Method and gas turbine combustion system for safely mixing H2-rich fuels with air

1. A method for mixing H2-rich fuels with air in a gas turbine combustion system having a combustion chamber with a burner, comprising:

providing a first stream of burner air, branched from a stream of compressor air, and a second stream of a H2-rich fuel, wherein the first stream of burner air is not used for liner cooling;

pre-premixing all of the H2-rich fuel to be injected with the first stream of burner air to produce a pre-premixed fuel/air mixture; and

providing a main air stream, taken from the stream of compressor air and used for liner cooling before entering the burner; and

in the burner, injecting the pre-premixed fuel/air mixture into the main air stream and premixing the pre-premixed fuel/air mixture and the main air to form a premixture within the burner which enters the combustion chamber;

wherein the pre-premixed fuel/air mixture is injected in an axial direction that is in a cross-flow direction with respect to a direction of injection of the main air stream flow,

wherein an air excess factor of A>1, is achieved in the premixing in the burner.

2. The method according to claim 1 , wherein the premixing is done in a manner for preventing flame anchoring at undesired locations, including at least one of near an injection location and in the burner.

3. The method according to claim 1 , comprising:

separating air into O2 and N2 with an air separation unit; and

adding a portion of the N2 from the air separation unit to at least one of the main burner air and the pre-premixed fuel/air mixture.

4. The method according to claim 1 , comprising:

using a pre-premixer formed as a channel with straight air flow to avoid at least one of recirculation and stagnation regions to produce the pre-premixed fuel/air mixture.