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Details of Grant 

EPSRC Reference: GR/J67031/01
Title: PARASITIC HEATING IN GAS TURBINE ENGINE STATOR WELLS
Principal Investigator: Childs, Professor P
Other Investigators:
Turner, Professor AB
Researcher Co-Investigators:
Project Partners:
European Gas Turbines Ltd Rolls-Royce Plc (UK)
Department: Thermo Fluid Mechanics Research Centre
Organisation: University of Sussex
Scheme: Standard Research (Pre-FEC)
Starts: 01 April 1994 Ends: 31 March 1996 Value (£): 88,880
EPSRC Research Topic Classifications:
Fluid Dynamics Heat & Mass Transfer
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine Energy
Related Grants:
Panel History:  
Summary on Grant Application Form
The subject of this proposal is the overheating of gas in compressor or turbine stator wells due to windage/viscous dissipation of energy and the consequential over-heating of adjacent highly stressed rotating metal structures. Shrouded stator blades are used in gas turbine engines to eliminate blade vibration problems and to enhance stage efficiency when mechanical considerations necessitate relatively large radial clearances. The use of a shroud on a stator blade row requires a trench in the rotor known as a stator wall. Excess stator well metal temperatures, above the mainstream annulus total temperature, of between 30C and 120C have been measured in engine development rigs. There is little quantitative understanding of flow and heat generation and heat transfer in stator walls to provide a basis for trustworthy predictive design. The penalties for failing to derive configurations at or near the optimum can be severe; use of more expensive or heavier alloys; reduction of component life. The objective of this research is to understand quantitatively the generation of heat in stator wells by windage/viscous dissipation and to model processes so that the temperature rise in the surrounding metal can be predicted. A combined experimental, theoretical and analytic approach is proposed.
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Organisation Website: http://www.sussex.ac.uk