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Volume 2: Combustion and Fuels; Oil and Gas Applications; Cycle Innovations; Heat Transfer; Electric Power; Industrial and Cogeneration; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; IGTI Scholar Award | 1993

GAS TURBINE TOPPING STAGE BASED ON ENERGY EXCHANGERS:PROCESS AND PERFORMANCE

Erwin Zauner; Yau-Pin Dr. Chyou; Frederic Walraven; Rolf Althaus

Power generation in gas turbines is facing three main challenges today:• Low pollution prescribed by legal requirements.• High efficiency to obtain low operating cost and low CO2 emissions.• High specific power output to obtain low product and installation cost.Unfortunately, some of these requirements are contradictory: high efficiency and specific power force the development towards higher temperatures and pressures which increase NOx emissions and intensify the cooling and material strength problems. A breakthrough can be achieved by applying an energy exchanger as a topping stage. Inherent advantages are the self-cooled cell-rotor which can be exposed to much higher gas temperature than a steady-flow turbine and a very short residence time at peak temperature which keeps NOx emissions under control.The basic idea has been proposed long time ago. Fundamental research has now led to a new energy exchanger concept. Key issues include symmetric pressure-wave processes, partial suppression of flow separation and fluid mixing, as well as quick afterburning in premixed mode. The concept has been proven in a laboratory-scale engine with very promising results. The application of an energy exchanger as a topping stage onto existing gas turbines would increase the efficiency by 17% (relative) and the power by 25%. Since the temperature level in the turbine remains unchanged, the performance improvement can also be fully utilized in combined cycle applications. This process indicates great potentials for developing advanced gas turbine systems as well as for retrofitting existing ones.Copyright


Archive | 1994

Mixing chamber with vortex generators for flowing gases

Rolf Althaus; Alexander Dr. Beeck; Yau-Pin Dr. Chyou; Adnan Eroglu


Archive | 1998

Combustion chamber with two-stage combustion

Yau-Pin Dr. Chyou


Archive | 1994

Mixing apparatus with vortex generating devices

Yau-Pin Dr. Chyou; Adnan Eroglu


Archive | 1994

Fuel supply system for combustion chamber

Yau-Pin Dr. Chyou; Adnan Eroglu


Archive | 1993

Method for providing partial load operation in a gas turbine plant

Rolf Althaus; Yau-Pin Dr. Chyou; Hans Ulrich Frutschi; Christian Genet; Peter Kamber; Anders Lindvall; Peter Rufli; Thomas Sattelmayer; Peter Senior


Archive | 1995

Combustion chamber having self-ignition

Rolf Althaus; Yau-Pin Dr. Chyou; Franz Joos; Jakob J. Keller


Archive | 1994

Method of establishing part-load operation in a gas turbine group

Rolf Althaus; Yau-Pin Dr. Chyou; Hans Ulrich Frutschi; Christian Genet; Peter Kamber; Anders Lindvall; Thomas Dr. Sattelmayer; Peter Senior; Peter Rufli


Archive | 1995

Gas turbine and method of operating it

Yau-Pin Dr. Chyou; Thomas Sattelmayer; Peter Senior


Archive | 1994

Combustion chamber with self-ignition

Rolf Althaus; Yau-Pin Dr. Chyou; Franz Joos; Jakob Dr. Keller

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