JET FUEL, PROCESS LIMITATIONS OF STABILIZATION AND FLAME COMBUSTION CHAMBER

摘要

1. Fuel injector for mixing the fuel flow and air flow, comprising: a downstream surface, fuel channels disposed on the downstream surface and adapted for flow of fuel flow therethrough, an annular bushing positioned around the downstream surface and having air vane for the flow therethrough of air flow, one or more air vanes have one or more blowing otverstiy.2. The fuel injector of claim 1, further comprising an outer tube with fuel channels, extending therethrough to the downstream poverhnosti.3. The fuel injector of claim 1, wherein the downstream surface has disposed thereon an end portion of the fuel forsunki.4. Fuel injector according to claim 3, wherein the end portion of the fuel nozzle has one or more apertures therethrough for flowing the fuel flow and / or flow vozduha.5. Fuel injector according to claim 4, wherein the flow of fuel through fuel channels is a first fuel flow, and fuel flow through one or more openings end part constitutes the second stream topliva.6. The fuel injector of claim 1, wherein the annular sleeve comprises a downstream ring disposed adjacent the air lopastyami.7. The fuel injector of claim 1, further comprising a fuel injector disposed in the combustion kamere.8. The fuel injector of claim 1, wherein after said one or more blowing openings extends vozduha.9 purge stream. The fuel injector of claim 8, wherein the flow of purging air through said one or more blowing apertures restricts fuel flow recirculation zone