首页>
外国专利>
TURBOJET ENGINE AFTERBURNER COMBUSTION CHAMBER COMBUSTION ZONE STABILIZATION METHOD AND THE TURBOJET ENGINE AFTERBURNER COMBUSTION CHAMBER
TURBOJET ENGINE AFTERBURNER COMBUSTION CHAMBER COMBUSTION ZONE STABILIZATION METHOD AND THE TURBOJET ENGINE AFTERBURNER COMBUSTION CHAMBER
展开▼
机译:涡轮喷气发动机后燃烧室燃烧室稳定方法及涡轮喷气发动机后燃烧室燃烧室
展开▼
页面导航
摘要
著录项
相似文献
摘要
FIELD: engines and pumps.;SUBSTANCE: turbojet engine afterburner combustion chamber combustion zone stabilization method includes colliding with each other paired fuel-air jets radial supply into the incident flow. Each pair of colliding jets axes are located in the passing through the engine axis plane. Each pair axes are inclined towards each other. Angle between the axes is 45–120 degrees.;EFFECT: invention is aimed at increase in the afterburner combustion chamber reliability, hydraulic losses and the infrared radiation level reduction.;3 cl, 4 dwg
展开▼