Supplemental fuel system for compression-ignition engine
A supplemental fuel system for a machine having a compression-ignition engine includes an air intake tube. The air intake tube has a first end configured to interface with an air cleaner of an air supply system that provides air to the compression-ignition engine, a second end configured to interface with a compressor of a turbocharger of the air supply system, and a sidewall extending between the first end and the second end. The sidewall includes a fuel interface configured to facilitate providing a supplemental fuel into the air intake tube to mix with the air upstream of the compressor of the turbocharger.
1. A supplemental fuel system for a machine having a compression-ignition engine, the supplemental fuel system comprising:
an air intake tube having:
a first end configured to interface with an air cleaner of an air supply system that provides air to the compression-ignition engine;
a second end configured to interface with a compressor of a turbocharger of the air supply system; and
a sidewall extending between the first end and the second end, the sidewall including a fuel interface configured to facilitate providing a supplemental fuel into the air intake tube to mix with the air upstream of the compressor of the turbocharger;
a stem extending through the sidewall and defining the fuel interface, wherein the sidewall defines an aperture through which the stem extends;
a pair of seals positioned at opposing sides of the aperture; and
a pair of fasteners configured to compress the pair of seals against the aperture to provide an air-tight seal between the aperture and the stem.
2. The supplemental fuel system of claim 1 , further comprising a nozzle positioned within the air intake tube, the nozzle defining a fuel inlet that interfaces with the stem.
3. The supplemental fuel system of claim 2 , wherein the nozzle defines an air inlet, an outlet, a nozzle passage extending from the air inlet to the outlet, and the fuel inlet positioned between the air inlet and the outlet.
4. The supplemental fuel system of claim 3 , wherein the nozzle has a first cross-sectional dimension that is less than a second cross-sectional dimension of the air intake tube such that (i) a first portion of the air flowing through the air intake tube flows through the nozzle passage and (ii) a second portion of the air flowing through the air intake tube flows around the nozzle.
5. The supplemental fuel system of claim 4 , wherein the nozzle is configured to generate a vacuum signal at the fuel inlet as the first portion of the air flows through the nozzle passage, and wherein the stem and, thereby, the nozzle is configured to receive a flow of the supplemental fuel in response to and based on the vacuum signal.
6. The supplemental fuel system of claim 5 , further comprising:
a supplemental fuel tank configured to store the supplemental fuel; and
a pressure regulator positioned downstream of the supplemental fuel tank and upstream of the stem, the pressure regulator configured to reduce a pressure of the supplemental fuel received from the supplemental fuel tank from a first pressure to a second pressure.
7. The supplemental fuel system of claim 6 , wherein the supplemental fuel tank is configured to store the supplemental fuel as a compressed, gaseous fuel.
8. The supplemental fuel system of claim 6 , wherein the pressure regulator is a first pressure regulator, further comprising a second pressure regulator positioned downstream of the first pressure regulator and upstream of the stem, and wherein the second pressure regulator is configured to reduce the pressure of the supplemental fuel received from the first pressure regulator from the second pressure to a third pressure.
9. The supplemental fuel system of claim 8 , further comprising a valve assembly including (i) a valve body defining a valve body inlet and a valve body outlet and (ii) an adjuster, the valve body outlet interfacing with the stem, the adjuster positioned to facilitate selectively restricting an amount of the flow of the supplemental fuel through the valve body outlet and provided to the stem and the nozzle.
10. A supplemental fuel system for a machine having a compression-ignition engine, the supplemental fuel system comprising:
an air intake tube having:
a first end configured to interface with an air cleaner of an air supply system that provides air to the compression-ignition engine;
a second end configured to interface with a compressor of a turbocharger of the air supply system; and
a sidewall extending between the first end and the second end, the sidewall including a fuel interface configured to facilitate providing a supplemental fuel into the air intake tube to mix with the air upstream of the compressor of the turbocharger;
a stem extending through the sidewall and defining the fuel interface;
a nozzle positioned within the air intake tube, the nozzle defining a fuel inlet that interfaces with the stem, wherein the nozzle defines an air inlet, an outlet, a nozzle passage extending from the air inlet to the outlet, and the fuel inlet positioned between the air inlet and the outlet, wherein the nozzle has a first cross-sectional dimension that is less than a second cross-sectional dimension of the air intake tube such that (i) a first portion of the air flowing through the air intake tube flows through the nozzle passage and (ii) a second portion of the air flowing through the air intake tube flows around the nozzle, wherein the nozzle is configured to generate a vacuum signal at the fuel inlet as the first portion of the air flows through the nozzle passage, and wherein the stem and, thereby, the nozzle is configured to receive a flow of the supplemental fuel in response to and based on the vacuum signal;
a supplemental fuel tank configured to store the supplemental fuel; and
a first pressure regulator positioned downstream of the supplemental fuel tank and upstream of the stem, the first pressure regulator configured to reduce a pressure of the supplemental fuel received from the supplemental fuel tank from a first pressure to a second pressure;
a second pressure regulator positioned downstream of the first pressure regulator and upstream of the stem, wherein the second pressure regulator is configured to reduce the pressure of the supplemental fuel received from the first pressure regulator from the second pressure to a third pressure;
a valve assembly including (i) a valve body defining a valve body inlet and a valve body outlet and (ii) an adjuster, the valve body outlet interfacing with the stem, the adjuster positioned to facilitate selectively restricting an amount of the flow of the supplemental fuel through the valve body outlet and provided to the stem and the nozzle;
an electronic lock off valve positioned between the supplemental fuel tank and the valve body; and
a controller configured to control the electronic lock off valve to selectively prevent the supplemental fuel from being provided to the nozzle.
11. A supplemental fuel system for a machine having a compression-ignition engine, the supplemental fuel system comprising:
an air intake tube having:
a first end configured to interface with an air cleaner of an air supply system that provides air to the compression-ignition engine;
a second end configured to interface with a compressor of a turbocharger of the air supply system; and
a sidewall extending between the first end and the second end, the sidewall including a fuel interface configured to facilitate providing a supplemental fuel into the air intake tube to mix with the air upstream of the compressor of the turbocharger;
a stem extending through the sidewall and defining the fuel interface; and
a nozzle positioned within the air intake tube, the nozzle defining a fuel inlet that interfaces with the stem, wherein the nozzle defines an air inlet, an outlet, a nozzle passage extending from the air inlet to the outlet, and the fuel inlet positioned between the air inlet and the outlet, wherein the nozzle has a first cross-sectional dimension that is less than a second cross-sectional dimension of the air intake tube such that (i) a first portion of the air flowing through the air intake tube flows through the nozzle passage and (ii) a second portion of the air flowing through the air intake tube flows around the nozzle, wherein the nozzle is configured to generate a vacuum signal at the fuel inlet as the first portion of the air flows through the nozzle passage, wherein the stem and, thereby, the nozzle is configured to receive a flow of the supplemental fuel in response to and based on the vacuum signal, wherein the nozzle passage has a non-uniform profile that includes a first transition point, a second transition point, an inlet taper extending from the air inlet 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 outlet, and wherein the inlet taper is different than the outlet taper.
12. The supplemental fuel system of claim 11 , wherein the inlet taper has a first longitudinal length and the outlet taper has a second longitudinal length, and wherein a ratio of second longitudinal length to the first longitudinal length is greater than 1:1.
13. The supplemental fuel system of claim 12 , wherein the ratio is about 3:1.
14. The supplemental fuel system of claim 11 , wherein the fuel inlet is positioned along the mixing chamber closer to the second transition point than the first transition point.
15. A supplemental fuel system for a machine having a compression- ignition engine, the supplemental fuel system comprising:
an air intake tube having:
a first end configured to interface with an air cleaner of an air supply system that provides air to the compression-ignition engine;
a second end configured to interface with a compressor of a turbocharger of the air supply system; and
a sidewall extending between the first end and the second end;
a stem extending through the sidewall between the first end and the second end, the stem configured to couple to a supplemental fuel source; and
a nozzle positioned within the air intake tube;
wherein the nozzle defines a nozzle passage that has an air inlet, an outlet, a first transition point, a second transition point, an inlet taper extending from the air inlet to the first transition point, a mixing chamber positioned between the first transition point and the second transition point, an outlet taper extending from the second transition point to the outlet, and a fuel inlet positioned along the mixing chamber and that interfaces with the stem;
wherein the nozzle has an outer diameter of about 3 inches, the mixing chamber has a chamber diameter of about 2 inches, the nozzle has a nozzle length of about 4 inches, the inlet taper has an inlet length of about 0.5 inches, the mixing chamber has a chamber length of about 2 inches, and the outlet taper has an outlet length of about 1.5 inches;
wherein the outer diameter is less than a cross-sectional dimension of the air intake tube such that (i) a first portion of the air flowing through the air intake tube flows through the nozzle passage and (ii) a second portion of the air flowing through the air intake tube flows around the nozzle; and
wherein the nozzle configured to generate a vacuum signal at the fuel inlet as the first portion of the air flows through the nozzle passage to facilitate drawing a supplemental fuel from the supplemental fuel source into the air intake tube to mix with the air upstream of the compressor of the turbocharger.