Intake bypass for liquid fuel engine

US11549451B1 · US · B1

Patent metadata
FieldValue
Publication numberUS-11549451-B1
Application numberUS-202217660794-A
CountryUS
Kind codeB1
Filing dateApr 26, 2022
Priority dateApr 26, 2022
Publication dateJan 10, 2023
Grant dateJan 10, 2023

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A fuel supply system for an internal combustion engine includes an air compressor, an air cooler connected downstream of the air compressor and the compressed air supply passage, and a bypass passage connected downstream of the air compressor. The fuel supply system also includes a fuel injector secured to the compressed air supply passage or secured to the bypass passage and a valve connected between the air compressor and the air cooler, the valve being configured to block a flow of intake air to the air cooler, causing the intake air to flow to the bypass passage or to permit the flow of intake air to the air cooler.

First claim

Opening claim text (preview).

What is claimed is: 1. A fuel supply system for an internal combustion engine, the fuel supply system comprising: an air compressor; a compressed air supply passage connected downstream of the air compressor; an air cooler connected downstream of the air compressor and the compressed air supply passage; a bypass passage connected downstream of the air compressor; a fuel injector secured to the compressed air supply passage or secured to the bypass passage; and a valve connected between the air compressor and the air cooler, the valve being configured to block a flow of intake air to the air cooler, causing the intake air to flow to the bypass passage or to permit the flow of intake air to the air cooler. 2. The fuel supply system of claim 1 , wherein the valve includes an inlet opening connected between the air compressor and the air cooler and an outlet connected between the inlet and the air cooler. 3. The fuel supply system of claim 2 , wherein the valve further includes an additional outlet connected between the inlet and the bypass passage. 4. The fuel supply system of claim 1 , wherein the fuel injector is connected upstream of the air cooler. 5. The fuel supply system of claim 1 , wherein the fuel injector is secured to the bypass passage. 6. The fuel supply system of claim 1 , further including an additional fuel injector configured to inject fuel directly into a cylinder of the internal combustion engine. 7. The fuel supply system of claim 6 , wherein the fuel injector secured to the compressed air supply passage is configured to inject a liquid fuel that is different than a fuel injected by the additional fuel injector. 8. A fuel supply system, comprising: an internal combustion engine; an air compressor configured to compress air received by the internal combustion engine; a compressed air supply passage connected downstream of the air compressor; an air cooler for reducing a temperature of the compressed air; a compressed air bypass passage connected downstream of the air compressor; a fuel injector secured to the compressed air supply passage or secured to the compressed air bypass passage; a bypass valve having a bypass position configured to cause at least a portion of the compressed air to bypass the air cooler; and an electronic control module configured to generate a command to cause the bypass valve to enter the bypass position. 9. The fuel supply system of claim 8 , further comprising a sensor system including at least one sensor configured to generate a signal that is received with the electronic control module for determining when to generate the command to cause the bypass valve to enter the bypass position. 10. The fuel supply system of claim 9 , wherein the at least one sensor includes an intake air pressure sensor, an intake air temperature sensor, an intake air flow sensor, an engine speed sensor, or a turbocharger speed sensor. 11. The fuel supply system of claim 10 , wherein the engine control module is configured to generate the command to cause the bypass valve to enter the bypass position based a sensed intake air temperature or a sensed intake air pressure. 12. The fuel supply system of claim 8 , wherein, when the bypass valve is in the bypass position, a path of fuel to the internal combustion engine from the fuel injector is lengthened. 13. A fuel supply method for supplying fuel to an internal combustion engine, the method comprising: compressing air with an air compressor; injecting fuel into the compressed air at a location upstream of an intake plenum to form a fuel and air mixture, the intake plenum being a portion of an intake manifold having a plurality of runners extending from the intake plenum toward the internal combustion engine; causing at least some compressed air to bypass an air cooler; supplying the air and fuel mixture to the internal combustion engine; and combusting the air and fuel mixture within the internal combustion engine. 14. The fuel supply method of claim 13 , wherein the fuel is injected upstream of the air cooler. 15. The fuel supply method of claim 13 , wherein the fuel is injected in a passage that bypasses the air cooler. 16. The fuel supply method of claim 13 , wherein the fuel includes at least 50% alcohol, by volume. 17. The fuel supply method of claim 13 , further including controlling a bypass valve to cause at least some of the air and fuel mixture to bypass the air cooler. 18. The fuel supply method of claim 17 , further including generating a command to control the bypass valve that causes a first portion of the air and fuel mixture to bypass the air cooler and a second portion of the air and fuel mixture to enter the air cooler. 19. The fuel supply method of claim 13 , wherein the fuel is methanol. 20. The fuel supply method of claim 13 , wherein the compressed air, when bypassing the air cooler, travels a greater distance to the internal combustion engine as compared to compressed air that does not bypass the air cooler.

Assignees

Inventors

Classifications

  • simultaneously using pluralities of fuels (F02D19/12 takes precedence) · CPC title

  • Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures · CPC title

  • Intake manifold pressure · CPC title

  • the injection nozzle opening into the air intake conduit · CPC title

  • Arrangement of fuel supply systems on engines or vehicle bodies; Components of the fuel supply system being combined with another device · CPC title

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What does patent US11549451B1 cover?
A fuel supply system for an internal combustion engine includes an air compressor, an air cooler connected downstream of the air compressor and the compressed air supply passage, and a bypass passage connected downstream of the air compressor. The fuel supply system also includes a fuel injector secured to the compressed air supply passage or secured to the bypass passage and a valve connected …
Who is the assignee on this patent?
Caterpillar Inc
What technology area does this patent fall under?
Primary CPC classification F02D41/0007. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 10 2023 00:00:00 GMT+0000 (Coordinated Universal Time) (B1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).