Control and Alleviation of Loads in Advanced Regional Turbo Fan Configurations
(CLAReT)
Date du début: 28 janv. 2012,
Date de fin: 27 sept. 2013
PROJET
TERMINÉ
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.
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Coordinateur
UNIVERSITY OF BRISTOL
€ 111 663,00- Julie Coombs
- TYNDALL AVENUE SENATE HOUSE BS8 1TH BRISTOL (United Kingdom)
Details
- 75% € 337 783,50
-
FP7-JTI
- Projet sur CORDIS platform
3 Participants partenaires
AIRCRAFT RESEARCH ASSOCIATION LIMITED
€ 113 187,00- Kieron Rentle
- MANTON LANE MK41 7PF BEDFORD (United Kingdom)
- Cherie Judge
- BROWNLOW HILL 765 FOUNDATION BUILDING L69 7ZX LIVERPOOL (United Kingdom)
Stirling Dynamics Ltd
€ 112 933,50- Simon Hancock
- REGENT STREET 26 CLIFTON BS8 4HG Bristol (United Kingdom)