Innovation Takes Off - Clean Sky (f) LPA InfoDay...From Clean Sky towards Clean Sky 2 CS1 Smart...

Innovation Takes Off

Innovation Takes Off

LPA – IADP AIRBUS

Brussels, 22nd of February 2017

Clean Sky 2 Information Day dedicated to the

6th Call for Proposal Partners (CfP06)

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 Info Day CfP06, Brussels 22/02/2017

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“



LPA-IADP Work Breakdown Structure

Overview of the LPA-CfP06 topics

Platform 1

Platform 3


Platform 2

7 topics / 6,4M€ ind. funding




Platform 1

Platform 3


Platform 2




Important for Partner-Applicants to note:

Cooperation between the GAP Partners and LPA members acting in

the „hosting“ work packages shall be done by means of an

Implementation Agreement (IA) for all CfP#06 topics.

The IA shall be used as published with the CfP#06 Call documents.


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





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 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 CfP06, Brussels 22/02/2017 Estimated Volume of Activities ~290M€



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 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)



Platform 1


7 Topics

Total funding

6,4 M€


Assignment of the LPA-CfP06 topics to the LPA-IADP WBS

LPA

01-29 LPA

01-30

LPA

01-33

LPA

01-35

LPA

01-34

LPA

01-31 LPA

01-32

JTI-CS2-2017-CFP06-LPA-01-29

Modelling of installed jet noise for UHBR engine

integration with forward flight effects

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

CFP06-LPA-1-13 ‘UHBR installed jet noise model’



• WP1.1.1.: JTI-CS2-2017-CFP06-LPA-1-13 (RIA activity)

• Title: Modelling of installed jet noise for UHBR engine integration with forward flight effects

Illustration of integrated propulsion system exhaust generating jet noise and jet-wing interaction noise.

• Objective: Build and validate a physics-based model of installed subsonic jet noise with forward flight effects for UHBR engine integration. The model shall have a short return time of the order of a few days. The effect of flight and the three-dimensional distortion of the jet flow under wing should be investigated and accounted for. Three work packages are envisaged:

– Eduction and modeling of « isolated » jet mixing noise sources (engine exhaust).

– Eduction and modeling of « installation noise » sources (engine exhaust + pylon + wing).

– Integration of isolated and installation noise components, and validation against experiments.

• Volume: 500k€ funding

UHBR = Ultra High Bypass Ratio



• Schedule: 48 months duration

Task Q1 Q2 Q3 Q4 Q5 Q6 Q7 Q8 Q9 Q10 Q11 Q12 Q13 Q14 Q15 Q16

WP1 Jet Mixing Noise modelling

WP1.1 Mixing noise source eduction from experiments

WP1.2 Mixing noise source and propagation modelling

WP2 Jet Installation Noise modelling

WP2.1 Installation noise source eduction from experiments

WP2.2 Installation noise source and propagation modelling

WP3 Total jet noise prediction and validation

WP3.1 Complete installed jet noise prediction model

WP3.2 Validation of prediction method against exp. measurements

Year 1 Year 2 Year 3 Year 4

• Targeted applicant: Partner with high skills in aeroacoustics of turbulent jets, flow and acoustic signal post-processing. Strong academic and research background shall be demonstrated.

• Required skills: – Capability to perform aeroacoustic analytical and semi-empirical modeling. – Knowledge of turbulent flows. – Capability to post-process aeroacoustic experimental data and extract noise source

characteristics. • Capabilities: Advanced experimental jet noise lab, with capability to capture the turbulence

dynamics in a turbulent jet for the frequency range of interest (for instance, time-resolved PIV) in a well-controlled aero-acoustic environment.

• Topic manager: Airbus • Intermediate and final versions of the model shall be made available to the topic manager during

the duration of CS2 LPA project, as model shall be used to predict installed jet noise of UHBR demonstrators.


JTI-CS2-2017-CFP06-LPA-01-30

Test Cell Control System for NPE Demonstrator


CfP06-LPA-01-30

CfP06-LPA-01-30

• JTI-CS2-2017-CfP06-LPA-01-30

• Title: Test Cell Control System for NPE Demonstrator

• Topic Manager: Safran Power Units

• Objective: The purpose is to develop an innovative test cell control system coupling real time models for main engines and hardware (Auxiliary Power Units, Starter generator, Generator, etc.). The objective is to demonstrate the ability of a new optimised Non Propulsive Energy (NPE) system to meet aircraft needs depending on Main Engine status and operating point. This system should be compatible with an existing APU test cell.

• Volume: 750 k€ funding

Power Management Unit

/

Power Dispatch Unit

Main Engine Model

(Real Time)

Main Engine Model

(Real Time)

Ke

y P

ara

me

ters

Main Engines Display

Panel

Requirements (Thrust,Electrical Power, …)

Pa

ram

ete

rs

Auxiliary Power Unit

(Gas Turbine, ECU,

Starter/Generator,

…)

Requirements (Start/Stop, …)

Electrical Loads

(Electrical Network)

Electrical Power

Key Parameters

APU Display Panel

Parameters

Kerosene

Air

Exhaust Gases

Pneumatic Circuit

(Bleed Network )

Pn

eu

ma

tic P

ow

er

Loads Display Panel

Parameters

Parameters

Aircraft Mission Profile

(Thrust + Non Propulsive Power)

Real APU Test Cell APU Control room + Full NPE System control and display

Key Parameters

Mission&Power

Management Display

Panel

Parameters

Re

qu

irem

en

ts (E

lectric

al a

nd

Pn

eu

ma

tica

l Po

we

r, …)


CfP06-LPA-01-30

• Proposed schedule

• Targeted applicant: Partner with industrial background in automatism, data acquisition systems, sensors, data exchange protocols. Special focus on real time software.

• Required skills: – Automatism, PLC technology

– Real time software architectures

– Data Acquisition System skills compatible with innovative sensors

– Innovative Engine sensors including signal treatment modules

– Aircraft network protocol communications CS2 Info Day CfP06, Brussels 22/02/2017

JTI-CS2-2016-CFP06-LPA-01-31

Representative HLFC leading edge structure –

torsion and bending stiffness test


CFP06-LPA-1-31


JTI-CS2-2016-CFP06-LPA-01-32

New acoustic signal processing methods


CFP06-LPA-1-32 ´Insect mitigation`


CS2 LPA-IADP Info day, 4th September 2014

The applicant shall have:

• Access to Wind/ice channel facility

• Availability of test equipment to investigate and assess insect impacts and coatings under realistic/representative A/C leading edge environment

• Skills and instruments for measurement of insect debris under simulated and realistic/ representative environment

• Substantiate technical knowledge in the domain of tasks, which is recognized in the scientific community and experience in project participation, international cooperation, project and quality management

CFP06-LPA-1-01 ´Insect mitigation`

Ref. No. Title – Description months

M1 Work plan agreed T0+2

M2 First Coatings for wind channel testing available T0+18

M3 Wind/ice tunnel tests completed T0+24

M4 Time plan and sample configuration for realistic environmental tests T0+24

M5 Coatings/surfaces for realistic environmental test available T0+24

M6 Realistic environmental tests completed T0+30

M7 Final report T0+36

Timeplan - milestones

Sample arrangement on wing leading edge

Required skills and expertise in field of:

• Experimental coating development and testing (coupon level)

• Performance of wind/ice channel test

• Performance of tests under realistic/representative aircraft leading edge environment

Microscopic analysis of debris

JTI-CS2-2017-CFP06-LPA-01-33

Innovative high temperature engine valve


JTI-CS2-2017-CFP06-LPA-01-33


JTI-CS2-2017-CFP06-LPA-01-06

• JTI-CS2-2017-CFP06-LPA-01-06

• Title: Multi-physics modelling of elementary physical phenomena applied to an innovative high temperature engine valve

• Objective: The design of valve, especially in engine environment (high temperature, high pressure, vibrations), requires high fidelity physical models to ensure performances and reduce risks of integration. The project proposal covers advances on multi-physics modelling of valve taking into account high temperature environment and high pressure flow: effects on mechanical frictions, aerodynamic torque, mechanics behaviour of dynamic seal for example. The physical models will be validated using test rigs results.


• Type of action: IA


JTI-CS2-2017-CFP06-LPA-01-06

• Schedule

& deliverables

Deliverables

Ref. No. Title - Description Type* Due Date

D1.1.1 Friction Coefficient - Test Bench HW T0+6

ID1.1.2 Friction Coefficient - Intermediate Experimental Study Report R T0+12

D1.1.2 Friction Coefficient - Experimental Study Report R T0+18

D1.1.3 Friction Coefficient - Experimental Database D T0+18

D1.2.1 Piston Sealing Ring Mechanism - Test Bench HW T0+12

ID1.2.2 Piston Sealing Ring Mechanism - Intermediate Experimental Study

Report

R T0+18

D1.2.2 Piston Sealing Ring Mechanism - Experimental Study Report R T0+30

D1.2.3 Piston Sealing Ring Mechanism – Friction Effort Model Report R T0+36

D1.3.1 Piston Sealing Ring Mechanism - Numerical Study Report R T0+36

D1.4.1 Butterfly Sealing Ring Mechanism - Test Bench HW T0+18

ID1.4.2 Butterfly Sealing Ring Mechanism - Intermediate Experimental

Study Report

R T0+24

D1.4.2 Butterfly Sealing Ring Mechanism - Experimental Study Report R T0+36

D1.4.3 Butterfly Sealing Ring Mechanism – Friction Effort Model Report R T0+36

D1.5.1 Diaphragm Material Experimental Study R T0+38

D1.5.2 Diaphragm Mechanical Properties - Experimental Study R T0+46

D1.5.3 Diaphragm Mechanical Properties - Experimental Study R T0+48

D2.1.1 Butterfly Sealing Ring Aerodynamic Properties - Test Bench HW T0+38

D2.1.2 Butterfly Sealing Ring Aerodynamic Properties - Experimental

Study Report

R T0+48


JTI-CS2-2017-CFP06-LPA-01-06

• Targeted applicant: Partner(s) with research background, thermo-mechanical & fluid mechanicals modelling knowledge and test benches set up capabilities

• Required skills:

Skills:

Mechanical Contact (Friction) applied to pneumatic products related with high temperature

- Experimental background to set-up a friction test bench

- Theoretical background regarding friction simulation

Thermo-Mechanics for temperature effects on diaphragm

- Theoretical and Numerical background to simulate such effects

Fluid Mechanics for aerodynamic torque study

- Experimental background to set-up an aerodynamic torque test bench

Capabilities:

Air Generation for test benches

Temperature / Pressure environmental control


JTI-CS2-2017-CFP06-LPA-01-34

3D-printing and harsh environment testing of flow

control actuators at aircraft scale


CFP06-LPA-01-034


CFP06-LPA-01-034

• JTI-CS2-2016-CFP06-LPA-01-034

• Title: 3D printing and harsh environment testing of flow control actuators at aircraft scale.

• Company managing the topic: Airbus Operations

• Objective: Manufacturing flow control actuators at aircraft scale using 3D printing method and expose them to harsh environment (HE) testing. Using the outcome of the first set of HE tests, an optimization loop for the actuators design will be performed followed by a second test at harsh environment conditions.


Example of a Flow Control Actuator


100mm Conditions for the harsh environmental tests: • Rain • Ice • Sand and Dust • Vibrations • Anti-icing fluid

• Schedule

• Targeted applicant: Partner with research background and a sound experience and capability in 3D printing (ALM

manufacturing), in aerodynamic and harsh environmental testing of flow control components and in design techniques applied for 3D printed components.

• Required skills: • Profound knowledge in 3D printing in titanium and other materials able to sustain thermal loads. • Proving a stable and repeatable 3D printing process. • The applicant must give proof of having profound knowledge of design techniques to be applied for 3D printed

components including optimization w.r.t. strength and weight. • The applicant shall have knowledge in aerodynamic and harsh environmental testing of flow control

components. • Experience in aerospace R&T and R&D programs

Duration 18 months

Start Q1/2018

Tasks

Ref. No. Title – Description Due Date

T1 Adaption of the design of flow control actuators and

infrastructure to 3D printing manufacturing principles. M2

T2 3D printing of flow control components (original design) M6

T3 Aerodynamic and harsh environment testing of flow control

components. M10

T4 Analysis of aerodynamic and harsh environment tests M11

T5 Definition of improved design and 3D printing of improved

flow control components M15

T6 Aerodynamic and harsh environment testing of improved

flow control components M17

T7 Analysis of aerodynamic and harsh environment testing of

improved flow control components M18

CS2 Info Day CfP06,

Brussels 22/02/2017 CS2 Info Day CfP06, Brussels 22/02/2017

CFP06-LPA-01-034

JTI-CS2-2017-CFP06-LPA-01-35

Innovative compact heat exchangers modelisations and characterization


JTI-CS2-2017-CFP06-LPA-01-35


JTI-CS2-2017-CFP06-LPA-01-35

• JTI-CS2-2017-CFP06-LPA-01-05

• Title: Innovative compact heat exchangers modelling & characterization

• Objective: The objective of this topic is to propose new fins and overall structures predictive models or laws (thermal and pressure drop) to be used for complex compact heat exchanger design including the one obtained by additive manufacturing. Characterization and experimental validation on samples and manufacturing of functional demonstrators will be required (aluminum alloy and nickel alloy).


• Type of action: RIA


JTI-CS2-2017-CFP06-LPA-01-35

• Schedule & deliverables

Deliverables


1 Bibliography Report R T0+6

2 Fins / Structure Design Report R T0+24

3 Test Campaign and Analysis at fins / elementary

structure scale

R+D T0+30

4 CHX Design Report R T0+40

5 Test Campaign and Analysis at CHX scale R+D T0+48

6 CHX + elementary fins specimen HW T0+48

Milestones (when appropriate)


1 Fins / Structure Design Intermediate Milestone R T0+12

2 CHX Design Intermediate Milestone R T0+35


JTI-CS2-2017-CFP06-LPA-01-35

• Targeted applicant: Partner(s) with research background and with experience in design and manufacturing exchangers


Skills:

Thermodynamics applied to Compact Heat eXchanger (CHX)

CHX design

CHX manufacturing knowledge

Additive Manufacturing knowledge

CFD & Finite element stress computations

Capabilities:

Computing facilities in order to be able to predict news shapes of fins’ / structure performances

Additive Manufacturing machines to manufacture elementary heat exchanger elements and full size heat exchanger (size 400 mm*200 mm*1300 mm) with Aluminum and Nickel alloy powders

Testing facilities in order to be able to characterized news shapes of fins / structure with air (temperature range: -15°C/+300°C , flow range: 0.01kg/s; 0.5kg/s) and full size heat exchangers with air (temperature range: -55°C/+600°C , flow range: 0.01kg/s; 3kg/s)




Platform 2

6 Topics

Total funding

4,88 M€


Assignment of CfP06-topics to the LPA-IADP WBS

LPA

02-16

LPA

02-17 LPA

02-18

LPA

02-19 LPA

02-20

LPA

02-21

JTI-CS2-2017-CFP06-LPA-02-16

Smart Container


CfP06-LPA-02-16 ‘SmartContainer’



• JTI-CS2-2017-CFP06-LPA-02-16

• Title: SmartContainer

• Volume: 2 Mio€ (funding)



• Schedule

• Targeted applicant: Partner (partner consortium) with capabilities in the definition, development,

manufacturing, testing and certification of an innovative A/C cargo container with all described functions.

• Required skills: The applicant shall have an aerospace industry background, experiences and

capabilities in all described functions of the cargo container.

Dilverables are described in the call


JTI-CS2-2017-CFP06-LPA-02-17

Glass fiber based temperature/air humidity and

Agent detection sensors & measurement systems


CfP06-LPA-02-17 Glass fiber based temperature/air humidity and Agent detection sensors & measurement systems


WP 2.2 Next Generation Cabin & Cargo

Functions

WP 2.2.1 Cabin Reconfiguration Enablers

WP 2.2.2 Cabin & Cargo Integration &

Materials

WP 2.2.3 Electrical & Mechanical Systems

WP 2.2.4 Infotainment & Operations

WP 2.2.5 Industrialization

WP 2.2.6 Integration and Testing


• JTI-CS2-2017-CfP06-LPA-02-17

• Title: Glass fiber based temperature/air humidity and Agent detection sensors & measurement systems

• Objective: This task will cover the development of a glass fibre based sensor system that shall equip the cargo hold of a A310 demonstrator in order to measure temperatures and humidity with a high resolution and quick timely response. The system shall be capable of measuring air and surface temperatures.

• The system shall be amended with a agent detection system to validate the distribution of fire knock-down agents.

To be equipped with sensor system for agent distribution validation



• Schedule

• Targeted applicant: partner with research background in glass fiber based sensor systems. Competencies in agent detection systems design are an advantage.

• Required skills: – Design of glass fiber based sensor systems for precise and quick measurement

– Adaptation and optimization of agent detection sensors for different gases

– Test system integration capability with other measurement and control systems

– Sensor distribution and attachment to assure proper decoupled measurements (temperature / humidity / physical stress)

Deliverable Month

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27

D1 Requirement and interface

specification

D2 Requirement Review

M1

D3 HW and SW description

D4 Critical Design Review

M2

D5 Validated prototype HW of the

demonstrator System M3

D6 Integrated HW on FTF

M4

D7 Documentation of installed HW/SW

for the demonstrator

M

5

D8 Delivery of final documentation

M

6


JTI-CS2-2017-CFP06-LPA-02-18

Multi-Physics methodology for phase change due

to rapidly depressurized two-phase flows


CfP06-LPA-02-18 Multi-Physics methodology for phase change due to rapidly depressurized two-phase flows


WP 2.2 Next Generation Cabin & Cargo

Functions

WP 2.2.1 Cabin Reconfiguration Enablers

WP 2.2.2 Cabin & Cargo Integration &

Materials

WP 2.2.3 Electrical & Mechanical Systems

WP 2.2.4 Infotainment & Operations

WP 2.2.5 Industrialization

WP 2.2.6 Integration and Testing


• JTI-CS2-2017-CfP06-LPA-02-18

• Title: Multi-Physics methodology for phase change due to rapidly depressurized two-phase flows

• Objective: This task will cover the development of an extended CFD approach for the simulation of jets with a two phase agent. The sudden evaporation the liquid parts of a 2 phase agent has a significant influence of the total jet behaviour. In order to create generic zonal jet models the behaviour of such complex shall be simulated, parametrized and validated.

• Contribution for the validation concept on small and large demonstrator scales is required.

Environment to be simulated, red arrows indicated possible loactions of jets, several load configurations shall be simulated



• Schedule

• Targeted applicant: Experienced CFD specialist with detailed knowledge about multi-physics methodologies and validation concepts and methodologies.


– development of user-defined functions coupled to CFD

– means to perform a review of existing two-phase and phase change models and to implement most suited models into a user-defined function.Test system integration capability with other measurement and control systems

– The applicant shall have a profound understanding of energy, enthalpy and mass flows during phase change.

Deliverable Month

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

D1 Two-phase and phase change models

review and requirements coverage report M1

D2 Two-phase and phase change model V1 M2

D3 Toolchain V1 to couple CFD and two-phase

and phase change model M3

D4 Parametric study on two-phase and phase

change

D5 Documentation of model and model usage

D6 Toolchain V2 to couple CFD and two-phase

and phase change model

D7 Dissemination Report M4


JTI-CS2-2016-CFP06-LPA-02-19

High performance landing gear fitting


CfP06-LPA-02-06 ‘HPLGF’

58


• JTI-CS2-2017-CFP06-LPA-02-06 – Type of action: IA

• LPA member hosting the topic : AIRBUS

• Title: High performance landing gear fitting (‚HPLGF‘)

• Objectives:

1. To develop a manufacturing method for a large landing

gear fitting of high strength and low cost.

2. Reduced distortions due to internal stresses with design-

to-forge strategies.

3. Reduce the buy to fly ratio with optimised geometry, new

generation alloys, or other proposals from the supplier.


59

WP 2 Platform 2 „Innovative Physical

Integration Cabin – System – Strucure“

WP 2.3 Next Generation Lower Center Fuselage

WP 2.3.1 High performance LCF components

WP 2.3.1.1 Landing gear large die-forged fitting


60

• Schedule/Tasks (expected start on Q1 2018)


61

• Targeted applicant:

– High capacity Press to forge large part

– High capacity Press to conduct cold compression

– Software to conduct the numerical simulation of the forging and thermal treatment (to identify the residual stresses)


– Knowledge of aeronautical environment

– Recognized skills in forging large aluminium parts

– Recognized experience in forging coupons of different alloys

– Recognized experience in manufacturing parts for aeronautic

– Experience with numerical simulation to identify the shape of the blank as close as possible to the final part shape

– Availability of experienced staff in numerical simulation and manufacturing route definition

– Recognized skills in Materials and Processes

JTI-CS2-2017-CFP06-LPA-02-20

Keel beam manufacturing oriented solution


CfP06-LPA-02-05 ‘KBMOS’

63


• JTI-CS2-2017-CFP06-LPA-02-05 – Type of action: IA

• LPA member hosting the topic : AIRBUS

• Title: Keal beam manufacturing oriented solution (‚KBMOS‘)

• Objectives:

1. Develop a high performance keel beam in order to sustain

high static compression loading

2. Reduce the manufacturing costs compared to actual

composite technologies and be ideally comparative to

metal ones.

3. Propose manufacturing and assembly processes enable a

production rate over 70 aircrafts a month, with a good

robustness, aiming at a very high ramp-up (Full production

rate in 4 years).


64

Keel beam location

WP 2 Platform 2 „Innovative

Physical Integration Cabin – System – Strucure“

WP 2.3 Next Generation Lower

Center Fuselage

WP 2.3.1 High performance LCF

components

WP 2.3.1.2 High efficient Keel Beam

A320 metallic Keel beam


65

• Schedule/Deliverables (expected start Q1 / 2018)

• Targeted applicant:

– CAD Software : CATIA – Numerical simulation Software – Manufacturing facilities and equipment

• Required skills: – Knowledge of aeronautical environment – Recognized skills in aircraft component Design – Recognized skills in aircraft component Static Stress – Recognized experience in development of Aircraft composite parts – Recognized knowledge and experience in Manufacturing and Assembly of composite parts

JTI-CS2-2017-CFP06-LPA-02-21

Development of Systems for

Automated Testing in the Aircraft Interior


CfP06-LPA-02-21 ‘Development of Systems for Automated Testing in the Aircraft Interior ’



• JTI-CS2-2017-CFP06-LPA-02-21

• Title: Development of Systems for Automated Testing in the Aircraft Interior (

• Objective: The main objective is to develop a system for automated testing on the base of an already available mobile system for cabin and cargo assembly. The tests to be performed are the gap and flush management of installed components including lining and hatracks and the quality of the aircraft interior such as textures, defects and colour.


• Type of Action: IA

• Duration: 30 months

• Start Date: Q1-2018

• Topic Manager: Fraunhofer IFAM

• Agreement: Implementation

Platform 2 Innovative Physical Integration Cabin-System-Structure

WP 2.4 Non specific cross functions & ITD Airframe

WP 2.4.4 Future Factory

WP 2.4.4.2 Automated Cabin & Cargo Lining and Hatrack installation method


• Targeted applicant: partner with experiences in different disciplines of automated measurement systems. Main focus should be in the field of aircraft production and assembly including all main aspects of a production system.


– Experience in future aircraft interior development and cabin and cargo architecture

– Experience in varied range of 3D scanning systems used within aircraft industry

– Knowledge in spectral colour analysis and aircraft colour and trim experience

– Experience in development of software for data management and IT integration

– Ability to replicate the aircraft environment with regards to actual tolerance





Platform 3

4 Topics

Total funding

4,2 M€


Assignment of CfP06-topics to the LPA-IADP WBS

LPA

03-09 LPA

03-10 LPA

03-11

LPA

03-12

JTI-CS2-2017-CFP06-LPA-03-09

Image based landing solutions for a disruptive

cockpit concept


CFP06-LPA-03-09 Image Based Landing


• Goal: Extend the aircraft automatic landing capability by developing a computer vision function:

– Algorithms for runway acquisition & tracking (Concept proven in Airbus simulation) – Computer vision platform to host multiple image based functions (time & safety critical)

• Target: Disruptive Cockpit concept TRL5 in 2021, and then flying prototype

• The Applicant should be able to offer: 1- Image based landing Algorithm - runway acquisition & tracking, inputs AP aircraft guidance for Autoland - ILS « lookalike » operations.

- On non-equipped airfields

- CATIII like performances in CATI visibility conditions.

2- Computer vision platform - Modular concept to host multiple Computer Vision functions - Proof of concept for Time critical and Safety critical functions - Full specification of API and hardware for third party algorithm developpment - Flying Prototype Note: Sensor definition is outside CfP scope.



• The applicant offer should be able to provide – Expertise in real time computer vision development: hardware and software – Platform prototype ready for flight exposure in 2021 – Image sensors are not part of the call but Bidder may suggest potential

solutions

• Skills & Capabilities expected from the Applicant Knowledge and experience in development, integration and certification of : - Image based systems for the aerospace industry - Image processing algorithm for civil or military aircraft environments - Object identification and tracking algorithms - Time critical and safety critical modular avionics Knowledge of aircraft operation at approach and landing, certification constraints (JAR AWO) and current landing technologies Experience in image sensors characterization for civil or military aircraft environments, including at least visible and infrared frequency ranges. Working prototypes (even at low maturity level) demonstrated of one or several building blocks of the targeted system.




2018 2019 2020 2021

Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4

System

Design

Project Plan

Definition

Requirement

Definition

V&V Plan

Definition

System Definition

Final Report

Planning &

WBS

System requirement compilation

V&V

System Validation

System Verification

System Design

System

Verification

Documentation

Project Plan FR SRD V&V Plan PDR System Definition Document

DR TRL5 TTR

V&V

Report


Project Schedule

JTI-CS2-2017-CFP06-LPA-03-10

Avionics technologies management solution for

pilot workload reduction


CFP06-LPA-03-10 Pilot Workload Reduction


JTI-CS2-2016-CFP06-LPA-03-10 Innovation Action Airbus Defence and Space SAU

LPA IADP. Platform 3

“Next generation Aircraft, Cockpits Systems & Avionics”

WP 3.1

Enhanced Flight Operations and Functions (AIRBUS)

WP 3.1.2 Functions for easier flight and efficient and easy systems

management for regional aircraft (AIRBUS DEFENCE AND SPACE)

• Title: "Avionics Technologies Management solution for Pilot Workload Reduction “

• Volume: 1400 k€ indicative funding

• Start Date : Q1 2018, duration 36 months

• Objective: The aim of this topic is to enhance the technologies that contribute to alleviate the Pilots in their ground and flight tasks, by using a combination of image recognition sensors (EO/IR), A/C sensors and equipment to develop tracking and command algorithms hosted on a dedicated computing platform.

• The successful applicant is expected to sign an Implementation Agreement



Scope of work The topic addresses three main streams T-1 Visual Recognition and Automatic Command for Takeoff, Approach and Airport Navigation. Visual recognition and automatic command system through visible and infra-red light spectrum EVS (EO/IR device) to provide redundancy to execute the take-off, final approach and airport navigation operations to supplement the guidance provided by the standard approach and airport navigation systems

T-2 Automatic Avoidance Maneuvers Automatic aircraft response to the Terrain Awareness and Warning System (TAWS) and Weather Radar (WXR) warnings to avoid collision with other aircrafts, with the terrain or to enter into dangerous weather threats respectively or in combination of them. The system will have to host the appropriate HW/SW to acquire the avionics parameter from the above systems, and the processing algorithms needed to determine the right command to perform the appropriate aircraft maneuvers to avoid collisions.

T-3 Avionics Technologies Host System Affordable and flexible housing hardware and base software system prototype to host and manage the interfaces of the functions developed



• Targeted applicant: partner with a background in research and proven track record in development of aeronautical systems, both HW and SW.

• Required skills by the applicant:

• Experience in aeronautical interfaces (ARINC429, ARINC629, MIL-STD-1553, AFDX)

• Experience in ARINC 653 / Integrated Modular Avionics (IMA)

• Experience in EO/IR systems, Flight Control Systems, and Surveillance Systems

• Experience in Systems Simulation and Stimulation and test rig environments

• Experience in Equipment qualification with EASA/FAA authorities

Tasks

Ref. No. Title – Description Due Date

Task 1 Project Development Plan T0+4

Task 2 Definition of requirements T0+7

Task 3 Validation & verification plan T0+16

Task 4

System Concept definition

a) State of the art and review of available technologies.

b) Trade Off and selection of potential solution

T0+20

Task 5

System Validation and Verification –Building of prototypes, system and

associated test rig for V&V

The expected maturity level for the final prototype is TRL5.

T0+34

Task 6 Final Report T0+36

Schedule & Tasks



JTI-CS2-2017-CFP06-LPA-03-11

Multimodal HMI development tools


JTI-CS2-2017-CFP06-LPA-03-11


JTI-CS2-2017-CFP06-LPA-03-12

High density electrical connectors


CFP06-LPA-03-12 ‘High density electrical connectors’



• JTI-CS2-2017-CFP06-LPA-03-12

• Title: High Density Electrical Connectors

• Type of action: IA

• Objective: Definition of a new type of connectors addressing Modular, low cost and high density connection for avionics application. These new connectors will be designed, manufactured and tested onto a Remote Data Power Cabined studied in the frame of the Platform 3 of LPA IADP. The applicant will benefit of this topic to prepare a future standard of connectors.

• Start Date: 01-2018

• Duration of the action: 24 months


• Topic Manager: Zodiac Aerotechnics



• Schedule

• Targeted applicant: industrial partner(s) with strong background and expertise as a provider of connectors and complete connection solutions for the A/C industry.

• Required skills by the applicant:

– Strong knowledge of environmental constraints applicable to Aircraft systems, in particular those related to electro-magnetic effects. Strong knowledge on electrical, wiring and installation aspects of aircraft systems.

– Innovation driven. Internal Research & Technology roadmap to be provided.

– Background and expertise on product standardization.


Questions?

Any questions on the 6th Call for Proposals can be addressed to the following mailbox:

[email protected]

Last deadline to submit questions – check CS2 website

Thank you !


mailto:[email protected]









Thank You

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