Research

NEW Aero engine core Concepts

Project “NEW Aero engine core Concepts”, AIP5-CT-2006-030876 (FP6)
Duration 12/2006 – 06/2007
Brief Description
  1. Development of new core engine concepts
  2. Identification of technology routes to environmentally friendly and economic propulsion solutions
Partners MTU (De), Snecma (Fr), Volvo (Se), Rolls Royce Deutschland (De), AUTh (Gr), ASBL (Be), Cranfield Univ. (UK), DLR (De), EnginSoft (It), ONERA (Fr), Oxford Univ. (UK), Univ. Aachen (De), Univ. de Belfort-Montbéliard (Fr), Univ. Graz (Au), Univ. de Liège (Be), Univ. Stuttgart (De), Rolls Royce Plc (UK), AVIO (It), Turbomeca (Fr), Techspace Aero (Be), ARTTIC S.A.S. (Fr), Airbus France (Fr), Cambridge Univ. (UK), SDA (Fr), Chalmers Univ. (Se), Univ. Lausanne (Sw), Loughborough Univ. (UK), NTUA (Gr), Sulzer Metco (Sw), Univ. Firenze (It), Univ. Karlsruhe (De), Univ. Sussex (UK)
Contribution WP 6 ; Task 6.2.2 ; Principal Investigator

  1. Preliminary design of the PERM injection system
  2. Characterization of the two-phase-flow at elevated pressure conditions by LDA and PDPA techniques
Funding
as partner		 720 k€
On-line Reference http://www.newac.org/