SYSTEM AND METHOD FOR TURBINE COMBUSTION CHAMBER Russian patent published in 2017 - IPC F02C3/34 

FIELD: machine engineering.

SUBSTANCE: fuel combustion system is proposed, comprising a turbine combustion chamber that includes a head part with a head chamber. The head part contains the exhaust gas channel, the fuel channel and the oxidant channel. The turbine combustion chamber also comprises a combustion chamber portion located downstream of the head chamber. The turbine combustion chamber includes a partition located between the head chamber and the combustion chamber so that the fuel from the fuel channel and the oxidant from the oxidant channel are intended for combustion inside the combustion chamber located downstream of the partition. The turbine combustion chamber comprises an end plate having at least one port connected to the exhaust gas channel or oxidant channel, the head chamber being coaxial between the partition and the end plate. Variants of a system for fuel combustion and a method for fuel combustion are also presented.

EFFECT: increased service life of the components, allows to control the temperature, pressure, flow rate, moisture content, particle content and the composition of the exhaust gas.

50 cl, 20 dwg, 2 tbl