ELUBSYS

	ELUBSYS
	Home Home Partners Techspace Aero MTU Aero Engines Rolls-Royce plc Rolls-Royce Deutschland SNECMA Turbomeca Industria de Turbo Propulsores S.A WSK "PZL - Rzeszow" S.A. ARTTIC SAS Centre de Recherche en Aéronautique Tekniker Université Libre de Bruxelles Frederick Institute of Technology Institut National des Sciences Appliquées de Lyon University of Bordeaux Universität Karlsruhe University of Nottingham University of Sheffield Université de Mons WP Descriptions WP1 Adv. Brush Seals for Bearing Chambers WP2 Bearing Chamber Flow & Heat Transfer WP3 Externals WP4 Oil Quality & Coking WP5 Scientific Coordination & Benefit Evaluation WP6 Dissemination & Exploitation Dissemination
	Available Documents The impact of flow inlet conditions on the two phase flow pattern and the heat transfer in a scavenge pipe of an Aero Engine bearing chamber sealed with brush seals_FIT_MTU Oil Systems for Next Generation Engines-ELUBSYS Project Mid Term Achievements, Aerodays Conference 2011
	Objectives Results Evaluation Exploitation