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Method and burner for the combustion of liquid or gaseous fuels.

机译:用于燃烧液态或气态燃料的方法和燃烧器。

摘要

In a method and a burner for combustion of liquid or gaseous CONSUME A SIGNIFICANT PORTION OF FUEL IN THE ZONE LIMITING THE INNER TUBE BURNER WALL AND THAT IS RUNNING DOWN WITH RESPECT TO A DISCO (7) REMANSO . IN THE EXHAUST GAS THAT IS IN SPACE COMBUSTION IS CARRIED OUT RETURN THROUGH A RECIRCULATION EXHAUST GAS INTERNAL IN AN AREA OF DEPRESSION FORMED DOWNSTREAM OF DISCO (17) Backwater, and hence the tube (1 ) IS INTERRUPTED AND BURNER USED EQUIPMENT (25,27, 29) driving SOAR IN THE AREA OF DEPRESSION.
机译:在用于燃烧液体或气体的方法和燃烧器中,在区域中的燃料的显着部分限制了内管燃烧器壁,并且就迪斯科而言(7)REMANSO正在逐渐减少。在空间燃烧中排出的气体是通过减压形成的,在迪斯科(17)死水下游形成的低压区中通过再循环排出的气体而返回,因此,软管(1)发生了中断,并且使用了燃烧器(25,27) ,29)在抑郁区驾驶飞机。

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