Combustor device for a gas turbine for being coupled to an oxygen generation unit

摘要

The present invention relates to a combustor device (100) for a gas turbine (150). The combustor device (100) comprises an inner shell (110) which forms a combustion chamber (111) and an outer shell (120) surrounding the inner shell (110) such that an outer channel (101) is formed between the inner shell (110) and the outer shell (120). The outer shell (120) comprises a first inlet (102) which is coupleable to a compressor (151) of the gas turbine (150) for feeding a compressed fluid from the compressor (151) into the outer channel (101) and a first outlet (103) for draining off the compressed fluid from the outer channel (101). The first outlet (103) is coupleable to a functional unit, in particular an oxygen generation unit, using the compressed fluid. The inner shell (110) comprises a second inlet (104) which is coupleable to the functional unit such that the compressed fluid is feedable from the functional unit (600) into the combustion chamber (111). The inner shell (110) further comprises a second outlet (105) which is coupleable to a turbine stage (152) of the gas turbine (150) for exhausting the compressed fluid out of the combustion chamber (111).