Gas turbine arrangement

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 6/06 (2006.01) B01D 53/56 (2006.01) F01K 23/10 (2006.01) F02C 3/30 (2006.01) F02C 6/00 (2006.01) F02C 6/16 (2006.01) F02C 9/40 (2006.01)

Patent

CA 2086184

ABSTRACT OF THE DISCLOSURE In a gas turbine arrangement having a plurality of independent pressure stages, with or without an integrated steam process, which is extended by an air cell cavern, ammonia is injected into the waste gases downstream of the first turbine and the first heat generator and upstream of a second heat generator. The location of this injection ensures that the so-called selective nitrogen conversion becomes effective when a temperature window of 800 - 900 degrees Celsius is present. By means of a purposeful, caloric preparation of the hot gases and appropriate design of the high-pressure turbine, the temperature window is made available at which NOx emissions can be minimized by means of injecting ammonia.

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