SILO COMBUSTION CHAMBER FOR A GAS TURBINE

The invention relates to a silo combustion chamber (1) for a gas turbine (46) which can be coupled to a heat exchanger (54) during operation, comprising a flame tube (12) which is made of an inner wall (2) and a flame tube base (8) and which delimits a combustion chamber (10); an outer wall (6) whic...

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Bibliographic Details
Main Author WILKE MARTIN
Format Patent
LanguageChinese
English
Published 16.11.2016
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Summary:The invention relates to a silo combustion chamber (1) for a gas turbine (46) which can be coupled to a heat exchanger (54) during operation, comprising a flame tube (12) which is made of an inner wall (2) and a flame tube base (8) and which delimits a combustion chamber (10); an outer wall (6) which surrounds the inner wall (2), thereby forming a cavity (4); an annular chamber (20) which at least partly surrounds the outer wall (6) and which has a number of supply lines (22), said supply lines (22) being fluidically coupled to the hot side (57) of a heat exchanger (54) during the operation of the gas turbine (46); and a number of burners (24), each of which opens into the combustion chamber (10) on the outlet side through an opening (26) in the flame tube base (8) and the oxygen supply (34) of which is fluidically connected to the annular chamber (20). A collecting chamber (16) is provided which is arranged over the flame tube base (8), and a number of connection pieces (18) are also provided. The annular ch
Bibliography:Application Number: CN201580017846