System for correction of the fuel injection time, upon variations in altitude, for a heat engine having an electronic injection system

• US 4,831,537 A
• Filed: 09/12/1986
• Issued: 05/16/1989
• Est. Priority Date: 09/20/1985
• Status: Expired due to Term

• Current Assignee: Weber SRL
• Original Assignee: Weber SRL
• Inventors: Scarnera, Michele, Francia, Paolo
• Primary Examiner(s): Gruber, Felix D.
• Assistant Examiner(s): TRANS, VINCENT N
• Application Number:
  US06/907,308
• Time in Patent Office: 977 Days
• Field of Search: 364/431.05, 364/558, 123/478, 123/427, 123/480, 123/357, 123/488, 123/412
• US Class Current: 701/105
• CPC Class Codes: F02D 31/005 by controlling a throttle by-pass
• CPC Class Codes: F02D 41/04 Introducing corrections for particular operating conditions F02D41/14 takes precedence

Abstract

A system for correction of the fuel injection time control upon variation in altitude, for a heat engine having an electronic fuel injection system, and having means for substantially detecting the value of the external atmospheric pressure and the consequently correcting the value of induction air pressure utilized by a central processing unit of the injection system for calculating the injection time.

Claims

1. A system for altitude-dependent automatic correction of the fuel injection time of an electronic fuel injection (EFI) system of a heat engine, comprising:

an accelerator;

an air supply valve to said engine controlled by said accelerator to open to a variable angular value;

a pressure sensor for detecting induction air pressure (IAP) value of said engine;

a speed sensor for detecting engine speed;

a central processing unit (CPU) in said EFI system utilizing a corrected IAP value for calcuation of said fuel injection time; and

means for correcting said IAP value;

comprising;

means for detecting operating conditions of said engine when said IAP value is substantially equal to the external atmospheric pressure and for consequently enabling second means for calculating a correction factor for determination of said correct IAP value, said means including;

(a) means detecting the operating condition of said engine upon start-up and enabling said second means when the speed of the engine is less than a first predetermined value and the measured IAP value is less than a predetermined upper limit;

(b) means detecting the operating condition of said engine under a first, full load, dynamic running condition and enabling said second means when not enabled at start-up (a) when the speed of the engine lies within a first predetermined range and said air supply valve is open to at least a first predetermined angular value;

(c) means detecting the operating conditions of said engine under a second dynamic running condition and enabling said second means when not enabled at start-up (a) or full load (b) when the speed of the engine lies within a second predetermined range and said air supply valve is opened to at least a second predetermined angular value;

wherein said second means utilizes an IAP value detected by said pressure sensor in calculating said correction factor.

2. The invention according to claim 1, wherein said second means comprises means for determining said correction factor in dependence upon the displacement of said external air pressure value substantially from sea level pressure, and in dependence upon the compression ratio of said engine, said second means adding said correction factor to said IAP value to determine the necessary enrichment of the fuel mixture of said engine.

3. The invention according to claim 1, wherein said detecting said correcting means are incorporated in said engine CPU.