The engine 3E core engine

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2008, Pages 93-102

  Klinger, Holger ^a   Lazik, Waldemar ^a   Wunderlich, Thomas ^a  

^a ROLLS ROYCE DEUTSCHLAND LTD AND CO KG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERO ENGINE PARTS; AERONAUTICS RESEARCH; ALTITUDE TEST FACILITY; CORE ENGINES; ENVIRONMENTAL FRIENDLINESS; FIRST QUARTER; FUEL STAGING; KEY TECHNOLOGIES; LEAN-BURN COMBUSTION; LOW NOX; MANUFACTURING COST; ROLLS-ROYCE; SHAFT ENGINES; SPECIFIC POWER; TECHNOLOGY DEMONSTRATORS; UNIT COST;

COMBUSTION; COMBUSTION CHAMBERS; MINING; STAGES; TEST FACILITIES;

ENGINES;

EID: 69949160843     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-50679     Document Type: Conference Paper

References (5)

1. Klinger, H., 2004, "Das Engine 3E Kerntriebwerk von Rolls-Royce Deutschland", Proceedings of the German Aerospace Congress, Dresden, DGLR-2004-178
2. Gümmer, V., Digele, R., Gietl, T., 2007, "Aerodynamic Technology Integration on the TP400 and E3E Core Compressors", CEAS European Air and Space Conference, Berlin
3. Lazik, W., Dorr, T., Bake, S., 2007, "Low NOx Combustor Development for the Engine 3E Core Engine Demonstrator", Bejing, 1SABE-2007-119
4. Feiler, C, Berg, P., Haselbach, F., Benton, R., "Some Aspects of Flow and Heat Transfer Measurements of Non-Axisymmetrically Contoured Turbine Endwall", 1SABE-2005-1117
5. Benton, R., Rabe, G, Schiffer, H-P., Berg, P., "Ballistic Cooling of Turbine Nozzle Guide Vane Platforms", 1SABE-2005-1113