Turbojet after burner and control system, has multiple injector nozzles arranged in geometry at after burner chamber-inner jacket and after burner chamber of fluid supplying system

摘要

The turbojet after burner and control system has multiple injector nozzles arranged in a geometry at the after burner chamber-inner jacket and after burner chamber (6) of fluid supplying system. A system of geometrically arranged injector nozzles for partial or complete control of injection milding control process is formed at cylinder shaped slide valve units. The slide valves are movable and are slided against each other.