technology trajectory

 
 

A recollection of previous projects presenting synergies with AFLoNext research
are listed/ illustrated below .


It depicts the technological trajectories on which  AFLoNext Technology Streams are relying and the benefits driven from them in terms of use of the results and beyond the state-of-the-art knowledge.


Project acronym

Full title

Application field

Type

3AS

Active Aeroelastic Aircraft Structures

Smart aeroelastic structural response

FP5/ FP6

ACTUATION2015

Prognostics and Health and Usage Monitoring

Design of embedded computer hardware and software

FP7

ANNA

New materials for aircraft structure

Novel composite structures

National

APART

Advanced Powerplant and Aerodynamics Research Technology

Civil Wing Technology

UK National

ARTIMA

Aircraft Reliability Through Intelligent Materials Application

Structural health monitoring

FP6

AVERT

Aerodynamic Validation of Emission Reducing Technologies

Flow Control High-Lift & High Speed

FP6

AWAHL

Advanced Wing And High-Lift Design

High-lift devices for a next-generation wing on a regional aircraft context

CS JTI-SFWA

AWIATOR

Aircraft Wing with Advanced Technology Operation

Innovative wing and high-lift design means

FP5

BUFET’N Co

Boucle Fermée appliquee au tremblement 3D démonstration du contrôle

Flow/buffet control

ONERA internal project

CS-JTI-SFWA-FloCoSys

Clean Sky- Joint Technology Initiative-Smart Fixed Wing Aircraft- Efficient Flow Control Systems

Flow control on flap

FP7

DEAMAK

Design And Manufacture of Krueger Flaps

Design and manufacture of Krueger flaps

CS-JTI-SFWA

DESIREH

Design, Simulation and Flight Reynolds-Number Testing for Advanced High-Lift Solutions

Aerodynamics for high-lift

FP7

DT-FA-AFC

Development and Test of Fluidic Actuators for Active Flow Control

Fluidic Acuator Design

FP7

EUROLIFT I and II

European High-Lift Programme I and II

High-Lift design capabilties

FP5/6

EXTICE

EXTream ICing Environements

Icing

FP7

FRIENDCOPTER

Integration of technologies in support of a passenger end environmentally friendly helicopter

Smart structures on helicopters

FP6

HIGHER-LE

High Lift Enhanced Research – Leading Edge

HLFC

National

IMS & CPS

Material Synergies & Composite Processing Strategies

Carbon Fibre Reinforced Polymer (CFRC)

FP7

NACRE

Novel passenger aircraft configurations

Novel concepts of aircraft design

FP6

MOET

More Open Electrical Technologies

Electrical Systems

FP6

OPENAIR

Optimisation for low Environmental Noise impact AIRcraft

Low noise high-lift solutions

 FP7

SADE

Smart High Lift Devices for Next Generation Wings

Testing of morphing structures for high-lift devices

FP7

SARISTU

Smart Intelligent Aircraft Structures

Morphing structures, integrated sensing structures, self-healing structures

FP7

SAWoF

Smart Active Wing of the Future

Civil Wing Technology

UK National

SCARLETT

SCAlable and ReconfigurabLe elEctronics plaTforms and Tools

 Design of embedded computer hardware and software

FP7

CS-JTI-SFWA

SFWA-ITD Smart Fixed Wing Aircraft Integrated Technology Demonstrator

Flow & Loads Control, NLF

FP7

SILENCER

Significantly lower community exposure to aircraft noise

Low noise aircraft design

FP5

SimOD

Aircraft Simulation at off-design Conditions

Civil wing Design

UK National

SysTAvio

System- und Avionik-Technologien der nächsten Generation

OAD/Systems

National

TELFONA

Testing for Laminar Flow on New Aircraft

Laminar flow

FP6

TIMPAN

 Technologies to IMProve Airframe Noise

Low noise design and treatments

FP6

VER²SUS

Verifikation und Validierung eines vereinfachten Absaugsystems

HLFC verification and validation of a simplified suction system in a large scale wind tunnel test

National: DLR project embedded in HIGHER:LE compound project

HIGHER_LE


Hight Lift Enhanced Research - Leading Edge

HLFC: experimental demonstration of simplified suction concept, verification and validation of design methods (same as written at HIGHER)

National

ALTTA

Application of Hybrid Laminar Flow Technology on Transport Aircraft HLFC: concept of simplified suction developed FP4

MDX, HYLDA, LATEC

Hybrid Laminar Flow Demonstration on Aircraft
Feasibility of HLFC for transport aircraft proven