Innovation Takes Off - Camera di commercio, Torino Takes Off. Clean Sky 2 12 Maggio 2014, ... INNOVATIVE FLIGHT CONTROL SYSTEM ... (EADS CASA + Systems) SYSTEMS ITD SYNERGIES

Innovation Takes Off

Clean Sky 2 12 Maggio 2014, Torino

Regional Aircraft (RA) IADPVito PERRUPATO, Alenia Aermacchi

Innovation Takes Off

1. THE REGIONAL AIRCRAFT• Current Clean Sky GRA• From Clean Sky towards Clean Sky 2

2. SET-UP AND IMPLEMENTATION• The Regional Aircraft IADP (R-IADP)• Work Breakdown Structure• Technologies Waves• Demonstrators• Organization, Risk Management• Widely opened programme

3. R-IADP HI-LEVEL TECHNICAL CONTENTS, PLANNING, OPPORTUNITIES• WP1 – High Efficiency Regional Aircraft• WP2 – Technologies Development• WP3 – Demonstrations• WP4 – Technologies Development & Demonstrations Results

4. LEADERS POCs

PRESENTATION OUTLINE

Structure of Current Clean Sky Program

Eco-designFor Airframe and Systems

Smart Fixed-Wing

Aircraft

Green Regional

Aircraft (GRA)

Green

Rotorcraft

Clean Sky Technology Evaluator

Sustainable and

Green Engines

Systems for Green

Operation

Leaders: Airbus

& SAAB

Leaders: Eurocopter

& AgustaWestlandLeaders: Alenia

& EADS CASA

Leaders: Dassault Aviation

& Fraunhofer Institute

Leaders: Rolls-Royce & Safran

Leaders: Liebherr

& ThalesITD: Integrated Technology Demonstrator

Tra

nsvers

e I

TD

for

all v

eh

icle

s

Vehicle ITDs

Regional AircraftCurrent Clean Sky GRA – 5 Domains

Innovative systems (All Electrical Aircraft)

Lower fuel consumption through

Bleed less architectures, Limited hydraulics,

Energy management

Advanced aerodynamics (Low Noise Configuration)

Improved aerodynamic efficiency

Drag reduction

Lower Airframe external noise through

innovative solutions for wing and high lift devices and landing

gears

New aircraft configurations (NC)

Lower fuel consumption

NOx & CO2 reduction through

Integration of Advanced turboprops, Open

Rotors, Advanced turbofan

Evaluation of new avionics architecture in

MTM domain for

Fuel & noise reduction

Lower Maintenance costs through

Upgraded capabilities for MTM

Innovative structures (Low Weight Configuration)

Lower weight

Lower maintenance costs through

multifunctional composites, advanced metallic materials,

structure health monitoring

Regional AircraftFrom Clean Sky towards Clean Sky 2

• Clean Sky GRA demonstrators on-track for 2015 demo’s:

• Strong need of a much higher level of technologies integration through Clean Sky 2 Demonstrators: regiona:

Electric

ECS

Electrical

Energy

Management

270 HVDC

network

demo channel

Advanced

Fuselage Panel

Static and Fatigue tests on:

Fwd Fuselage SectionWing Box Section Cockpit Section

Full Scale Flying and

GroundDemonstrations

Component Flying Demonstrator

(Structural Panel, Electrical Energy

Management, E-ECS)

Ground Validation tests

Scope : Component, Single Discipline

(E.g. Struct. Component Tests, W/TT, Test Rigs)

Fuselage

Wing

High Integration of Technologies at Aircraft Level

GRA

CS2

In Clean Sky GRA, several advanced technologies will be demonstrated but not fully integrated. Coherently with budget and time schedule constraints, GRA covers:• Green Impact (yes)• Integration and Flight Testing (limited)• Industrial Impact (very limited) • Industrial Competitiveness (very limited )

Regional AircraftFrom Clean Sky towards Clean Sky 2




4. LEADERS POCs


Setup and Implementation Structure of the Clean Sky 2 Program

The need to further address the environment (integrating maturedtechnologies, mainly from current CS GRA) as well as to matureother technologies necessary for a future regional a/c to besuccessful and make a real change towards the strategic objectivesset, has driven the need for a Regional Aircraft IADP and RegionalA/C activities in the ITDs of the Clean Sky 2 Proposal.

Setup and Implementation The Regional Aircraft IADP (R-IADP)

Major involvement of Core Partners

Setup and Implementation The R-IADP WBS

Total R-IADP net funding~104 M€

Setup and Implementation Management Approach – The Technological Waves

WV1 – ADAPTIVE WING (Liquid Infusion, Morphing, HLD, Winglets, NLF, Drag, High Lift…)

WV2 - REGIONAL AVIONICS (FMS, HMI, Health Monitoring…)

WV3 - COCKPIT (Advanced composite materials, systems, ….)

WV4 - INNOVATIVE FLIGHT CONTROL SYSTEM (Fly-by-Wire, EMA , …)

WV5 - ENERGY OPTIMIZED REGIONAL A/C (Low Power WIPS, Electrical Landing gears, EPGDS, E-ECS, ..)

WV6 - FUSELAGE STRUCTURE (Advanced composite materials, advanced manufacturing, ….)

WV7 - PAX CABIN (Human centered design, Materials,…)

WV8 - NACELLE FOR REGIONAL A/C (JET + TP) (Nacelle Materials, Ice protection, Drag Reduction…)

Setup and Implementation Management Approach – The Technological Waves

WP 3.1Air Vehicle FTB#1

(ALA + Others)

SYSTEMS ITD SYNERGIES

(ALA + Systems)

WP 2.4INNOVATIVE FCS

(ALA + Others) WV4

WP 3.5HL Advanced TP FTB#2 (EADS-CASA + Others)


(ALA + Others)


(ALA + Syst.)

WP 2.3 ENERGY OPTIM. A/C

(ALA + Others) WV5

WP 3.2FUSELAGE/CABIN DEMO

(ALA + Others) WP B-4.3 Airfr. ITDCOMPOSITE FUSELAGE

(ALA + Others)

WP B-4.4 Airfr. ITDHCD-LW-LC CABIN

(ALA + Others)

WP 3.2FUSELAGE/CABIN DEMO

(ALA + Others)

WP B-2.3Airfr. ITD NACELLES

(ALA + Others)

WP B-2.3, B-3.2 Airfr. ITD TP NACELLES(ALA + CASA + Others)


(ALA + Syst.)

WV6

WV7

WV8


WP B-3.3 Airfr. ITDGROUND WING DEMO (EADS-CASA + Others)


(ALA + Others)

SYSTEMS ITDSYNERGIES

(EADS-CASA + Syst.)

WP B-2.3 Airfr.ITDHigh Lift Wing

(EADS-CASA + Others)

WP 2.1 Adaptive Electric Wing

(ALA + Others) WV1

WP 3.3FLIGHT SIMULATOR

(ALA + Others)


(ALA + Systems)

WP 2.2 REGIONAL AVIONICS

(ALA + Others)

WV3 WP B-3.1 Airfr. ITDCOCKPIT GND DEMO (EADS-CASA + Others)

WP B-3.1 Airfr. ITD COCKPIT

(EADS-CASA + Others)

WP 3.4 IRON BIRD

(ALA + Others)

WV2


WP 2Technologies Development

WP 3Demonstrations


(EADS-CASA + Systems)


(ALA + Syst.)

Setup and Implementation The R-IADP Demonstrators (“Waves of Waves”)

CLEAN SKY 2

“REGIONAL”

Regional a/c IADP Airframe ITD Engines ITD A/C Syst&Eq. ITD

Flight Demonstration Ground Demonstration

NG HE Regional A/C

FTB1

Horizon 2020Flightpath2050

mid-term

ALENIA EADS-CASA

ALENIA

ALENIA

ALENIA

FP-7

FTB2

CMC Chairman

Programme Manager

FTB1Demo Leader

Waves

(ITD’s interfaces)

Roadmap

FTB2 WING COCKPIT Fuselage Flight Sim Iron Bird A/C CONFIG. DEMO RES.

Deliver’s

RA-IADP Steering Committe

(CSJU+ITD’s as permitted non-voting observers)

Programme Policy & Steering

15

Setup and Implementation R-IADP Organization

WV1 -WV2 -WV3 -WV4 -WV5 -WV6 -WV7 -WV8 -

CS2 “Regional” RBS

RISK MANAGER

Tech. Waves Deliverables RISKS OWNERS

Flying Demonstrators

RISK OWNERS

Ground Demonstrators

RISK OWNERS

Tech. Waves Deliverables RISKS OWNERS

CS2 “Regional” SC

RISKS STEERINGCS2 “Regional” Coordinator

OVERALL RISKS MGMT

FTB1

- WV1

- WV4- WV5

- WV8

A/C Config. Demonstrators

RISK OWNERS

16

Setup and Implementation R-IADP Risk Management Organization

FTB2

• The R-IADP is widely open to participation of Core Partners (long term participation, from technologies development up to development of complex end items for the demonstrators) and Partners (for specific projects with limited duration)

• Main expected Core Partners / Partners: EU supply chain of regional a/c manufactures

Systems Suppliers

Propeller Manufacturer(s)

Academia

Research Centers with complex test facilities

and other SMEs

In the following charts, this symbol is used to highlight the WPs where contributions from Core Partners is expected

CP

Setup and Implementation R-IADP A Widely Open Programme




4. LEADERS POCs


Hi-Level Technical ContentsWP1 – High Efficiency Regional Aircraft

WP 1

HIGH EFFICIENCY REGIONAL AIRCRAFT

WP 1.1

INNOVATIVE A/C CONFIGURATIONS

WP 1.2

TOP LEVEL A/C REQUIREMENTS

WP 1.3

TECHNOLOGIES REQUIREMENTS

More efficient powerplant

•Bleedless engine/aircraft integration

•High temperature nacelle composite structure

• Innovative low power ice protection

•Highly integrated nacelle and associatedsystems

•Thermal management and energyharvesting

Air Vehicle•Low drag and noise with morphing wing /winglet, hingeless devices

•Relaxed Stability to reduce trim drag•Gust effects Active Control

•Advanced Flight Controls •Low speed / short field performance optimized wing

Fuselage•Composite fuselage with SHM•All / More Electric Aircraft

•Thermal Management •Cabin Systems

•Scraps and EoL recyclingAdvanced Cockpit and Avionics•Optimized Hybrid Multifunctional CFRP cockpit structure with integrated systems

• New Cockpit Interaction Concepts and functionalities for pilot reduction workload

• Mission management in a global environment

Maintenance• Simplification of maintenance operations• Availability improvements

• Wireless centralized maintenance• Systems heath monitoring

WTT DEMONSTRATION OF A BREAKTHROUGH REGIONAL

AIRCRAFT CONFIGURATION

CP

Preliminary Timescale:

WT Model Available: Q2 2019

WT Tests….............: Q2 2020

WP 2

TECHNOLOGIES DEVELOPMENT

WP 2.1

ADAPTIVE ELECTRIC WING

WP 2.2

REGIONAL AVIONICS

WP 2.3

ENERGY OPTIMIZED REGIONAL AIRCRAFT

WP 2.4

INNOVATIVE FCS

The starting point for this WP will be the development of relevanttechnologies achieved in the current Clean Sky GRA ITD. Thesetechnologies will be further developed with the aim to achieve muchhigher integration and validation levels. Other technologies,including the ones from other EU projects and National Projects willbe considered as well.

Hi-Level Technical ContentsWP2 – Technologies Development

WP2 – Technologies Development (Preliminary Schedule)

I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV I II III IV

GRA Domains Outcomes:

Low Weight Configuration (LWC)Low Noise Configuration (LNC)All Electric Aircraft (AEA)Mission and Trajectory Management (MTM)

WP 2 - Technologies Development

WP 2.1 - Adaptative Electric Wing

WP 2.2 - Regional Avionics

WP 2.3 - Energy Optimized Regional Aircraft

WP 2.4 - Innovative Flight Control Systems

ECD = Estimated Completion Date

2018 2019

Activity

2014 2015 2016 2017 2020 2021 2022 2023 2024

LWC

LNC

MTM

AEA

AEA

LNC

Initial set oftechnologies for

the Flight Simulator

Technologies passing this gate will go to R-IADP WP 3.1 FTB1

TRL 4 GATE ECD

TRL 5 GATE ECD

Technologies passing this gate will be further developed and demonstrated in R-IADP WP 3.3 Flight Simulator

TRL 5 GATE ECD

TRL 4 GATES

ECD

Down-selection of technologies for ground / flight demos

Final selection of technologies for ground / flight demos

1st TRL 4 GATE ECD

Selected technologies passing this gate will go to R-IADP WP 3.1 FTB1 and to WP 3.2 Fuselage / Cabin Demo

Selected technologies passing this gate will go to R-IADP WP 3.2 Fuselage / Cabin Demo and to WP 3.4 Iron Bird

Technologies passing this gate will be further developed in R-IADP WP 3.4 Iron Bird and are candidate for Flight Test in WP

Down-selection of technologies for flight test

Final selection of technologies for flight test

2nd TRL 4 GATE ECD

Technologies passing this gate will be further developed and demonstrated in R-IADP WP 3.4 Iron Bird

Main objective of this WP is to furtherdevelop and mature the integration ofGRA wing technologies, featuringadvanced performances (highaerodynamic efficiency, load control &alleviation functions, low noise impact,low-weight).

Wing technologies for regional a/c willbe developed in the R-IADP as well as inthe Airframe ITD.

WP 2.1ADAPTIVE ELECTRIC

WING

WP 2.1.1Innovative Wing Structure

D&M

WP 2.1.2Morphing Structures

WP 2.1.3Advanced HLD

WP 2.1.4Load Control & Alleviation

WP 2.1.5Wing NLF

WP 2.1.6Drag Reduction

CP

CP

CP

CP

CP

CP

Hi-Level Technical ContentsWP2.1 – Adaptive Electric Wing

In this WP, starting from common solutions developed in Systems ITD, regional specificities (e.g. HMI, regional a/c constraints and capabilities) will be identified in order to customize them for New Generation Regional a/c.

WP 2.2REGIONAL AVIONICS

WP 2.2.1Avionic Functions

WP 2.2.2Innovative Flight Deck

WP 2.2.3Performance / Health

Monitoring

WP 2TECHNOLOGIES DEVELOPMENT

CP

CP

Hi-Level Technical ContentsWP2.2 – Regional Avionics

• Avionics Functions: FMS NG including

Green Functions and taking into account newATM constraints

• Innovative Flight Deck: Pilot interaction,

Data Fusion, Data format presentation

• Performance/Health Monitoring: architectures, integration in avionics, data collection, advanced model

The aim of this work package is to addresstechnologies related to innovative on-boards systems for regional a/c, mainlythrough synergies between the R-IADP andthe Systems ITD.

W.r.t. current Clean Sky, furtherdevelopment of the innovativetechnologies for aircraft systems will bepursued, so as to:• effectively improve the overall aircraft energy

efficiency, reducing the environmental impact• simplify the maintenance, reducing the

ownership costsWP 2.3.8

Other Novel Technologies

WP 2.3ENERGY OPTIMIZED REGIONAL AIRCRAFT

WP 2.3.1Low Power WIPS

WP 2.3.2Electrical Landing Gear

WP 2.3.3Thermal Management


WP 2.3.4Advanced EPGDS

WP 2.3.5Electrical ECS

WP 2.3.6Advanced Low Noise

Propeller

WP 2.3.7Ehnanced Fuel System &

Inerting

CP

CP

CP

High-Level Technical ContentsWP2.3 – Energy Optimized Regional Aircraft

Hi-Level Technical ContentsWP2.4 – Innovative Flight Control Systems

The high-level objective is to replace on Regional A/C all or part of the hydraulic systems that feed the FCS with lighter and simpler electrical systems offering unchanged reliability and performances, by means of:

WP 2.4INNOVATIVE FCS

WP 2.4.1Advanced Fly-by-Wire

WP 2.4.2EMA


CP

CP

• Advanced Fly-by-Wire:- Advanced and affordable flight control system architecture for regional A/C - Load control and Load Alleviation System (sensor, control laws and actuation for new

aerodynamic devices/conventional control surfaces actuated I also in unconventional ways)

• Electro-Mechanical Actuation: EMAs of different types will be investigated /

integrated

Hi-Level Technical ContentsWP3 – Demonstrations

WP 3

DEMONSTRATIONS

WP 3.1

AIR VEHICLE TECHNOLOGIES

FTB1

WP 3.2

FUSELAGE / CABIN INTEGRATED GROUND

DEMO

WP 3.3

FLIGHT SIMULATOR

WP 3.4

IRON BIRD

WP 3.5INTEGRATED TECHNOLOGIES

DEMONSTRATORFTB2

•To minimize technical and program risks, two Flying Test Beds are foreseen for demonstration campaigns of: Wing structure, aerodynamic and loads alleviation flight testing, Advanced Flight Controls and General Systems.

• Flight Simulator and Iron Bird Demonstrator are linked to FTB#1

• A full scale fuselage/pax cabin demonstrator will integrate technologies to be matured in the Airframe ITD WPs B-4.3 and B-4.4

ALENIA EADS-CASAALENIA ALENIA ALENIA

Objective of this demonstrator is the integration and flight-testing, focusing on high speed cruise and climb performance, of innovative technologies, mainly from GRA, for a new generation wing with advanced flight control systems as well as for innovative systems.

Hi-Level Technical ContentsWP3.1 – Air Vehicle Technologies Demonstrator (FTB1)

An existing aircraft will be modified to integrate advanced technologies in the following main areas:• Aerodynamics• Load Control and Load Alleviation• Aerolasticity (models validation)• Wing structure• Fligh Controls • Onboard Systems

WP 3.1Air Vehicle Technologies

Demonstrator (FTB1)

WP 3.1.1Demo A/C Mod’s Requirements

and Flight Test Requirements

WP 3.1.2Demo A/C Mod’s design and

manufacturing

WP 3.1.3Components / Equipment Design,

Manufacturing, Procurement

WP 3.1.4Demo A/C Integration, Ground

Testing and Permit to Fly

WP 3.1.5In-flight Demonstrations


Main Opportunity Areas for Participants:

•Demo aircraft, a/c modification and flight tests execution •Design and manufacturing of innovative wing structural parts•Design and manufacturing of equipment •WT Models design and manufacturing •3D WT testing/validation•3D IWT testing/validation•Engineering WPs for demo a/c modification design

CP


Demonstration Flight Tests: Q2 2021

Objective of this demonstrator is the integration and flight-testing, focusing on Low Speed and High Lift Performance, of innovative technologies, for a new generation wing with advanced high lift devices. Most of the technologies to be tested on FTB2 will come from other ITDs.


FTB2 will integrate and Flight Test Advanced technologies in the following main areas:• Composite wingbox structure, including

System integration• Adaptive winglet• More Electrical wing• High Lift devices

• Integrated Flight Controls including MLA/GLA


Main Opportunity Areas for Participants:

•Design and manufacturing of Wing CFRP structure• Wing systems integration • A/C integration•Engineering WPs for demo a/c modification design

CP


Demonstration Flight Test (1st campaign): Q1-Q2 2018

Demonstration Flight Test (2nd campaign): Q1-Q2 2020

Main objective is the integration and testing of a full scaleinnovative fuselage and passenger cabin including on boardsystems and advanced solutions for increasing passenger comfortand safety.

Structural demonstration: Long One Piece Fuselage Barrel, incomposite, integrating all feasible technologies andmethodologies developed within the Airframe ITD for regional a/c.

Pax Cabin demonstration: full scale equipped fuselage barrel(length tbd) for demonstration and validation of identified cabincomfort objectives as well as of innovative cabin/systemsintegrated solutions.

Hi-Level Technical ContentsWP3.2 – Fuselage/Cabin Integrated Demonstration

WP 3.2.1Demonstration Definition

WP 3.2.2Full Fuselage Design

WP 3.2.3Full Fuselage Manufacturing

and Assembly

WP 3DEMONSTRATIONS

WP 3.2.4Demonstration Preparation

WP 3.2.5Full Fuselage Demonstration

(Structural Tests )

WP 3.2.6Systems and Pax CabinIntegration (one barrel)

WP 3.2.7Pax Cabin Demonstration

(Systems, Thermal, ComfortTests )

WP 3.2FUSELAGE / CABIN

INTEGRATED DEMONSTRATION

WP3.2 – Fuselage/Cabin Integrated Demonstration (cont’d)

Opportunity Areas for Participants•Aeronautical Materials •Manufacturing and assembling tools•High-Automated Devices for manufacturing and assembly•Advanced Window Frames and Doors •Floor Design and Manufacturing•OOA Infused pressure bulkhead•Thermoplastic ATL Tailcone•Cabin Systems Items and support to testing •Ground Test Facility and Test Execution.

CP


Final Demonstration Tests: Q1-Q2 2021

WP3.3 – Flight Simulator

WP 3.3FLIGHT SIMULATOR

WP 3.3.1Regional Flight Simulator

Set-up

WP 3.3.2Technologies Customization

WP 3.3.3Technologies Integration

WP 3.3.4Demo Test Preparation and

execution

WP 3.3.5Reporting

Opportunity Areas for Participants• Flight simulator models• Equipment Prototypes (hardware /software).

CP


Demonstration Tests: Q1-Q2 2020

Starting from the Clean Sky GRA Flight Simulator, an advanced FlightSimulator will be set up and used to demonstrate new cockpitinteraction concepts as well as advanced avionics functionalities.

WP 3.4.1Iron Bird Definition

WP 3.4.2Iron Bird Design

WP 3.4.3Iron Bird Manufacturing and

Assembly

WP 3.4.4Integration of Equipment

and Software

WP 3.4.5Demo Test Preparation and

execution

WP 3.4IRON BIRD

WP 3.4.6Reporting

Main objectives of this WP are:• On ground full-scale demonstration, as essential step

towards the optimization and validation of Regional A/Cadvanced flight control system configuration andinteracting aircraft systems incorporating innovativetechnologies enabling the application of the All/MoreElectrical Regional Aircraft Concept such as the Electro-mechanical Actuation (for Flight Control and LandingGear), the Enhanced Electrical Power Distribution andPower/Load Management .

• Support the permit-to-fly process for FTB1

Hi-Level Technical ContentsWP3.4 – Iron Bird

Opportunity Areas for Participants

• FCS Equipment (hw/sw) and Models• Electrical Distribution Equipment (hw/sw) and

Models • Test Benches Items: hardware/software.

CP


Demo Tests: Q1-Q2 2020

Hi-Level Technical ContentsWP4 – Technologies Development & Demostration Results

WP 4

TECHNOLOGIES DEVELOPMENT &

DEMONSTRATION RESULTS

WP 4.1

TECHNOLGY ASSESSMENT

WP 4.2

ECODESIGN

Information flows for R-IADP Interfaces with TE and ECO Transverse activity




4. LEADERS POCs


Leaders PoCs

• Leader PoC:Marco Protti Vito Perrupato

Business Development & Research Business Development&Research – Advanced Research

Head of Advanced Research Head of Clean Sky 2 Project

Alenia Aermacchi Alenia Aermacchi

Corso Francia, 426 Viale dell’Aeronautica, s/n

10146 Turin (Italy) 80038 – Pomigliano d’Arco (Naples), Italy

Phone: +39.011.756.2871 Phone: +39.081.887.3116

E-mail: [email protected] E-mail: [email protected]

• Co-Leader PoC:Miguel Angel Llorca Sanz

Head of Clean Sky II

Airbus Military

Paseo de John Lennon, s/n

28906 Getafe-Madrid

Phone: +34.91.443.1418

E-mail: [email protected]

Documents

Innovation Takes Off - Camera di commercio, Torino Takes Off. Clean Sky 2 12 Maggio 2014, ... INNOVATIVE FLIGHT CONTROL SYSTEM ... (EADS CASA + Systems) SYSTEMS ITD SYNERGIES