Single Vs. Two stage high pressure turbine design of modern aero engines

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Ahmad, Fathi ^a   Mirzamoghadam, Alexander V ^b,c  

^a TECHNISCHE UNIVERSITÄT BERLIN   (Germany)

^b BMW Rolls Royce Aero Engines Methods and Technology   (Germany)

^c SIEMENS POWER GENERATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BYPASS RATIO; COST EFFECTIVENESS; COST REDUCTION; COSTS; DESIGN; ENGINES; INLET FLOW; MARINE ENGINEERING; MARINE ENGINES; TEMPERATURE; THERMODYNAMIC PROPERTIES;

COMPETITIVE PERFORMANCE; DESIGN CONFIGURATIONS; HIGH PRESSURE TURBINE; OVERALL PRESSURE RATIOS; SECONDARY-AIR SYSTEM; SPECIFIC FUEL CONSUMPTION; THRUST-TO-WEIGHT RATIO; TURBINE INLET TEMPERATURE;

GAS TURBINES;

EID: 84928576468     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-001     Document Type: Conference Paper

References (8)

1. Ahmad, F., 1998. 'Comparative Study of the Single & Two Stage HPT for the BR7I5-56 Undenving Aplication', BMW-RR & The Technical University of Berlin; Diplom-Thesis.
2. Dundas, R.E. and Japikse, D., 1985. Preliminary Design of The Gas Turbine, Sawyer's Gas Turbine Engineering Handbook, Vol. I Chapter 9.
3. Dundas, RE., 1985. Mechanical Design of The Gas Turbine, Sawyer's Gas Turbine Engineering Handbook, Vol. I Chapter 10.
4. Hourmouziades, J., 1995. Lecture Manual for aircraft Propulsion, Technical University of Berlin.
5. Khatib, F., 1998. ' Design Analysis of a Single Stage HPT Casing for Shrouded / Unshrouded Blades in an Alternative Engine Cycle with Comparable Overall Requirements to the BR7I5-56 ', BMW-RR and the Technique University of Berlin; Diplom-Thesis.
6. Kurzke, J., 1996. GASTURB manual and the Program.
7. Moravecek, J.J., 1997, The PW6000 Design Philosophy Meets Today's 100 Passenger Aircraft Propulsion System Requirements, Pratt & Whitney, external presentation.
8. Wilson, D.C., 1991. The Design of High - Efficiency Turbomachinery and Gas Turbines. The MIT Press Cambridge/ Massachusetts/ London.