B G. A. Halls, Air cooling of turbine blades and vanes, pp. 241-85GA.HALLS.Air Cooling of Turbine Blades and Vanes:An account of the history and development of gas turbine cooling.Aircraft Engineering. 1967
to a central rotating hub. The rotating assembly of blades and hub is known as an impeller, a rotor, or a runner; and it may or may not be enclosed in a housing. Fans may be driven by anelectric motor, aninternal-combustion engine, a steamturbine, agasturbine, or other motive power...
A gas turbine power plant in which a mixture of steam and compressed air, the mixture being primarily steam, is used to cool the rotating blades and stationary vanes in the turbine section. The air is bled from the compressor. The flow rate of steam that is mixed into the compressed air...
An air cooled turbine airfoil, such as a rotor blade, with a sequential impingement cooling circuit that provides a high level of cooling with a low amount of cooling air. The airfo
Gas turbine blades are cooled internally and externally and one widely used blade cooling technique is film cooling. In this type of cooling, relatively co... V Baghel,S Chandel,RS Reddy - 《Universal Journal of Mechanical Engineering》 被引量: 0发表: 2013年 Cooled nozzled guide vane or tu...
The advanced cooling technology for the 1 500 °C class gas turbines: steam-cooled vanes and air-cooled blades[J]. ASME J of Eng for Gas Turbine ... H Nomoto,A Koga,S Ito,... - Electric Power 被引量: 76发表: 1997年 An advanced impingement/film cooling scheme for gas turbines – ...
Simplicity and low manufacturing cost are achieved by having substantially all gas flow confining surfaces in the form of surfaces of revolution. Cooling of nozzle vanes and the drive turbine impeller blades by air ducted from the tubular flow allows turbine gas inlet temperatures of 2,200 DEG F...
The experimental data are presented on the deposition of particulate on transpiration air-cooled turbine vanes operating in a cascade for a series of tests... RAJ,R - 《J Eng Power》 被引量: 4发表: 1983年 Analysis and Testing of Air-Cooled Turbine Rotor and Stator Blades Problem definition...
The compressed air from which a mechanical equivalent of work has been taken out, is rectified through stationary vanes 8, and then is heated to give impact energy to a turbine impeller 1B. A cooling cylinder provided with cooling-air blow-out ports 9 is laid on an opened surface 3C, ...
Hot section components of stationary gas turbines, such as turbine blades and vanes, are coated with thermal barrier coatings (TBCs) to increase the compon... Yalnyüz Behiye Aybike,Kamutzki Franz,Gurlo AleksanderRupprecht Christian - 《Journal of Thermal Spray Technology》 被引量: 0发表: 2023...