Abstract: A propulsion device including an unducted upstream propeller and a counter-rotating and coaxial downstream propeller. At least one blade of the upstream propeller is configured to generate a corotating secondary vortex for acting upstream of the downstream propeller to destabilize a blade tip vortex of the same at least one blade.
Type:
Application
Filed:
April 13, 2012
Publication date:
May 15, 2014
Applicants:
CENTRE DE RECHERCHE EN AERONAUTIQUE ASBL-CENAERO, SNECMA
Inventors:
Clement Marcel, Maurice Dejeu, Sebastien Pascal, Jerome Talbotec, Michael Leborgne, Ingrid Irene, Catherine Lepot