC’

Type of action (RIA or IA)

CS2-IA

Programme Area

WP1.4.4

Joint Technical Programme (JTP) Ref.

JTP_v5

Indicative Funding Topic Value

10.0 M€

Topic Leader

Airbus

Duration of the action (in Months)

72 Start Date January 2018

Identification Number Title

JTI-CS2-2016-CPW04- LPA-01-01 Design of a wing with HLFC (Hybrid Laminar Flow Control) technology

Short description (3 lines)

Design and construction of a wing with HLFC technology and corresponding manufacturing process, proven by means of a large-scale ground-based demonstrator.

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Background’

• The HLFC technology has a significant drag reduction

potential.

• HLFC physics and the technical principles are well

understood.

• No “industrial” technology solution could be developed

keeping the complexity and weight of the required systems low.

• Effort and cost to manufacture, operate and maintain these

systems need to be brought down to an acceptable level.

• This Strategic Topic covers the WP1.4 “Hybrid Laminar Flow

Control Large Scale Demonstration” in IADP-LPA, Platform 1.

• Major scope is the design and construction of a wing with

HLFC (Hybrid Laminar Flow Control) technology and corresponding manufacturing process, proven by means of a large-scale ground-based demonstrator.

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Background’

SUCTION SHAPING

HLFC is used to reduce friction drag on the wing.

• Total aircraft drag reduction can be achieved

through aerofoil profiles assisted by passive suction through the wing skin forward of the front spar.

• The aerodynamic design of the aerofoil should

allow for laminar flow and be tolerant to surface imperfections.

• A matured structure and simplified air system

concept is needed for laminar flow at acceptable cost and weight

• A mature industrial process is needed to allow

tight manufacturing tolerances to be achieved.

• An integrated means to protect against

contamination on the leading edge is needed to ensure operability.

Up to 8% reduction in total aircraft drag is achievable

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Objectives’

Highly multidisciplinary and integrated working environment requiring ‚Plateau‘ phases Demonstrate a fully integrated HLFC wing by means of a large-scale ground based demonstrator to achieve Technology Readiness Level 4 (TRL4). TRL4: Validation in laboratory environment. Basic technological components are integrated to establish that the pieces will work together.

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Objectives’

• Aerodynamic shape design and determination of the aerodynamic performance incl. boundary layer

characterisation by means of stability calculations. Validation of numerical results by Wind Tunnel model testing.

• HLFC wing based on a passive suction concept (fall-back solution is minimum active suction support).

Aerodynamics Structure & Manufacturing

• Design and manufacturing process to target highest ecological standards (“ECO” design).
• Design and manufacturing process to comply with the standards and procedures of the topic proposer

Airbus.

• Fulfilment of surface quality requirements following wing technical design directive of Airbus.
• Proof of structure and system integrity in case of damage or heavy environmental conditions.
• Development of the complete manufacturing process suitable to pave the way for pre-serial

production of the HLFC wing demonstrator.

• Manufacturing process to target for a later HLFC wing production at high-rate and low cost.
• Development of repair solutions for the chosen structure and manufacturing concept.

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Objectives’

• A functioning ice protection system in the leading edge of the HLFC wing.
• A functioning passive suction system (fall-back solution is minimum active suction support).

Systems Operability

• Support the determination of the operational envelope of aircraft equipped with HLFC technology on

wing.

• Early consideration of in-service/maintenance aspects such as easy interchangeability and interface

design concepts between components.

• Development of the test plan and definition of required tests for proof of structure concept and system

integrity.

• Development of all necessary tests, reports, means of compliance to qualify the HLFC wing including all

integrated structural elements, technologies and systems to a TRL status at integrated major component level, which will enable the realization of an industrial demonstrator. Tests

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Objectives’

• Prove the complete functionality of the integrated HLFC system, operational envelope limited to ground-

based test conditions.

• Integration capability of all other required systems (such as high-lift devices, actuators, pipes, harness,

etc.).

• Support the determination of the operational envelope of aircraft equipped with HLFC technology on

wing.

• Close interaction with the topic proposer Airbus, working in a multi-disciplinary environment of various

design organizations/teams, either remotely or in a collocated manner.

• “Plateau” phases of collocated teams of the Airbus and the Core Partner are seen as a strong enabler to

jointly and efficiently develop the HLFC wing configuration and preliminary integrated HLFC wing design concept.

• 1st level design responsibility on Airbus side.
• Determination and the monitoring of the evolution of the Non-Recurring Costs (NRC) and Recurring

Costs (RC) along the proposal phase.

• Assessment of the detailed design concept for the HLFC wing on overall aircraft level so that finally a

precise determination of the net benefit level is possible. Integration

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing - ‘Scope of Work’

Major research pillars in Europe for HLFC design experience: I. FP7 L2 Project ”AFLoNext” - Application of a simplified HLFC technology on fin of a Large Passenger Aircraft - flight test campaign in 2017. HLFC wing demonstrator (mid scale) to investigate micro-perforated wing leading edge skin manufacturing concept and to demonstrate the principle physical integration of all essential systems, structure and technologies. II. “HIGHER-LE” - Demonstration by means of a large-scale Wind-Tunnel Test (WTT) of advanced HLFC design and manufacturing concept for the fin of a Large Passenger Aircraft. Improvement of new- or refinement of existing methods and tools to assess the performance of the HLFC technology. III. CS2 - in LPA, Platform 1, WP1.4.1 - Development of the HLFC technology applied on Horizontal Tail Plane (HTP) of a Large Passenger Aircraft.

Main Scope of Work

• Demonstration of a fully integrated HLFC wing
• by means of a large-scale demonstrator plus supporting small-scale

demonstrators

• including all essential systems, sub-structures and sub-technologies to

achieve a TRL4 on integrated major component level

Access to all the necessary IPs and IP protection to be demonstrated by the applicant

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing- ‘Major Deliverables’

Type: R: Report RM: Review Meeting D: Delivery

• All deliverables might be subject to change
• Further deliverables will be defined during negotiation phase and during the 1st project phase

Deliverables

• Ref. No.

Title - Description Type Due Date

D1.4.4-1 Project design finalized, configuration and

• verall aircraft assessment of HLFC wing

done. R/RM Q1/2018 D1.4.4-2 Preliminary integrated wing design with selected structure and system concept available R/RM Q3/2018 D1.4.4-3 Test plan available and required tests defined (for proof of concept) R/RM Q2/2019 D1.4.4-4 Fully multidisciplinary design loop for baseline design and concept definition available R/RM Q2/2020 D1.4.4-5 Wind Tunnel (WT) model designed and ready for test RM/R/D Q2/2021 D1.4.4-6 Wind-Tunnel Test (WTT) performed and analysed R Q1/2022 D1.4.4-7 Large-scale ground-based demonstrator ready to test D Q4/2022 D1.4.4-8 Final aerolines and HLFC wing concept frozen RM/R Q3/2022 D1.4.4-9 Data from test with large-scale ground-based demonstrator analysed, validated and reported RM/R Q2/2023 D1.4.4-10 Detailed design concept for HLFC wing available RM/R Q3/2023

Deliverables

CS2 Info Day CPW04, Brussels 30/11/2016

Type: RM: Review Meeting

• All milestones might be subject to change
• Further milestones will be defined during negotiation phase and during the first project phase

Milestones

• Ref. No. Title – Description

Type Due Date

M1.4.4-1 TRL3: concept freeze RM Q3/2020 M1.4.4-2 Feasibility demonstration towards TRL4 RM Q2/2023

WP1.4.4 HLFC on Wing Milestones

Concept Freeze

2018 2017 2019 2020 2021 2022 2023

TRL4 TRL3 Feasibility Demonstration

Milestones

CPW04 - WP1.4.4 HLFC Wing- ‘Major Milestones’

CS2 Info Day CPW04, Brussels 30/11/2016

Start January 2018

CPW04 - WP1.4.4 HLFC Wing – ‘Skills & Capabilities’

• High experience in working in a multidisciplinary and integrated design environment.
• Core Partner as essential management element in the organisation of the project management

plan.

• A world-class background and experience in overall aircraft design, in particular in the field of

flight physics, structure- and system design compliant to FAR 25/EASA CS-25 rules and regulations and all respective ATA chapters.

• Design Organization Approval (DOA) for commercial aircraft design and build and signature

authority or delegated authority by the customer.

• Outstanding skills and capabilities in manufacturing and assembly of major airframe

components, either in metallic and/or composite, for Large Passenger Aircrafts or other certified aircrafts in commercial aviation.

• Readiness to:

 take responsibility in the technical lead of action  follow possible necessary technical program changes/adaptions

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04 - WP1.4.4 HLFC Wing – ‘Skills & Capabilities’

• Proven and widely recognized expertise, methods and tools for virtual and physical testing,

design and execution of experiments.

• Experience in-depth project management in time, cost and quality together with evidence.
• Responsibility for work package lead co-developing the project management plan and closely

monitoring the project progress.

• Special required skills in aircraft design and production:

 For shape design, component design, structural analysis tool set commonly used by the topic proposer Airbus, such as CATIA v5, NASTRAN.  Installation, assembly and space allocation studies having Digital Mock-Up (DMU) capability.  High-fidelity numerical (CFD) and experimental skills for aerodynamic design, modelling and analysis.  Proven and widely recognized expertise in HLFC design capability using a validated tool chain, incl. stability calculations, suction and surface requirements, etc.

CS2 Info Day CPW04, Brussels 30/11/2016

Overview of the LPA-CPW04 topics

Platform 1 Platform 3

CS2 Info Day CPW04, Brussels 30/11/2016

Platform 2

3 topics / 23,65 M€

1 Topic Total funding 10 M€

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

Assignment of CPW04-topics to the LPA-IADP WBS

LPA 02-15

JTI-CS2-2016-CPW04-LPA-02-03 Development and manufacturing of multifunctional and integrated thermoplastic fuselage shell, passenger floor and cargo floor including the main system, cabin and cargo elements

Innovation Takes Off

http://www.cleansky.eu/content/homepage/about-clean-sky-2

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

Top objectives

WP2.1 objective is the integration of cabin and systems into primary aircraft structure to reduce weight, enhance space for passengers and cargo and to reduce manufacturing cost by

• removing artificial separation of functions already at

the aircraft design stage.

– Significant weight and hence environmental improvements expected

• consideration of the aircraft manufacturing,

assembly and installation processes

– aircraft cost reductions.

Structure technology is enabler for integration Timescale: Q3 2014 – 2023

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

CS2 Info Day CPW04, Brussels 30/11/2016

Background

The overall objectives, linked closely to the CS2 objectives are:

• Enable a high production rate of minimum 60 aircrafts per month
• Weight reduction: -1t
• Competitive improvements (reduction of recurring costs): -1M€

compared to a fully equipped current Single Aisle Aircraft fuselage as benchmark.

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

The applicant’s work will be directly linked to WP2.1.5 “Demonstrator Design and Manufacturing” with smaller contributions to WP2.1.3. “Integrated Concepts Definition and Maturation” and WP2.1.6 “Demonstrator Test”

CS2 Info Day CPW04, Brussels 30/11/2016

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

TS

2014 2015 2016 2017 2018 2019 2020 2021 2022 2023

Multi Functional Fuselage Demonstrator

CS2 Info Day CPW04, Brussels 30/11/2016

Multi functional fuselage demonstrator

Maturation Phase Demo design & Manufacturing Concept phase Proof of Operational performance Means of Production Technology Development Demonstrator and Validation

Manufacturing Concepts Manufacturing Infrastructure Demonstrator Engineering Tooling, lay-up heads, grippers

Definition of toolings Order of toolings

Manufacturing Design & Simulation Development of Joining Technologies Development of Manufacturing Processes Cost Estimation Concept and Validation Barrel Assembly Panel Manufacturing Shell Assembly

Delivery of toolings Handover to Final Assembly Demonstrator ready Architecture/ Concepts TRL1 TRL2 TRL3 TRL4 TRL5 partly TRL6

CP W4

Route to TRL6

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

CS2 Info Day CPW04, Brussels 30/11/2016

Length of the shell: >8 meters Radius: ~1.98 meter (single aisle configuration)

CS2 Info Day CPW04, Brussels 30/11/2016

General skills, capabilities

• It is expected that the applicant has a strong aerospace industry background and

experience in overall aircraft design, airframe manufacturing and overall integration

• Furthermore, the applicant shall be able to demonstrate sound technical

knowledge in the field of proposed contributions; he shall be able to demonstrate that this knowledge is widely recognized.

• The applicant shall demonstrate experience in-depth project management in

Time, Cost and Quality together with evidence of past experience in large project participation.

• It is intended that the applicant takes also responsibility for work package co lead

(incl. co-developing the project management plan and closely monitoring the project progress) which in detail has to be defined in the negotiation phase.

• The applicant shall provide evidence to be able to cope with the required high

level of adequate resources in qualified personnel, required tools and equipment.

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

CS2 Info Day CPW04, Brussels 30/11/2016

Special Skills:

The applicant has:

• the capability for fuselage stress analyses and design (airframe and installation cabin or systems),
• A/C manufacturing engineering capabilities,
• Simulation capabilities for static, dynamic structural behavior as well as for acoustics and system

behavior

• Capabilities and experience to manufacture large A/C thermoplastic composite structure parts,
• Engineering capabilities in water/ waste systems, ventilation systems, monuments like galleys,

lavatories, stowage and partitions, electrical systems like cabin light, avionics, sensors, wireless communication

• capabilities in integration of fuselage structure, cabin and system,
• capabilities in Material & Processes to select appropriate combinations,
• Project management skills as requested in chapter 2,
• Automation specialists to optimize the concept between manufacturing and development of the new

integrated approach,

• capabilities in certification (across related ATA chapters, CS-25),
• capabilities and knowledge in requirement based engineering and lean manufacturing
• capabilities to perform static and dynamic mechanical tests on small test elements like structural

coupons, lining parts, interior parts and air ducts

• capabilities to perform FST (fire, smoke, toxicity) tests
• capabilities to perform acoustic tests on SA (Single Aisle) fuselage shells and sections
• knowledge of and experience in the Airbus supply chain
• ability to work in an integrated supply chain

CPW04-LPA-02-03 ‘Multifunktional Thermoplastic Shell’

Overview of the LPA-CPW04 topics

Platform 1 Platform 3

CS2 Info Day CPW04, Brussels 30/11/2016

Platform 2

3 topics / 23,65 M€

No Topics

CS2 Info Day CPW04, Brussels 30/11/2016

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 Applied technologies for enhanced aircraft performance WP 1.6 Demonstration of radical aircraft configurations Platform 2 – WP 0 Innovative Physical Integration Cabin-System-Structure WP 2.1 Next generation fuselage, cabin and systems integration WP 2.2 Next generation cabin & cargo functions WP 2.3 Next generation lower centre fuselage WP 2.4 Non-specific cross functions Platform 3 – WP 0 Next Generation Aircraft, Cockpits Systems & Avionics WP 3.1 Enhanced flight operations & functions WP 3.2 Innovative enabling technologies WP 3.3 Next generation cockpit functions flight demonstration WP 3.4 Enhanced cockpit demonstration WP 3.5 Disruptive cockpit demonstration WP 3.6 ADVANCE (Maintenance)

Assignment of CPW04-topics to the LPA-IADP WBS

Questions?

Any questions on the 4th Call for Core Partners can be addressed to the following mailbox:

Info-Call-CPW-2016-01@cleansky.eu

Last deadline to submit questions – check CS2 website and EC Participant Portal

Thank you !

CS2 Info Day CPW04, Brussels 30/11/2016

Thank You

Not legally binding 09/03/2016 43

Disclaimer

• The content of this presentation is not legally binding and subject to modifications and evolution over the info days on Clean Sky 2 until

the adoption of the Regulation on Clean Sky 2 JU. Any updated version will be regularly advertised on the website of the Clean Sky JU.

• The selection of Partners will be based on Horizon 2020 Rules for Participation (already in force), the rules for submission of proposals,

evaluation and selection of Partners as adopted by the Governing Board of Clean Sky 2 JU .

• The proposed content/approach is based on the consultation with the “National States Representative Group” and the “Task Force “ of the

Clean Sky 2 Programme