Liquid fuel combustion chamber with air nozzles in walls at diverse angles

Claim 1

APPARATUS FOR THE COMBUSTION OF FLUID FUEL COMPRISING, IN COMBINATION, A LONGITUDINALLY ELONGATED COMBUSTION CHAMBER INCLUDING SUBSTANTIALLY PARALLEL FRONT AND REAR WALLS AND SUBSTANTIALLY PARALLEL BOTTOM, TOP AND SIDE WALLS, A MECHANICALLY FUEL INJECTOR EXTENDING INTO SAID COMBUSTION CHAMBER THROUGH SAID FRONT WALL FOR PROJECTING ATOMIZED LIQUID FUEL ALONG THE LONGITUDINAL AXIS OF THE COMBUSTION CHAMBER, MEANS FORMING AIR CHANNELS EXTENDING ALONG THE TOP, BOTTOM AND SIDE WALLS OF THE COMBUSTION CHAMBER, A PLURALITY OF TUBULAR AIR NOZZLES PROJECTING FROM SAID CHANNELS INTO SAID COMBUSTION CHAMBER, THE NOZZLES ADJACENT SAID FRONT WALL BEING INCLINED INWARDLY AND REARWARDLY WITH THE NOZZLES NEAREST SAID FRONT WALL HAVING A GREATER REARWARD INCLINATION THAT THOSE NOZZLES FARTHER FROM THE FRONT WALL, THE NOZZLES AT THE CENTER OF THE CHAMBER BEING SUBSTANTIALLY PERPENDICULAR TO THE LONGITUDINAL AXIS THEREOF AND THE NOZZLES ADJACENT THE REAR WALL BEING FORWARDLY AND INWARDLY INCLINED, WITH THE NOZZLES NEAREST THE REAR WALL HAVING A GREATER FORWARD INCLINATION THAN THOSE MORE REMOTE THEREFROM, SAID NOZZLES ADJACENT SAID FRONT WALL BEING SPACED FROM SAID INJECTOR INITIALLY TO OXIDIZE THE FUEL AT A DISTANCE THEREFROM, ADDITIONAL NOZZLES IMMEDIATELY ADJACENT SAID REAR WALL EXTENDING SUBSTANTIALLY PARALLEL TO THE LONGITUDINAL AXIS OF THE COMBUSTION CHAMBER, AND MEANS FOR SUPPLYING AIR UNDER PRESSURE TO SAID AIR CHANNELS.