Supplemental fuel system for compression-ignition engine
A supplemental fuel system includes a supplemental fuel tank, a first pressure regulator, a second pressure regulator, and a nozzle. The supplemental fuel tank is configured to store a supplemental fuel at a first pressure. The first pressure regulator is configured to reduce the first pressure of the supplemental fuel received from the supplemental fuel tank to a second pressure. The second pressure regulator is configured to reduce the second pressure of the supplemental fuel received from the first pressure regulator to a third pressure. The nozzle is configured to be positioned (i) downstream of the second pressure regulator and (ii) within a conduit of an air supply system for the compression-ignition engine. The nozzle is configured to receive a flow of the supplemental fuel and provide the supplemental fuel to air flowing though the conduit.
1. A supplemental fuel system for a machine having a compression-ignition engine, the supplemental fuel system comprising:
a supplemental fuel tank configured to store a supplemental fuel at a first pressure, the supplemental fuel configured to supplement a primary fuel used by the compression-ignition engine;
a first pressure regulator configured to be positioned downstream of the supplemental fuel tank, the first pressure regulator configured to reduce the first pressure of the supplemental fuel received from the supplemental fuel tank to a second pressure;
a second pressure regulator configured to be positioned downstream of the first pressure regulator, the second pressure regulator configured to reduce the second pressure of the supplemental fuel received from the first pressure regulator to a third pressure;
a nozzle configured to be positioned (i) downstream of the second pressure regulator and (ii) within a conduit of an air supply system for the compression-ignition engine, the nozzle configured to receive a flow of the supplemental fuel and provide the supplemental fuel to air flowing though the conduit, wherein the nozzle has a body defining a first inlet positioned at a first nozzle end thereof, an outlet positioned at an opposing second nozzle end thereof, a second inlet positioned between the first nozzle end and the opposing second nozzle end, and a nozzle passage extending from the first nozzle end to the opposing second nozzle end that is configured to receive the air flowing through the conduit;
a stem having a first stem end and a second stem end, the first stem end interfacing with the second inlet, the stem configured to extend through a wall of the conduit such that the second stem end is positioned outside of the conduit, the stem configured to receive the flow of the supplemental fuel from the second pressure regulator and provide the flow of the supplemental fuel to the nozzle passage of the nozzle through the second inlet;
a pair of seals configured to be positioned at opposing sides of an interface where the stem extends through the wall of the conduit;
a pair of fasteners configured to compress the pair of seals against the interface to provide an air-tight seal at the interface;
an electronic lock off valve configured to be positioned between the supplemental fuel tank and the nozzle; and
a controller configured to control the electronic lock off valve to selectively disengage the supplemental fuel system and prevent the supplemental fuel from being provided to the air flowing through the conduit.
2. The supplemental fuel system of claim 1 , further comprising the conduit, wherein the conduit is an air intake tube.
3. The supplemental fuel system of claim 1 , wherein the nozzle is configured to be positioned within the conduit between an air intake and a turbocharger of the air supply system.
4. The supplemental fuel system of claim 1 , wherein the supplemental fuel tank is configured to store the supplemental fuel as a compressed, gaseous fuel.
5. The supplemental fuel system of claim 1 , wherein the electronic lock off valve is configured to be positioned between the first pressure regulator and the second pressure regulator.
6. The supplemental fuel system of claim 1 , wherein the electronic lock off valve is a first electronic lock off valve, further comprising a second electronic lock off valve configured to be positioned downstream of the first electronic lock off valve and upstream of the nozzle.
7. The supplemental fuel system of claim 1 , further comprising a user interface configured to receive a user input from an operator, wherein the controller is configured to control the electronic lock off valve based on the user input.
8. The supplemental fuel system of claim 7 , wherein the controller is configured to control the user interface to provide an indication to the operator regarding an operating characteristic of the supplemental fuel system.
9. The supplemental fuel system of claim 1 , further comprising a sensor configured to acquire data regarding operation of at least one of the supplemental fuel system or the machine, wherein the controller is configured to control the electronic lock off valve to at least one of automatically engage or automatically disengage the supplemental fuel system based on the data.
10. The supplemental fuel system of claim 1 , wherein the nozzle has a first cross-sectional dimension that is configured to be less than a second cross-sectional dimension of the conduit such that only a portion of the air flowing through the conduit is configured to flow through the nozzle.
11. The supplemental fuel system of claim 1 , wherein the nozzle is a Venturi nozzle that is configured to generate a vacuum signal at the second pressure regulator as the air flowing through the conduit flows through the nozzle, and wherein the nozzle is configured to receive a flow of the supplemental fuel from the second pressure regulator in response to and based on the vacuum signal.
12. The supplemental fuel system of claim 1 , wherein the nozzle passage has a non-uniform profile including a first transition point, a second transition point, an inlet taper extending from the first nozzle end to the first transition point, a mixing chamber positioned between the first transition point and the second transition point, and an outlet taper extending from the second transition point to the opposing second nozzle end, wherein the inlet taper is different than the outlet taper, and wherein the second inlet is positioned along the mixing chamber.
13. The supplemental fuel system of claim 12 , wherein the second inlet is positioned closer to the second transition point than the first transition point.
14. A supplemental fuel system for a machine having a compression-ignition engine, the supplemental fuel system comprising:
a supplemental fuel tank configured to store a supplemental fuel at a first pressure, the supplemental fuel configured to supplement a primary fuel used by the compression-ignition engine;
a first pressure regulator configured to be positioned downstream of the supplemental fuel tank, the first pressure regulator configured to reduce the first pressure of the supplemental fuel received from the supplemental fuel tank to a second pressure;
a second pressure regulator configured to be positioned downstream of the first pressure regulator, the second pressure regulator configured to reduce the second pressure of the supplemental fuel received from the first pressure regulator to a third pressure;
a nozzle configured to be positioned (i) downstream of the second pressure regulator and (ii) within a conduit of an air supply system for the compression-ignition engine, the nozzle configured to receive a flow of the supplemental fuel and provide the supplemental fuel to air flowing though the conduit, wherein the nozzle has a body defining a first inlet positioned at a first nozzle end thereof, an outlet positioned at an opposing second nozzle end thereof, a second inlet positioned between the first nozzle end and the opposing second nozzle end, and a nozzle passage extending from the first nozzle end to the opposing second nozzle end that is configured to receive the air flowing through the conduit, wherein the nozzle passage has a non-uniform profile including a first transition point, a second transition point, an inlet taper extending from the first nozzle end to the first transition point, a mixing chamber positioned between the first transition point and the second transition point, and an outlet taper extending from the second transition point to the opposing second nozzle end, wherein the inlet taper is different than the outlet taper, wherein the second inlet is positioned along the mixing chamber, wherein the body has a first diameter of about 3 inches, the mixing chamber has a second diameter of about 2 inches, the body has a first length of about 4 inches, the inlet taper has a second length of about 0.5 inches, the mixing chamber has a third length of about 2 inches, and the outlet taper has a fourth length of about 1.5 inches, an electronic lock off valve configured to be positioned between the supplemental fuel tank and the nozzle; and
a controller configured to control the electronic lock off valve to selectively disengage the supplemental fuel system and prevent the supplemental fuel from being provided to the air flowing through the conduit.