par Outirba, Bilal 
;Hendrick, Patrick ;Nicolas, Kevin C.
Référence Aeronautical Journal, 121, 1245, page (1627-1647)
Publication Publié, 2017-11
;Hendrick, Patrick ;Nicolas, Kevin C.Référence Aeronautical Journal, 121, 1245, page (1627-1647)
Publication Publié, 2017-11
Article révisé par les pairs
| Résumé : | Over the last decades, it has been progressively acknowledged that reducing the specific fuel consumption and the emission of pollutants, as well as improving the thrust-To-weight ratio involves extensive research on advanced sealing technologies. Amongst these, brush seals are particularly well considered for their excellent leakage performance, their low friction properties, and their ability to cope with inevitable rotor excursions during flights. This paper presents the experimental work that has been carried on in order to characterise carbon fibre brush seals leakage rate in function of the bristle pack geometry, under different pressure loads and rotational speeds. The analysed parameters are the bristle-free length, the density and the inter-plate distance. The work, performed by the ULB (Université Libre de Bruxelles) in collaboration with French engine manufacturer Safran Aircraft Engines, highlights specific behaviour of carbon fibre brush seals under differential pressure, proposes a leakage prediction model developed through empirical equations, and discusses over the most influential parameters that influence the air consumption of a brush seal. |
