FIELD: gas turbine engines.
SUBSTANCE: invention relates to devices designed for the formation and combustion of a fuel-air mixture in the combustion chambers of gas turbine engines. The countercurrent burner pre-mixing module contains an air supply channel, a pilot gas supply channel, gas outlet openings, and additionally contains a primary limited mixing chamber. The primary limited mixing chamber is profiled in the form of a diffusor-confusor channel. The primary limited mixing chamber is made reversible. The countercurrent burner pre-mixing module has a secondary direct-flow semi-limited mixing chamber with a fuel supply system distributed along its length.
EFFECT: invention provides ability to control the spatial position of the deflagration wave of the reaction and the implementation of the mechanisms of diffusion-kinetic combustion of fuel. It has a high degree of homogenization of the components of the fuel-air mixture, eliminates flame leakage and makes dynamic control of the combustion process possible.
4 cl, 2 dwg
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Authors
Dates
2021-06-23—Published
2020-12-14—Filed