CLARET
Control and Alleviation of Loads in Advanced Regional Turbo Fan Configurations
| Coordinatore | UNIVERSITY OF BRISTOL
Organization address
address: TYNDALL AVENUE SENATE HOUSE contact info |
| Nazionalità Coordinatore | United Kingdom [UK] |
| Totale costo | 450˙379 € |
| EC contributo | 337˙783 € |
| Programma | FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives |
| Code Call | SP1-JTI-CS-2010-05 |
| Funding Scheme | JTI-CS |
| Anno di inizio | 2012 |
| Periodo (anno-mese-giorno) | 2012-01-28 - 2013-09-27 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
UNIVERSITY OF BRISTOL
Organization address
address: TYNDALL AVENUE SENATE HOUSE contact info |
UK (BRISTOL) | coordinator | 111˙663.00 |
| 2 |
AIRCRAFT RESEARCH ASSOCIATION LIMITED
Organization address
address: Manton Lane contact info |
UK (BEDFORD) | participant | 113˙187.00 |
| 3 |
Stirling Dynamics Ltd
Organization address
address: REGENT STREET 26 CLIFTON contact info |
UK (Bristol) | participant | 112˙933.50 |
| 4 |
THE UNIVERSITY OF LIVERPOOL
Organization address
address: Brownlow Hill, Foundation Building 765 contact info |
UK (LIVERPOOL) | participant | 0.00 |
Mappa
Word cloud
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
Obiettivo del progetto (Objective)
'A novel adaptive winglet concept will be developed to enable controlled cant angle orientation and twist throughout the flight envelope whilst also providing a passive gust loads alleviation capability. A CFD based aerodynamic design of the device applied on a baseline Turbo-Fan Aircraft configuration model will be undertaken, followed by a preliminary lay-out definition of the structure and actuation system required for the device. Detailed parametric studies will then be performed to investigate the performance of the device in terms of both drag and loads alleviation capabilities on its own, and also in combination with conventional control actuators, and both compared to the baseline configuration.'
Introduzione (Teaser)
Despite major advances in engine design, aircraft configurations have remained relatively the same over the last 50 years. Now, a novel morphing wing concept has demonstrated potential to reduce drag and thus fuel consumption and emissions.