Electro-thermal pulsed fuel injector and system

• US 5,165,373 A
• Filed: 05/24/1991
• Issued: 11/24/1992
• Est. Priority Date: 05/24/1991
• Status: Expired due to Fees

• Current Assignee: Dah Y. Cheng
• Original Assignee: Dah Y. Cheng
• Inventors: Cheng, Dah Y.
• Primary Examiner(s): ARGENBRIGHT, TONY MICHAEL
• Application Number:
  US07/705,501
• Time in Patent Office: 550 Days
• Field of Search: 123/294, 123/299, 123/300, 239/5, 239/13, 417/207, 417/208, 417/209
• US Class Current: 123/300
• CPC Class Codes: F02B 1/04 with fuel-air mixture admission into cylinder
• CPC Class Codes: F02D 41/2096 for controlling piezoelectric injectors drive and control circuit for piezoelectric devices in general H10N30/802
• CPC Class Codes: F02D 41/30 Controlling fuel injection F02D41/182, F02D41/24 take precedence
• CPC Class Codes: F02M 45/02 with each cyclic delivery being separated into two or more parts
• CPC Class Codes: F02M 45/04 with a small initial part , e.g. initial part for partial load and initial and main part for full load
• CPC Class Codes: F02M 51/00 Fuel-injection apparatus characterised by being operated electrically
• CPC Class Codes: F02M 53/00 Fuel-injection apparatus characterised by having heating, cooling or thermally-insulating means
• CPC Class Codes: F02M 53/06 with fuel-heating means, e.g. for vaporising

Abstract

A concept of pulse input thermal energy to induce a rapid volume change in a vessel is introduced to provide rapid pressure raise as a means to inject fuel into internal combustion engines. A computer and sensor means are incorporated to provide pulse width, height and multiple pulse using engine conditions such as RPM, exhaust pollution and efficiency, etc. as control parameters.

Claims

1. A fuel injection system for delivering fuel to an internal combustion engine at a rate matching engine needs for substantially constant pressure combustion, said engine having a rotary crank and engine sensors, and said fuel injection system comprising:

a supply of liquid fuel;

a source of electrical pulses having selected shapes and occurring at a selected timing;

heating means coupled to receive said pulses and responsive to each received pulse to electrically heat said liquid fuel rapidly to thereby temporarily and locally change the liquid fuel to vapor and cause a corresponding temporary pressure rise;

means utilizing at least in part pressure rise for delivering fuel under pressure to said internal combustion engine.

means for controlling said source of electrical pulses to cause the delivery of a plurality of said electrical pulses to the heating means per combustion cycle of said engine, at a timing matching fuel flow needs for constant pressure combustion; and

engine sensors and means coupled to said controlling means and to said sensors and said rotary crank to detect crank angle position and supply information respecting said sensors and said crank position to the controlling means to help time said train of pulses relative to combustion cycles.

2. A fuel injection system as in claim 1, wherein the heating means comprises a heating element in the form of a thin platinum wire.

3. A fuel injection system as in claim 1, wherein the heating means comprises a heating element made of a high temperature metal or its alloy.

4. A fuel injection system as in claim 1, wherein the controlling means comprises a programmed computer and means to monitor said sensors and thereby the condition of the engine and feed information thereon back to said computer.

5. A method of delivering fuel to an internal combustion engine by fuel injection at a rate matching fuel needs of the engine for substantially constant pressure combustion, comprising:

generating a succession of a short duration pressure pulses in a liquid fuel line for each combustion cycle of the engine by alternate rapid heating a small portion of the fuel to vapor and allowing the vapor to at least partially collapse in response to each of said pulses; and

controlling said short duration pressure pulses relative to the TDC of combustion chambers of said engine for each combustion cycle to match fuel needs of the engine for substantially constant pressure combustion.

6. A method as in claim 5, including using check valves to help control the pressure pulse shape of said pressure pulses and utilizing the vapor collapse in the fuel line between said pressure pulses for quickly cutting off fuel flow to the engine.

7. A fuel injection system for supplying fuel for substantially constant pressure combustion in an internal combustion engine having at least one combustion chamber, comprising:

a fuel tank for liquid fuel, a fuel intake line supplied with liquid fuel from the fuel tank, a pump receiving fuel from the fuel intake line and delivering the received fuel to an outlet line at a raised pressure, pressure regulator means coupled to said outlet line to regulate the fuel pressure therein, a check valve, a high pressure fuel line coupled to the outlet line through said check valve to receive fuel therefrom, said check valve providing for one way flow only of fuel from the outlet line to the high pressure line;

an electro-thermal unit in said pressure line, a fuel nozzle coupled with the pressure line downstream from the electro-thermal unit, and another check valve which is between the electro-thermal unit and the fuel nozzle to provide one way flow into the fuel nozzle;

an energy network coupled with the electro-thermal unit to deliver energy pulses thereto, said electro-thermal unit responding to each energy pulse to rapidly heat and locally and temporarily vaporize fuel and thereby cause a fuel pulse to be delivered through said another check valve to said nozzle;

a programmed computer coupled to the energy delivery network to control the delivery of energy pulses to the electro-thermal unit to cause the electro-thermal unit to deliver a number of fuel pulses to each combustion chamber of the engine for each combustion cycle;

a crank position sensor, an RPM detector and at least one other sensor coupled to the computer and to the engine to derive information regarding engine requirements and supply said information to the computer for use in controlling the delivery of energy pulses to the electro-thermal unit; and

said computer controlling the delivery of said energy pulses to the electro-thermal unit to cause the delivery of fuel pulses matching engine needs for substantially constant pressure combustion.

8. A method of using an electro-thermal fuel injection system comprising operating the fuel injection system for each combustion cycle and each combustion chamber to:

first inject into the combustion chamber a relatively minor amount of fuel to establish a pilot flame; and

thereafter inject into the combustion chamber a relatively major amount of fuel as a sequence of fuel pulses arranged to match fuel needs for substantially constant pressure combustion.

9. A method of using an electro-thermal fuel injection system as in claim 8, including energizing said system with a sequence of electrical pulses causing the step of injecting a relatively major amount of fuel after the pilot flame to comprise the injection of discrete multiple fuel pulses for each combustion cycle, each fuel pulse corresponding to a respective one of said electrical pulses.

10. An electro-thermal pressure pulse generator for supplying a sequence of fuel pulses per combustion cycle for each combustion chamber of an internal combustion engine, comprising:

a high pressure fuel line supplying fuel to the engine;

a source of electrical energy pulses;

an electro-thermal fuel pulse generating device in line with said high pressure fuel line and responsive to each energy pulse to generate a respective fuel pulse for delivery to said engine;

a control coupled with the fuel pulse generating device to control the delivery of said energy pulses thereto and thereby the delivery of said fuel pulses to the engine to cause each combustion chamber in the engine to receive for each combustion cycle a plurality of fuel pulses delivering fuel at a rate matching fuel needs for substantially constant pressure combustion.

11. An electro-thermal pressure pulse generator as in claim 10, wherein the electro-thermal device comprises a material inserted in the fuel flow through said high pressure high and selected from the group consisting of:

(i) an electrically conductive thin film attached to an electrically insulating material wall, (ii) a length of an electrically conductive thin wall conduit enclosed by said high pressure line and spaced therefrom by an electrically insulating material, and (iii) a length of an electrically conductive wire or strip.