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Full-Text Articles in Mechanical Engineering
Development Of Novel Passive Control Techniques For More Uniform Temperature At Combustor Exit And Hybrid Les/Rans Modeling, Alka Gupta
Theses and Dissertations
Gas turbines have become an important, widespread, and reliable device in the field of power generation. For any gas turbine system, the combustor is an integral part responsible for the combustion of the fuel. A number of studies have shown that the flow field exiting a combustor is highly non-uniform in pressure, velocity and, most importantly, temperature. Hot streaks amongst other non-uniformities cause varying thermal stresses on turbine blades and put pressure on the blade materials. In particular, these non-uniformities can have detrimental effects on the performance of the engine and cause a reduction in the expected life of critical …
Operational Characteristics Of An Ultra Compact Combustor, Christopher J. Damele
Operational Characteristics Of An Ultra Compact Combustor, Christopher J. Damele
Theses and Dissertations
Ultra Compact Combustors offer unique solutions to minimize engine size and weight. They accomplish this by reducing the number of components in the engine core and perform the combustion in a circumferential cavity that encircles the core flow. Within this cavity, the fuel is injected rich. Burning continues to occur in the vane passage beneath the circumferential cavity which must be completed in a controlled manner prior to the inlet plane of the turbine rotor. Furthermore, the temperature distribution at the exit of the vane passage must be controlled to generate high work extraction from the turbine. The primary metrics …