초록 ▼

A novel laminar flow nozzle for fuel injected racing cars is described herein. One novel feature comprises a narrow angle between converging conduit component channels. These channels, in turn, supply vaporized fuel and nitrous oxide to the main chamber of the nozzle. Another important novel feature

A novel laminar flow nozzle for fuel injected racing cars is described herein. One novel feature comprises a narrow angle between converging conduit component channels. These channels, in turn, supply vaporized fuel and nitrous oxide to the main chamber of the nozzle. Another important novel feature is the integral structure of the nozzle; the conduit components, generally rigid and cylindrical in shape, are physical integral components of the nozzle. The result of our invention is a nozzle with a smooth laminar flow of gases which results in less turbulence and greater horsepower.

대표청구항 ▼

[ We claim:] [1.] A laminar flow nozzle of one piece design and physically integral structure comprising(a) a hollow chamber, said chamber having a first upper end and a second, opposite end, said hollow chamber comprising a first and a second channel,(b) a first cylindrical conduit component for tr

[ We claim:] [1.] A laminar flow nozzle of one piece design and physically integral structure comprising(a) a hollow chamber, said chamber having a first upper end and a second, opposite end, said hollow chamber comprising a first and a second channel,(b) a first cylindrical conduit component for transporting a stream of nitrous oxide from said first upper end to said second lower end, said conduit component comprising a jet for controlling said stream of nitrous oxide, said jet comprising an orifice, said orifice having a diameter of approximately 0.016 to 0.136 inches, said orifice leading to said first channel through said conduit component(c) a second cylindrical conduit component for transporting a stream of said fuel from said first upper end to said second, lower opposite end of said chamber, said conduit component comprising a jet for controlling said stream of fuel, said jet comprising an orifice leading to said second channel, said jet orifice being approximately 0.016 to 0.136 inches in diameter;(d) an aperture at said second lower end of said nozzle reby said vaporized fuel and said nitrous oxide combust at said second opposite end of said nozzle chamber, thereby creating less turbulence and producing more horsepower.