Innovation Takes Off - NCP · PDF fileo Advanced load control architectures and function ......

Innovation Takes Off

Clean Sky 2 Information Day Large Passenger Aircraft - IADP

Michel Goulain /Jens König Airbus

Brussels / Belgium, 28th March 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 and large scale ground and flight demonstrators

provides the frame for well aligned objective driven R&T covering

development and maturation through numerical simulation, rig

demonstrators, wind tunnel testing, small and large scale test

under condition 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 HLFC- technologies

o CROR engine integration

o Innovative empenage 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, 28th March 2014

Setup and Implementation

rr

Platform 1 Advanced Engine and

Aircraft Configuration

Platform 2 Innovative Physical

Integration Cabin-System-

Structure

Platform 3 Next Gen. Electrical A/C

Systems, Cockpit

Systems & Avionics

„Mature and validate disruptive

technologies for next generation

Large Passenger Aircraft through

large scale integrated

demonstration“


LPA-IADP WBS


LPA-IADP WBS – “Platform 1”



Estimated Volume of Activities ~560M€

Next Gen. Electrical 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 dynamically scaled flight testing

WP 1.4 Hybrid laminar flow control large scale demonstration • HLFC large-scale specimen demonstrator in flight operation

• High speed demonstrator with hybrid laminar flow control wing

WP 1.5 Innovative Flight operations

WP 1.6 Demonstration of radical aircraft configurations


Advanced Engine and Aircraft Configurations WP1.1 CROR Engine Demonstrator FTD

• Validate of the principle performance of a full size integrated CROR pusher engine under operational conditions

• Demonstrate and validate a principle pylon concept and system integration, in particular addressing loads, vibration, and noise attenuation technologies in real size

• Demonstrate and validate the viability of assumptions for the chosen engine concept like power gearbox, pitch control, lubrication system, energy and thermal management, FADEC concept (NPE considered)

• Validate the selected propeller and blade design • Synthesize available data from Clean Sky with CROR demo-engine

flight test data, re-calibrate tools analysis and converge results to accomplish TRL 6

• Aerostructure manufacturers • Systems Developers • Research Establishments

• Q3 / 2014 – Q3 / 2020

• 192M€

Gross budget

Objectives

Potential partners

Timescales


Advanced Engine and Aircraft Configurations WP1.2 Advanced Engine Driven Fuselage

• Demonstrate an engine integration solution at a full CFRP fuselage rear end and pylon, including tail cone and APU and being fully compliant with certification rules

• Demonstrate the loads capability of the structural solution at full scale

• Development of test capabilities both physical at full scale and virtual for various purposes such as static, fatigue, vibrations, impact, system integration and operability

• Develop and demonstrate concepts for structural health monitoring

• Demonstrate repair-technologies

• Aero structure manufacturers

• Aircraft manufacturers

• Research Establishments

• Test facilities operators

• Q3 / 2014 – Q3 / 2020

• 80M€

Gross budget

Objectives

Potential partners

Timescales


Advanced Engine and Aircraft Configurations WP1.3 Validation of Dynamically Scaled Flight Testing

• Assessment of dynamically scaled flight testing for research and validation of new aircraft technologies and new aircraft configurations regarding fluid- and flight mechanics similarity

• Development of a complete suite of procedures for dynamically scaled flight testing

• Finalizing the development of flight test vehicle

• Development of the whole operational hardware required to operate the vehicle, such as: ground station, test range, data link


• Small/Medium Enterprises for Systems Development

• UAV Developers

• Test Range Operators

• Q1 / 2015 – Q1 / 2018

• 10,8M€

Gross budget

Objectives

Potential partners

Means & Enablers

Timescales


Advanced Engine and Aircraft Configurations WP1.4 HLFC Large Scale Demonstration

• Acquire operational experience with HLFC structure and

system-based on the simplified HLFC concept (HLFC fin in

long-term airline operation)

• First flight test experience with HLFC equipped wing

counting on experiences gathered from AFloNext HLFC

wing ground-based demonstrator and HLFC fin experience

in CS2

• Airlines, Aircraft manufacturers, Aircraft Suppliers,

Small/Medium Enterprises, Research Establishments

• HLFC for VTP: Q1 / 2015 – Q2 / 2019

• HLFC for wing: Q2 / 2017 – Q2 / 2023

• 142M€

Gross budget

Objectives

Potential partners

Timescales


Advanced Engine and Aircraft Configurations WP1.5 Innovative Flight Operations

• Formation of flight demonstration.

• Development and demonstration of new, environmental flight procedures enabled by next generation aircraft technologies. Example: develop and validate new take-off, climb and approach trajectories of a CROR-powered, laminar wing equipped next generation aircraft

•

• Dedicated flight tests to address specific operational issues required for an aircraft featuring NLF

• Dedicated flight tests to exploit next generation technologies like HLFC, flow separation control, etc.

• RE´s, Systems Developers, Air traffic Control Authorities

• Formation flight Q1 / 2015 – Q4 / 2020 (TRL6)

• Operational noise procedures Q1 / 2015 – Q4 / 2018

• NLF flight procedures Q1 / 2020 – Q2 / 2024

• 37M€

Gross budget

Objectives

Potential partners

Timescales

Means & Enablers


Advanced Engine and Aircraft Configurations WP1.6 Demonstration of Radical Aircraft Configurations

• To provide the demonstrator platform for a combination of best candidate technologies for a next generation large short and medium transport aircraft.

• The results of WP1.3 and the final choice of technologies to be integrated in the most promising aircraft architectures to be matured towards TRL 6 will define the demonstration and flight-test requirements. This includes in particular the option of a dynamically-scaled demonstrator.


• Small/Medium Enterprises for Systems Development

• UAV Developers

• Test Range Operators

• Q2 / 2018 – Q2 / 2024 (TRL6)

• 98M€

Gross budget

Objectives

Potential partners

Timescales








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, 28th March 2014 Estimated Volume of Activities ~290M€

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


• 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 CS2 LPA-IADP Info day, 28th March 2014

Innovative Physical Integration Cabin-System-Structure WP2.2.2 Technologies for elementary parts, sub-components and modules

Objectives

• Validation of structural integration concepts

• Innovative manufacturing processes

Enabling

• Rivetless assembly

• Automation

• Quality assurance

• Net shape manufacturing

• Topology optimisation - Bionic design

Potential partners


• 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




Setup and Implementation LPA Platform 3

Estimated Volume of Activities ~230M€




Large Passenger Aircraft Platform – integration topics TRL 4-6 Aircraft Level

Airbus with Thales, Liebherr,

SAFRAN and Partners

Platform 3 Next Gen. Electrical Aircraft A/C Systems, Cockpits & Avionics

WP 3.1 Enhanced flight operations and functions

WP 3.2 Avionic backbone technologies development and integration

WP 3.3 Integrated advanced system s and avionics demonstration

WP 3.4 Next generation cockpit ground demonstrator

WP 3.5 Next generation cockpit features flight demonstration

WP 3.6 “Pilot case” demonstrators

Cockpit of the future (Fenics)


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 Q3-2014 up to Q2-2020

• WP3.1 activities set the basis of platform 3 and are re-entry points for validating results from other WP3.x

Gross budget provisions

• 47 M€


WP 3.2 Avionic backbone technologies development & integration

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


• Quantified benefit at aircraft level (weight, cost…)

Potential partners



Timescales

• From Q1-2015 up to Q4-2019


• 24 M€


WP 3.3 Integrated advanced systems and avionics demonstration

Objectives

• Adapt demonstration platform with the outcome of WP3.1 and WP3.2

• Define and develop additional avionics technologies for implementation of advanced functions


• Feasibility + maturity assessment new standards

Potential partners



Timescales

• From Q1-2015 up to Q4-2019


• 12 M€


WP 3.4 Next generation cockpit ground demonstrator

Objectives

• Develop a highly representative cockpit “crew in the loop” simulator embedding all the novel functions

• Demonstrate enhanced flight operations in a realistic (simulated) environment

• Validate the proposed concepts and novel type of operations


• Overall functional integration

• Crew evaluation and buy-in

Potential partners



Timescales

• From Q3-2014 up to Q2-2020


• 75 M€


WP 3.5 Next generation cockpit features 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 Q3-2014 up to Q4-2019


• 70 M€


LPA-IADP High level technology roadmap

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 -

2 3 4 5 6

Contribute to TRL - Scale

1

6

6

5

n/a n/a 4

4

LPA-IADP high level provisional schedule

Platform 1

o CROR demo engine FTD

o Advanced engine integration driven fuselage

o Validation of dynamically scaled flight testing

o HLFC large scale demonstration

o Innovative flight operations

o Demonstration of radical aircraft

configurations

Platform 2

o Next gen. fuselage, cabin and systems

integrated demonstrator

o Next gen. cabin & cargo functional

demonstrator

o Next. Gen. Lower centre fuselage structural

demonstrator

Platform 3

o Integrated system and avionics

demonstration

o Next gen. Cockpit ground demonstrator

o Cockpit feature flight demonstrator

o Pilot case demonstrator

5 5 6

6 4

4

4

6

5

5 5 4

6

6

6 4 5 (6)

6 5 4 3

6 4 3 5

3 4 5 6

Case by case

3 4 5 6

3 6 5 4

Update and detailing to be made based on

„bottom-up planning, with Core Partners

3

4

4

6

5


LPA-IADP provisional first wave CP content


LPA-IADP High-Level Objectives

LPA prospected contribution to H2020 environmental targets

Advanced engine integration (incl. expected engine benefits) 15 - 20%

Laminar Flow technology 6 - 9%

Innovative flight operations 5 - 10%

Next generation integrated fuselage - Cabin & Cargo 5 - 10%

Next generation Cockpit, Navigation & Avionics 8 - 10%

Note: Targets vs. 2014 state of the art.

Targets cannot be expected to be fully cumulative when integrated at aircraft level


Further Information

Airbus PoC : Michel Goulain and Jens König

Please use:

[email protected]


Date post:	09-Mar-2018
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Innovation Takes Off - NCP · PDF fileo Advanced load control architectures and function ......

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