A dual orifice fuel nozzle characterized in the provision of a pressure responsive flow modulating member in the primary fuel supply passage upstream of the spin passages and spin chamber of the primary discharge orifice, said member being operative in response to increasing primary fuel pressure to decrease the flow through the primary discharge orifice and to increase the angle of the fuel spray pattern therefrom once engine ignition and/or some low power condition is reached.
A fuel injection system for an internal combustion engine has two intake valves for a combination chamber. The fuel injection system is comprised of a fuel injector installed in an intake manifold to supply fuel into the engine. The fuel injector is formed with at least two fuel discharge openings through which fuel sprays are ejected respectively toward the two intake valves. The fuel injector is further formed with at least one air discharge opening through which air is ejected at a high speed toward a position between the fuel sprays thereby to positively separate the fuel sprays from each other.
In some fuel injectors having VOP (valve opening pressure) type needle checks, the check return spring cavity also functions as a portion of the fuel supply passage. A return spring is compressed within the return spring cavity between an end wall and one end of the needle check. Instead of utilizing a pin stop to limit the movement of the needle check as in the prior art, the present invention utilizes a shoulder stop surface which comes into contact with one end of the needle check when the needle valve is fully open. This elimination of the prior art pin stop is believed to eliminate or reduce cavitation damage to the check return spring, pin chipping problems, beat in problems due to pin stop cocking or tipping within the return spring cavity, and other wear and functionality problems caused by a free floating pin stop.
A device for introducing fuel into the head space of cylinder of non-premixed charge (diesel) engines is disclosed, which distributes fuel in atomized form in a plume, whose fluid dynamic properties are such that the compression heated air in the cylinder head space is entrained into the interior of the plume where it is mixed with and ignites the fuel in the plume interior, to thereby control combustion, particularly by use of a multiplicity of individually controllable devices per cylinder.
A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. The inner fuel passage extends axially along a longitudinal axis to a first terminal end defining a first discharge orifice of the nozzle. The outer air passage extends coaxially with the inner fuel passage along the longitudinal axis to a second terminal end disposed concentrically with the first terminal end and defining a second discharge orifice oriented such that the discharge therefrom impinges on the fuel discharge from the first discharge orifice. An array of turning vanes is disposed within the outer air passage in a circular locus about the longitudinal axis. Each of the vanes is configured generally in the shape of an airfoil and has a pressure side and an opposing suction side. The vanes extend axially from a leading edge surface to a tapering trailing edge surface along a corresponding array of chordal axes, each of axes is disposed at a given turning angle to the longitudinal axis. The suction side of each vane is spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Atomizing air is directed through the air flow channels to be issued from the second discharge orifice as a generally helical flow having a substantial uniform velocity profile.
A fuel nozzle for dispensing an atomized fluid spray into the combustion chamber of a gas turbine engine. The nozzle includes a body assembly with an inner fuel passage and an annular outer atomizing air passage. The inner fuel passage extends axially along a longitudinal axis to a first terminal end defining a first discharge orifice of the nozzle. The outer air passage extends coaxially with the inner fuel passage along the longitudinal axis to a second terminal end disposed concentrically with the first terminal end and defining a second discharge orifice oriented such that the discharge therefrom impinges on the fuel discharge from the first discharge orifice. An array of turning vanes is disposed within the outer air passage in a circular locus about the longitudinal axis. Each of the vanes is configured generally in the shape of an airfoil and has a pressure side and an opposing suction side. The vanes extend axially from a leading edge surface to a tapering trailing edge surface along a corresponding array of chordal axes, each of axes is disposed at a given turning angle to the longitudinal axis. The suction side of each vane is spaced-apart from a juxtaposing pressure side of an adjacent vane to define a corresponding one of a plurality of aligned air flow channels therebetween. Atomizing air is directed through the air flow channels to be issued from the second discharge orifice as a generally helical flow having a substantial uniform velocity profile.
