A method of operating a gas turbine assembly comprising the injection of a diluent in the gas turbine arrangement.

摘要

A method of injecting a diluent into a gas turbine assembly (110) is provided. The method comprises channeling an air stream into a first compressor (522) for compression, injecting a diluent into a diluent compressor (520) for compression, and channeling the compressed diluent into a compressed air stream exiting the first compressor To dilute oxygen content of the compressed air stream.