FUEL INJECTION SYSTEM FOR STATOREACTOR, STATOREACTOR PROVIDED WITH SUCH AN INJECTION SYSTEM AND MISSILE PROPULSE THROUGH THIS STATOREACTOR

摘要

Fuel injection system for a ramjet 2 of the type comprising a vortex combustion chamber 5. BR/ According to the invention, this system comprises: BR/ - at least a first injector 181 arranged in the interior part 19 of the corresponding air sock to send, in common with said first injectors 181 of the other individual injection devices, fuel into a common area 16 of said combustion chamber adjacent to said closed end 9 and delimited peripherally by said air socks ; BR/ - at least one second injector 182 arranged in the outer part 20 of the corresponding air sock to deliver fuel to a specific zone 17i of said combustion chamber located near the wall thereof, downstream of the outlet 10i of the corresponding air sock. BR/ Missile propulsion. BR/ (CF DRAWING IN BOPI) BR/ BR/