Patent ID: 6116225
Filing Date: 2000-09-12
Classification: F02M,Y02T

Abstract:
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 nozzleWhereby 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.