Specification of

Combustion Systems

Combustion Systems is a gas turbine component used as a combustion chamber. In a gas turbine engine, combustor or combustion chamber is fed a high pressure air by the compression system. Combustor then heats this air at constant pressure. After heating, the air passes from the combustion chamber through the guide of the nozzle blades for the turbine. In the case of a ramjet or scramjet engine, the air is directly fed to the nozzle. We provide various spare parts of other gas turbine engines.