Fuel injection apparatus and system

• US 4,509,483 A
• Filed: 01/24/1984
• Issued: 04/09/1985
• Est. Priority Date: 01/24/1984
• Status: Expired due to Fees

• Current Assignee: Coltec Industries Incorporated (Enpro Industries Incorporated)
• Original Assignee: Colt Industries Operating Corporation
• Inventors: Johnson, Kalin S.
• Primary Examiner(s): Nelli, Raymond A.
• Application Number:
  US06/573,336
• Time in Patent Office: 441 Days
• Field of Search: 123/438, 123/437, 123/457, 123/489, 123/440, 123/432, 261/50 R, 261/69
• US Class Current: 123/672
• CPC Class Codes: F02M 51/02 specially for low-pressure fuel-injection F02M51/005 takes precedence; pumpsper se F02M51/04; injectors per se F02M51/08
• CPC Class Codes: F02M 69/04 Injectors peculiar thereto
• CPC Class Codes: F02M 69/047 injectors with air chambers, e.g. communicating with atmosphere for aerating the nozzles F02M69/325 takes precedence

Abstract

A fuel metering apparatus is shown as having a throttle body with an induction passage therethrough and a throttle valve for controlling flow of induction air through the induction passage, first and second passages are provided with the first passage having an inlet at one end and communicating at its other end with a source of fuel, the second passage has an inlet at one end and communicates with the flow of induction air thereby serving as a metered fuel discharge nozzle, fuel at a regulated superatmospheric pressure is delivered as through a movable tubular member and discharged through an open end thereof in a manner whereby such discharged fuel is alternately directed toward the inlet of the first passage and toward the inlet of the second passage, a magnetic field is cyclically produced as to thereby cause movement of the movable tubular member as to thereby cause such discharged fuel to be alternately directed to the inlets of the first and second passages, the portion of the fuel directed to the inlet of the second passage being that used in forming the fuel-air mixtures supplied to the engine.

Claims

1. Fuel injection apparatus and system for a combustion engine, comprising throttle body means, induction passage means formed through said throttle body means, throttle valve means for controlling the flow of induction air through said induction passage means, an associated source of fuel, metered fuel discharge nozzle means for discharging metered fuel into said flow of induction air through said induction passage means, said metered fuel discharge nozzle means comprising first fuel inlet means, fuel return passage means for operative communication with said associated source of fuel, said fuel return passage means comprising second fuel inlet means, fuel discharge orifice means, means for providing a supply of fuel under regulated superatmospheric pressure to said fuel discharge orifice means as to be discharged therethrough, and means responsive to indicia of engine operation for causing a first portion of said fuel as is discharged from said discharge orifice means to flow into said second inlet means and through said fuel return passage means and causing a second portion of said fuel as is discharged from said discharge orifice means to flow into said first inlet means and be discharged by said metered fuel discharge nozzle means into said flow of induction air, said second portion of said fuel as is discharged into said flow of induction air determining the rate of metered fuel flow being supplied to said engine, said means responsive to indicia of engine operation being effective to vary the relative proportion of said first portion compared to said second portion as to thereby vary the rate of said metered fuel flow in accordance with engine operating conditions.

2. Fuel injection apparatus according to claim 1 wherein said means responsive to indicia of engine operation comprises magnetic field generating means.

3. Fuel injection apparatus according to claim 1 wherein said discharge orifice means is movable relative to said first and second inlet means.

4. Fuel injection apparatus according to claim 1 wherein said means for providing a supply of fuel under regulated superatmospheric pressure comprises deflectable tubular means, wherein said tubular means comprises conduit means, and wherein said fuel discharge orifice means comprises an open end of said conduit means.

5. Fuel injection apparatus according to claim 4 wherein said means responsive to indicia of engine operation comprises magnetic field generating means, and wherein said magnetic field generating means is effective to deflect said tubular means in order to determine whether said fuel discharged by said discharge orifice means is directed to either of said first or second inlet means.

6. Fuel injection apparatus and system for a combustion engine, comprising throttle body means, induction passage means formed through said throttle body means, throttle valve means for controlling the flow of induction air through said induction passage means, an associated source of fuel, metered fuel discharge nozzle means for discharging metered fuel into said flow of induction air through said induction passage means, said metered fuel discharge nozzle means comprising first fuel inlet means, fuel return passage means for operative communication with said associated source of fuel, said fuel return passage means comprising second fuel inlet means, fuel discharge orifice means, means for providing a supply of fuel under regulated superatmospheric pressure to said fuel discharge orifice means as to be discharged therethrough, and means responsive to indicia of engine operation for causing a first portion of said fuel as is discharged from said discharge orifice means to flow into said second inlet means and through said fuel return passage means and causing a second portion of said fuel as is discharged from said discharge orifice means to flow into said first inlet means and to be discharged by said metered fuel discharge nozzle means into said flow of induction air, said second portion of said fuel as is discharged into said flow of induction air determining the rate of metered fuel flow being supplied to said engine, said means responsive to indicia of engine operation being effective to vary the relative proportion of said first portion compared to said second portion as to thereby vary the rate of said metered fuel flow in accordance with engine operating conditions, wherein said means for providing a supply of fuel under regulated superatmospheric pressure comprises deflectable tubular means, wherein said tubular means comprises conduit means, wherin said fuel discharge orifice means comprises an open end of said conduit means, wherein said tubular means is supported in a cantilevered manner as to have said discharge orifice means movable relative to said first and second inlet means, wherein said means responsive to indicia of engine operation comprises magnetic field generating means, and wherein said magnetic field generating means is effective to cause deflection of said tubular means in order to thereby determine whether said fuel discharged by said discharge orifice means is directed to either said first or second inlet means.

7. Fuel injection apparatus according to claim 6 wherein said tubular means has an inherent spring rate, wherein said magnetic field generating means comprises a field winding and associated pole-piece means, and armature means operatively connected to said tubular means and effective to be magnetically attracted toward said pole-piece means upon energization of said field winding.

8. Fuel injection apparatus according to claim 7 wherein said fuel discharge orifice means is effective for discharging fuel therefrom and toward said first inlet means when said armature means is attracted to said pole-piece means.

9. Fuel injection apparatus according to claim 6 and further comprising spring means for supporting at least a portion of said tubular means, wherein said magnetic field generating means comprises a field winding and associated pole-piece means, wherein said spring means is effective to be magnetically attracted toward said pole-piece means upon energization of said field winding, and wherein said tubular means moves with said spring means when said spring means is attracted to said pole-piece means.

10. Fuel injection apparatus according to claim 9 wherein said spring means is supported in a manner as to be cantilevered, and wherein when said cantilevered spring means is attracted to said pole-piece means said spring means and said tubular means are angularly deflected.

11. Fuel injection apparatus according to claim 10 wherein said tubular means is comprised of flexible material.

12. Fuel injection apparatus according to claim 6 wherein said magnetic field generating means comprises an annular field winding defining a generally medially situated axially extending clearance passageway therethrough, wherein said tubular means extends at least partly through said clearance passageway, and wherein said tubular means when in a null position is situated as to be eccentrically disposed with respect to the axis of said clearance passageway.

13. Fuel injection apparatus according to claim 6 wherein said magnetic field generating means comprises field winding means having at least portions disposed at generally opposite sides of said tubular means, wherein said tubular means is deflected as a consequence of moving to a position whereat the spring force of said tubular means is balanced by the magnetic force of the magnetic field generated by said magnetic field generating means when said field winding means is energized.

14. Fuel injection apparatus according to claim 6 wherein said fuel return passage means extends transversely of and through said induction passage means.