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Experimental Verification of High-Temperature Resistance and High Resolution of Inductive Tip Clearance Measurement System. [PDF]
Sensors (Basel)Zhao Z, Zhao L, Lyu Y, Liu Z.
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Investigation of a staggered dual-rotor wound field synchronous motor for offshore wind turbine full-scale testing platforms. [PDF]
Sci RepXue Y +5 more
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Hydrogen-cooled turbine generators
Electrical Engineering, 1940ONE of the most radical innovations in the design of electrical machinery in recent years has been the adoption of hydrogen cooling for large turbine generators. Now that a number of the large hydrogen-cooled units are in operation, it would seem timely to review the experience gained in building and operating this new-type equipment.
M. D. Ross, C. C. Sterrett
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Proceedings of the Institution of Mechanical Engineers, 1970
This paper lists the steps in the development chain of air cooling for gas turbine components, and represents transpiration cooling as the ultimate method. The three modes of heat transfer involved in transpiration cooling, gas side heat transfer, coolant side heat transfer and interstitial heat transfer, are discussed separately.
F. J. Bayley, A. B. Turner
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This paper lists the steps in the development chain of air cooling for gas turbine components, and represents transpiration cooling as the ultimate method. The three modes of heat transfer involved in transpiration cooling, gas side heat transfer, coolant side heat transfer and interstitial heat transfer, are discussed separately.
F. J. Bayley, A. B. Turner
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Journal of Propulsion and Power, 2006
The durability of gas turbine engines is strongly dependent on the component temperatures. For the combustor and turbine airfoils and endwalls, film cooling is used extensively to reduce component temperatures. Film cooling is a cooling method used in virtually all of today's aircraft turbine engines and in many power-generation turbine engines and yet
D. G. Bogard, K. A. Thole
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The durability of gas turbine engines is strongly dependent on the component temperatures. For the combustor and turbine airfoils and endwalls, film cooling is used extensively to reduce component temperatures. Film cooling is a cooling method used in virtually all of today's aircraft turbine engines and in many power-generation turbine engines and yet
D. G. Bogard, K. A. Thole
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Proceedings of the Institution of Mechanical Engineers, 1950
The cooling of turbines offers the alternative advantages of the use of higher cycle-maximum-temperatures than are possible with uncooled turbines, with consequent increase of thermal efficiency and power output for a given size of compressor, or the use of lower quality materials for a given turbine inlet-temperature.
A. G. Smith, R. D. Pearson
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The cooling of turbines offers the alternative advantages of the use of higher cycle-maximum-temperatures than are possible with uncooled turbines, with consequent increase of thermal efficiency and power output for a given size of compressor, or the use of lower quality materials for a given turbine inlet-temperature.
A. G. Smith, R. D. Pearson
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Journal of Engineering for Power, 1959
Turbine cooling, originally developed because of a shortage of heat-resistant alloys, is of interest for certain applications to permit operation of gas-turbine engines above uncooled temperatures. Specific power output would be increased, and in some cases specific fuel consumption decreased, depending on the engine type.
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Turbine cooling, originally developed because of a shortage of heat-resistant alloys, is of interest for certain applications to permit operation of gas-turbine engines above uncooled temperatures. Specific power output would be increased, and in some cases specific fuel consumption decreased, depending on the engine type.
openaire +1 more source