Clean Sky Joint Undertaking

Airframe ITD

Vittorio Selmin Project Officer

Step changes in the “efficiency” of all airframe elements by the means of a systematic “re-thinking”

Re-think the a/c architecture

Re-think the fuselage

Re-think the wing

Re-think the control

Re-think the cabin

Smart Fixed Wing Aircraft

• Greener Airframe Technologies • More Electrical a/c architectures

• More efficient wing • Novel Propulsion Integration Strategy • Optimized control surfaces

• Integrated Structures • Smart high lift devices

Background

Weight New Materials

Manufacturing Cost

Drag Maintenance More Efficient Airframes Cabin

Efficiency of the engineering & manufacturing process Time to Market

(lead Time)

High Performance & Energy Efficiency High Versatility & Cost Efficiency

Innovative Aircraft

Architecture

Advanced Laminarity

High Speed Airframe

Novel Control

Novel travel

experience

Next generation optimized

wing

Optimized high lift configs.

Advanced integrated structures

Advanced Fuselage

REG

IADP/Integrated Demonstrators

FRC

LPA

AIR Bizjet

SAT

SUPPORT TO IADP: Maturate technologies up to TRL 6

TRANSVERSE Eco-Design for Airframe & Modeling to certification ability

FUTURE: De-risk novel generation product in the prospect of changing step by 2030+

Noise

FRC

AIR Bizjet

SAT

LPA

REG

Key General Objectives

Work Breakdown Structure

M - Management

& Interface

TS A-1: Innovative

Aircraft

Architecture

TS A-2: Advanced

Laminarity

TS A-3: High Speed

Airframe

TS A-4: Novel

Control

TS A-5: Novel

travel experience

WP M-1 WP A-1.1 WP A-2.1 WP A-3.1 WP A-4.1 WP A-5.1

Overall

Management

Optimal engine

integration on rear

fuselage

Laminar nacelleMultidisciplinary wing

for high & low speed

Smart mobile control

surfaces

Ergonomic flexible

cabin

WP M-2 WP A-1.2 WP A-2.2 WP A-3.2 WP A-4.2 WP A-5.2

Business Aviation

OAD & config. Mgt

CROR & UHBR

configurations

NLF smart

integrated wing

Tailored front

fuselageActive load control

Office Centered

Cabin

WP M-3 WP A-1.3 WP A-2.3 WP A-3.3

LPA

OAD & config. Mgt

Novel high

performance

configuration

Extended laminarityInnovative shapes &

structure

WP M-4 WP A-1.4

RotorCraft OAD &

configuration Mgt

Virtual modelling for

certification

WP M-5

Regional a/c

OAD & config. MgtC - Eco-Design

TS B-1: Next

Generation

optimized wing box

TS B-2: Optimized

high lift

configurations

TS B-3: Advanced

Integrated

Structures

TS B-4: Advanced

Fuselage

WP B-1.1 WP B-2.1 WP B-3.1 WP B-4.1 WP C-1

Wing for incremental

lift & transmission

shaft integration

High wing / large

Tprop nacelle

configuration

Advanced

Integration of syst. in

nacelle

Rotor-less tail for Fast

RotorcraftEco-Design TA Link

WP B-1.2 WP B-2.2 WP B-3.2 WP B-4.2 WP C-2 (ex A-3.4)

More affordable

composite structuresHigh lift wing All electrical wing

Pressurized fuselage

for Fast Rotorcraft

Eco-Design for

airframe

WP B-1.3 WP B-3.3 WP B-4.3 WP C-3 (ex B-3.6)

More efficient wings

technologies

Highly integrated

cockpit

More affordable

composite fuselage

New materials &

manufacturing

WP B-1.4 WP B-3.4 WP B-4.4

Flow & shape controlMore affordable small

a/c manufacturing

Low weight, low cost

cabin

A - High Performance and Energy Efficiency

B - High Versatility and Cost Efficiency

AERNNOVA Aerospace S.A.U. (ATP) AERNNOVA Aerostructuras ALAVA, S.A. (ATP) AERNNOVA Composites ILLESCAS S.A. (ATP) Internacional de Composites SAU (ATP) Fibertecnic SAU (ATP) INTEC-AIR (ATP) Componentes aeronauticos SA (ATP)

AERNNOVA ENGINEERING DIVISION SAU (ATP)

MEGGITT Aerospace LTD

University of Sheffield

Vrije Universiteit Brussel

Deutsches zentrum fuer Luft und Raumfahrt EV

Barcelona Supercomputing Centre

CT Ingenieros A.A.I. S.L.

CAETANO AERONAUTIC SA

ACUMEN Design Associates Ltd

GEVEN Spa

Akzo Noble Car Refinishes BV

Universidad Politécnica de Madrid

Testing and Engineering of Aeronautical Materials and Structures SL

ONERA

Imperial College of London

GE Aviation

Stichting Nationaal Lucht- en Ruimtevaartlaboratorium

TU DELFT

Fundación Andaluza para el Desarrollo Aeroespacial

Fundación Tecnalia Research & Innovation

Fundación Centro de Tecnologías Aeronáuticas

Fundacion para la Investigacion, Desarollo y Aplication de Materiales Compuestos

PARTICIPATING LEADERS**

Precision Micro Limited (ATP)

University of Nottingham

ARTUS SAS

Meggitt A/S

Ultra Electronics LTD

AEROTEX UK LLP

CIRA

INVENT Gesellschaft mit beschränkter Haftung

Università degli Studi di Napoli "Federico II"

PGA Electronic

Alma Mater Studiorum- Università di Bologna

Noesis Solutions NV

Design Manufactoring Spa

SIEMENS Industry Software NV

Politecnico di Torino

Israel Aerospace Industries Ltd.

INtegrated Aerospace Sciences COrporation

ALTRAN Deustchland SAS & Co KG

LORTEK S.COOP

Aero-Magnesium Limited ACS

University of Patras

Universitaet Stuttgart

CORIOLIS Composite Technologies

DANOBAT S.Coop

TECHNI-MODUL ENGINEERING

ALMADESIGN CONCEITO E DESENVOLVIMENTO DE DESIGN LDA CRITICAL MATERIALS SA EDISOFT-EMPRESA DE SERVICOS E DESENVOLVIMENTO DE SOFTWARE SA GMVIS SKYSOFT SA OPTIMAL STRUCTURAL SOLUTIONS Lda CENTRO PARA A EXCELENCIA EINOVACAO NA INDUSTRIA AUTOMOVEL TEKEVER - TECNOLOGIAS DE INFORMACAO, S.A.

AERTEC Ingenieria y Desarollos SLU

AVIAERTEC LDA

Instituto de Ciencia e Inovacao EM Engenharia Mecanica e Engenharia Industrial

Instituto de Soldadura e Qualidate

INSTYTUT LOTNICTWA

Polskie Zaklady Lotnicie sp zoo

EUROTECH

SZEL-TECH

P.W Metrol Dabkowski Dariusz

ULTRATECH Sp zoo

ZAKLADY LOTNICZE MARGANSKI & MYSLOWSKI SA

FOKKER Aerostructures B.V. Fokker Technologies Holding B.V.

ASCO Industries N.V.

BALANCE DEMOS

NEODAMP

SIMCODEQ

RESET

NEWCORT

DISTRACTION

BLADEOUT

INSCAPE

REDISH

ERACLE

FRCDOORDEMONSTRATOR

HEPODIS

ASPIRE

CRORTET

ELEMENT

DADIYSO COMP

CRO-INSPECT

BRIDAS

COFRARE 2.0

TRANSITION

PIPS

E2S2A2

INDUCTICE

IMCA

OLTITA

OLFITT

WINNER SPECTRAL

WINBOXTOOL

TAMI

ADDMAN

FORMIT

HAIRD

TR4EMACS

SMART-LAYUP

PILOT

COBOMEGA

CORDIAL

RODEO

WIN-TOOL

AMTRAS

SHERLOC QSP

TESTCONCERT

MOTIVATE

OPTIMORPH

CRISTA

ARIESS

RIB-ON

PSIDESC

C-JOINTS

MISSP

ACCURATE

CfP PROJECTS

CORE PARTNERS

LEADER

**incl. Affiliates and Third Parties

[Project ] = related to Small Air Transport

Share of funding foreseen

Participants to date

Countries involved to date

Leader 16.7% 4* 4

Part. Leaders

23.2% 13* 6

Core Partners

30.0% 76* 12

Partners 30.1% 124** 16**

*incl. Affiliates and Third Parties

PIPS

PRODIGE

DOVER

INNOHYBOX

OPTIWIND

OASIS

I3PS

AMULET

AFPMET

ADD-ON

ASTRASY

DILECO

MAF

PASSPORT LABOR MEPAFUS

** till CfP04

RAMAL srl

Broad Participation: e.g. AIR (till CfP06)

AIR ITD - CfP Status – CfP08

Topic nb CfP Title Topic

Leader

WP/

Task

Type of

Action

Duration

(Month)

Est.

budget

[k€]

HPE

AIR-01-37 Composite mould tool based on 3D printing. SAAB A-3.1 RIA 24 800

AIR-01-38 Investigation of gust loads in a transonic flow based on an innovative test rig. ONERA A-4.2 RIA 24 1000

AIR-01-39 In-Seat Ventilation & Supply for Personalized Comfort Control on Board an Aircraft AIB A-5.1 IA 18 450

HVC

AIR-02-60 Full Scale Innovative Integrated Tooling for Composite Material Wing Box (SAT) IAI B-1.2 IA 20 950

AIR-02-61 Development and Optimization of Bonding Assembly Technology for a Wingbox (SAT) IAI B-1.2 IA 20 900

AIR-02-62 Virtual-Hybrid-Real On Ground demonstration for HVDC & EMA Integration ADS B-3.2 IA 24 400

AIR-02-63 Enhanced Low Cost Complex Composite Structures ADS B-2.2 IA 18 750

AIR-02-64 Cold Spray of metallic coatings on polymer and composite materials. (SAT) PZL B-3.4 IA 24 700

AIR-02-65 Design of special welding head for FSW process with automatic adjustable pin and welding force

control system (SAT)

PZL B-3.4 IA 24 700

AIR-02-66 Evaluation and modelling of comfort driving parameters in a Cabin Demonstrator FhG B-4.4 RIA 36 1100

AIR-02-67 Model based development of an innovative ECS air distribution system supported by a generic

laboratory ECS analogue allowing for piecewise integration of ECS components prototypes for

ground testing with a Cabin Demonstrator

FhG B-4.4 RIA 36 1300

Eco-Design (ED)

AIR-03-01 Bio contamination survey and tests DAv C-2.1 IA 36 500

AIR-03-02 Non destructive control (NDT) of sticking and assemblies focused on tightness DAv C-2.1 IA 36 600

AIR-03-03 Sizing for recycled carbon fibres to optimise adhesion in organic/inorganic composite materials. FhG C 2.1.4 RIA 30 500

AIR-03-04 Development of an anaerobic digester prototype for aircraft use FhG C 2.1.4 RIA 24 400

AIR-03-05 Development and evaluation of a manufacturing process for a lightweight aircraft wheel made of

CFRP

FhG C 2.3.1 IA 24 450

16 Topics 11.5 Meuro

Innovation Takes Off

Q&A

Thank You

Backup Slides

11

CfP08 - HPE

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-01-37 Composite mould tool based on 3D printing. HPE A-3.1 RIA 24 800

12

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-01-38 Investigation of gust loads in a transonic flow based on an

innovative test rig.

HPE A-4.2 RIA 24 1000

CfP08 - HPE

13

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-01-39 In-Seat Ventilation & Supply for Personalized Comfort Control on

Board an Aircraft

HPE A-5.1 IA 18 450

CfP08 - HPE

14

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-60 Full Scale Innovative Integrated Tooling for Composite Material

Wing Box

HVC B-1.2 IA 20 950

CfP08 - HVC

15

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-61 Development and Optimization of Bonding Assembly Technology

for a Wingbox

HVC B-1.2 IA 20 900

CfP08 - HVC

16

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-62 Enhanced Low Cost Complex Composite Structures HVC B-2.2 IA 18 750

CfP08 - HVC

17

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-65 Cold Spray of metallic coatings on polymer and composite

materials.

HVC B-3.4 IA 24 700

CfP08 - HVC

18

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-63 Virtual-Hybrid-Real On Ground demonstration for HVDC & EMA

Integration

HVC B-3.2 IA 24 400

CfP08 - HVC

19

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-65 Designing of special welding head for FSW process with

automatic adjustable pin and welding force control system

HVC B-3.4 IA 24 700

CfP08 - HVC

20

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-66 Evaluation and modelling of comfort driving parameters in a Cabin

Demonstrator

HVC B-4.4 RIA 36 1100

CfP08 - HVC

21

JU Ref. CfP Title Activity

Line WP/Task RIA or IA

Duration

(Month)

Est. budget

[k€]

JTI-CS2-2018-CFP08-AIR-02-67 Model based development of an innovative ECS air distribution

system for ground testing with a Cabin Demonstrator

HVC B-4.4 RIA 36 1300

CfP08 - HVC

CfP08 – ECO DESIGN

CfP08 – ECO DESIGN

CfP08 – ECO DESIGN

CfP08 – ECO DESIGN

CfP08 – ECO DESIGN

27

Key Objectives • Validate through demonstration of integrated technologies :

• To introduce innovative airframe architecture

• To introduce technologies for more efficient airframe : drag, weight, cost, environmental impact, passenger well-being, maintenance, servicing, …

• To enhance the efficiency of the engineering & manufacturing process : time-to-market and competitiveness against low-cost labour countries,

• To fully address a technology issue from modeling to certification ability

• Serve maturity up to TRL 6 of airframe technologies

• De-risk novel generation product in the prospect of a next game changing step by 2030+

• Support next generation bizjets and general aviation directly

• Support Large a/c, regional a/c and rotorcraft directly and through IADPS

• Create Product differentiators

Supporting a 5 Product’s Segments Strategy Base

Concept

Analysis

Technology Streams

Innovative Aircraft Architecture

Advanced Laminarity

High Speed Airframe

Next Gen. optimized wing box

IADP LPA

IADP RA

IADP Rcraft

ITD Engine ITD Systems

Novel Control

Advanced Fuselage

Novel Travel Experience

Optimized high lift configurations

Advanced Integrated Structures

IADP LPA

IADP RA

IADP Rcraft

SAT Transverse

act°

ITD Systems

TEECO

Specifications & Requirements

Technology Development & Demonstration

Integration Profile Development Integrated

Concept demonstrat°

prototype airframe componts

Inte

rfac

ing

& c

ross

inte

ract

ion

man

agem

ent

Novel innovation

waveTRL <= 5

HPE

HVC

HPE: High Performance and Energy Efficiency

HVC: High Versatility and Cost Efficiency

Overall Technical Overview