OCR Text |
Show that they can maintained decreasing fuel flow rate and improving production quality. The combustion chambers were certified and recommended for nationwide deployment. REFERENCES 1. Combustion chamber for gas turbine engine (its variants): Patent # 2,062,409 Russia, 6 F23 R3/18. 2. Method of gaseous fuel combustion in air flow: Patent # 2,064,634 Russia, 6 F23 R3/34. 3. Zeldovich Ya.B., Acta Phvsicochim. USSR, 1946, vol.21, P.577. 4. Roslyakov P.V., Theoretical foundations of nitrogen oxides formation for organic fuel combustion and methods to decrease their emission in boilers and power equipment. Abstract of the doctoral thesis, Moscow, 1993. 5. Dubrovkin N.F., A handbook of hydrocarbon fuels and their combustion products. Gosenergoizdat. Moscow-Leningrad, 1962, P.288. 6. Kuznetsov V.R., Lebedev A.B., Sekundov A.N. and Smimova I.P., Calculation of diffusion flame of turbulent combustion regarding concentration fluctuations and buoyancy forces. Izv. A N SSSR, Fluid and Gas Mechanics, 1977, No.l. pp.32-40. 8 |