Fuel injector having a magnetostrictive actuator device
The present disclosure provides a fuel injector including a magnetostrictive actuator that is capable of precise control of a needle or nozzle valve element. The magnetostrictive actuator is direct-acting on the nozzle valve element, which extends into the magnetostrictive actuator, providing a compact fuel injector configuration that may provide rate-shaping of a fuel injection event.
1. A fuel injector for an internal combustion engine, comprising:
a fuel injector body including a longitudinal axis, an upper body portion, a fuel injector cavity, and a nozzle housing having at least one injector orifice positioned at a distal end thereof in communication with the fuel injector cavity;
a magnetostrictive actuator extending along the longitudinal axis and positioned in the fuel injector cavity, the magnetostrictive actuator including at least a first annular magnetostrictive element, a second magnetostrictive element, and a carrier component positioned transversely between the first and second annular magnetostrictive elements, and at least one of the first and second magnetostrictive elements is comprised of a galfenol material, and the magnetostrictive actuator further includes a coil positioned to provide a magnetic field to the first and second annular magnetostrictive elements; and
a nozzle valve element extending along the longitudinal axis and into a first end of the first annular magnetostrictive element and out from a second end of the first annular magnetostrictive element, the first and second annular magnetostrictive elements being extendable in the presence of the magnetic field generated by the coil to move the nozzle valve element from a closed position, blocking a fuel flow into the at least one injector orifice from the fuel injector cavity, to an open position, permitting fuel flow into the at least one injector orifice from the fuel injector cavity, and the first and second magnetostrictive elements being contractable to permit the nozzle valve element to move from the open position to the closed position upon removal of the magnetic field.
2. The fuel injector of claim 1 , wherein the at first and second annular magnetostrictive elements are configured to elongate when under tension.
3. The fuel injector of claim 1 , further including a bias spring positioned longitudinally between a proximate end of the nozzle valve element and the upper body portion to apply a bias force to the nozzle valve element.
4. The fuel injector of claim 1 , wherein the magnetostrictive actuator includes three annular magnetostrictive elements and a second carrier component positioned transversely between a second two of the three annular magnetostrictive elements.
5. A fuel injector for an internal combustion engine, comprising:
a fuel injector body including a longitudinal axis, an upper body portion, a fuel injector cavity, and a nozzle housing having at least one injector orifice positioned at a nozzle housing distal end in communication with the fuel injector cavity;
a first annular magnetostrictive element having a longitudinally extending central passage, a second annular magnetostrictive element, and a first annular coupler positioned transversely between the first annular magnetostrictive element and the second annular magnetostrictive element, the first annular magnetostrictive element, the second annular magnetostrictive element and the coupler positioned in the fuel injector cavity between the upper body portion and the at least one injector orifice, and the first annular magnetostrictive element, the second annular magnetostrictive element and the coupler extending along the longitudinal axis;
a coil positioned to provide a magnetic field to the first annular magnetostrictive element and the second annular magnetostrictive element; and
a nozzle valve element extending along the longitudinal axis and into the central passage, the first annular magnetostrictive element being expandable in the presence of the magnetic field to apply an actuating force to move the first coupler in a direction that is longitudinally away from the at least one injector orifice, and the second annular magnetostrictive element being expandable in the presence of the magnetic field to move the nozzle valve element from a closed position, blocking a fuel flow into the at least one injector orifice from the fuel injector cavity, to an open position, permitting fuel flow into the at least one injector orifice from the fuel injector cavity, and the first annular magnetostrictive element and the second annular magnetostrictive element being contractable upon removal of the magnetic field to permit the nozzle valve element to move from the open position to the closed position.
6. The fuel injector of claim 5 , wherein first annular magnetostrictive element includes a distal end and a proximate end, and the nozzle valve element extends into the distal end and extends from the proximate end.
7. The fuel injector of claim 5 , further including a bias spring positioned longitudinally between a proximate end of the nozzle valve element and the upper body portion to apply a bias force to the nozzle valve element.
8. The fuel injector of claim 5 , further including a third annular magnetostrictive element positioned transversely between the second annular magnetostrictive element and the coil, and a second coupler positioned transversely between the second annular magnetostrictive element and the third annular magnetostrictive element.
9. The fuel injector of claim 5 , wherein at least one of the first and second annular magnetostrictive elements includes a material selected from the group consisting of gallium, iron, nickel, copper, manganese, cobalt, terbium, and dysprosium.
10. The fuel injector of claim 5 , wherein at least one of the first and second annular magnetostrictive elements is comprised of one of galfenol and terfenol.
11. The fuel injector of claim 1 , wherein at least one of the first and second annular magnetostrictive elements is exposed to the nozzle valve element.