| 摘要 |
FIELD: aircraft industry. SUBSTANCE: aircraft turbojet engine has air intake diffuser, main combustion chamber with exit nozzles, turbine and additional combustion chamber with nozzle and air supply channel installed in behind-the-turbine space. Air supply channel provided with air heaters is connected at inlet to compressor outlet. Wall of exit nozzle serves as wall of additional combustion chamber. EFFECT: enhanced reliability of operation. 2 dwgs |
