FIELD: manufacture of gas-turbine engines. SUBSTANCE: proposed combustion chamber includes mixing zone and combustion zone separated by means of stabilizer and shield secured to stabilizer and separated from it by means of cavity. Shield located in mixing zone includes additionally holes for communication of mixing zone with said cavity. Shield may be made in form of screen. Provision is made for avoidance of ignition of fuel-and-gas mixture in mixing zone from hot stabilizer, thus excluding burning-out and fusion of stabilizer reducing length of mixing section. EFFECT: enhanced efficiency. 2 cl, 3 dwg
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