Fuel control apparatus
The invention, described herein, is an improved Fuel Injection Servo (“Servo”) for the homebuilt aircraft. The Servo has been designed to allow the manufacturer to more easily fine tune the pressure differential over the air diaphragm. The Servo also provides an idle valve that the manufacturer and homebuilder can easily fine tune. In a second embodiment, the Servo is further adapted to replace the carburetor in smaller aircraft.
1. In a fuel injection system for an internal combustion engine, said fuel injection system comprising:
(a) an air passage mechanism where the air passage mechanism comprises a central section;
(i) where the central section defines a plenum allowing air passage through the air passage mechanism;
(ii) where the central section further comprises a venturi and a throttle valve mounted within the plenum; where flow of air through the air passage mechanism generates an air pressure differential which is the difference between impact pressure and venturi suction pressure;
(iii) the air passage mechanism comprising an air pressure differential adjustment mechanism comprising a single venturi suction tube and a shim; where the venturi suction tube is configured to allow measurement of the venturi suction pressure; where the venturi tube is attached to the shim; where the shim is mounted within the plenum and configured to be manipulated to adjust the location of the venturi suction tube to thereby adjust the venturi suction pressure;
(b) a fuel pressure modifying mechanism which receives fuel from a supply and delivers the fuel at a pressure different from the supply comprising a fuel regulator and an idle valve; and
(c) a fuel metering mechanism.
2. The fuel injection system of claim 1 where the idle valve comprises an integrated metering jet where there is a flow of liquid through the metering jet and a mechanism to modify the flow through metering jet where:
(a) the metering jet extends axially from a near end of a barrel valve and rotatably mates with a sleeve valve; where the barrel valve defines a notched hole and the sleeve defines an outlet hole;
(b) where the mechanism to modify the flow through the metering jet comprises a needle valve; where the needle valve rotatably mates with a far end of the barrel valve; where the flow through the metering jet is adjusted by extending or contracting the needle valve to or from the far end of the barrel valve.
3. The fuel injection system of claim 2 where the flow through the metering jet is increased by aligning the notched hole and the outlet hole.
4. The fuel injection system of claim 2 where the needle valve is rotated into the barrel valve by a screw; where the flow through the metering jet is decreased by rotating the needle valve into the barrel valve.
5. In a fuel injection system for an internal combustion engine, said fuel injection system comprising:
(a) an air passage mechanism where said air passage mechanism comprises a central section:
(i) where the central section defines a plenum allowing air passage through the air passage mechanism;
(ii) where the central section further comprises a venturi and a throttle valve mounted within the plenum; where said flow of air through the air passage mechanism generates an air pressure differential which is the difference between impact pressure and venturi suction pressure;
(iii) where fuel is delivered downstream of the throttle valve;
(iii) the air passage mechanism comprising an air pressure differential adjustment mechanism comprising a single venturi suction tube and a shim; where the venturi suction tube is configured to allow measurement of the venturi suction pressure; where the venturi tube is attached to the shim; where the shim is mounted within the plenum and configured to be manipulated to adjust the location of the venturi suction tube to thereby adjust the venturi suction pressure;
(b) a fuel pressure modifying mechanism which receives fuel from a supply and delivers said fuel at a pressure different from said supply comprising a fuel regulator and an idle valve;
(c) a fuel metering mechanism; and
(d) an accelerator pump.
6. The fuel injection system of claim 5 where the idle valve comprises an integrated metering jet where there is a flow of liquid through the metering jet and a mechanism to modify the flow through metering jet where:
(a) the metering jet extends axially from the near end of a barrel valve and rotatably mates with a sleeve valve; where the barrel valve defines a notched hole and the sleeve defines an outlet hole;
(b) where the mechanism to modify the flow through the metering jet comprises a needle valve; where the needle valve rotatably mates with the far end of the barrel valve; where the flow through the metering jet is adjusted by extending or contracting the needle valve to or from the far end of the barrel valve.
7. The fuel injection system of claim 6 where the flow through the metering jet is increased by aligning the notched hole and the outlet hole.
8. The fuel injection system of claim 6 where the needle valve is rotated into the barrel valve by a screw; where the flow through the metering jet is decreased by rotating the needle valve into the barrel valve.
9. The fuel injection system of claim 6 where said accelerator pump comprises a fuel reservoir.
10. The fuel injection system of claim 9 where said fuel reservoir empties when an increase of differential pressure creates a sudden drop in metered fuel pressure.
11. The fuel injection system of claim 10 where said fuel reservoir fills when the throttle valve is still or closing and the amount of metered fuel pressure stabilizes.