Arrangement for supplying a maximum quantity of fuel

• US 4,572,142 A
• Filed: 11/27/1984
• Issued: 02/25/1986
• Est. Priority Date: 10/02/1982
• Status: Expired due to Term

• Current Assignee: Robert Bosch GmbH
• Original Assignee: Robert Bosch GmbH
• Inventors: Horbelt, Michael, Arnold, Herbert, Dahlke, Gerald
• Primary Examiner(s): Nelli, Raymond A.
• Application Number:
  US06/675,458
• Time in Patent Office: 455 Days
• Field of Search: 123/478, 123/484, 123/485, 123/490, 123/491, 123/179 L, 123/179 G, 123/488
• US Class Current: 123/478
• CPC Class Codes: F02D 2200/703 Atmospheric pressure
• CPC Class Codes: F02D 31/007 controlling fuel supply
• CPC Class Codes: F02D 41/38 of the high pressure type

Abstract

A method of and arrangement for supplying a maximum quantity of fuel which is supplied to a combustion engine in certain operational conditions independent of rate of airflow and rotational speed is provided with an altitude-correcting signal which depends the maximum amount of fuel to be supplied on the air density of the actual operational altitude of the combustion engine. Through the provision of such an altitude-correction signal, a too rich mixture of fuel and air is prevented.

Claims

1. A method of limiting a quantity of fuel to be supplied to a combustion engine of a motor vehicle, comprising the steps of defining in dependency on load and rotary speed a first quantity of fuel to be supplied, determining air density of the surrounding air, determining in dependency on the air density and rotary speed a second quantity of fuel which is a limit for said first quantity, and limiting said first quantity of fuel to be supplied to the engine to said second quantity.

2. A method as defined in claim 1, wherein said determining step includes measuring an instantaneous altitude of a motor vehicle above sea level, said limiting step including reducing the first quantity of fuel to be supplied in correspondence with an increase of the measured instantaneous altitude.

3. A method as defined in claim 1 wherein said defining step is performed independently of the air mass flow in the engine.

4. An arrangement for limiting a quantity of fuel to be supplied to a combustion engine of a motor vehicle, comprising first means for defining in dependency on load and rotary speed, a first quantity of fuel to be supplied to the engine, means for determining air density of surrounding air, second means for defining in dependency on the determined air density, a second quantity of fuel;

and means for limiting the first quantity of fuel to be supplied to the engine to said second quantity of fuel.

5. An arrangement as defined in claim 4, wherein said determining means includes means for measuring an instantaneous altitude of a motor vehicle above the sea level, said limiting means including means for reducing the first quantity of fuel to be supplied in correspondence with an increase of the measured instantaneous altitude.

6. An arrangement as defined in claim 5, wherein said first defining means includes a first circuit for generating an injection impulse of varying duration corresponding to the first quantity of fuel to be supplied, said measuring means including a second circuit for generating an air density impulse whose duration depends on the measured instantaneous altitude, and said limiting means combining said injection impulse with said air density impulse to generate an output injection impulse whose duration depends on the measured instantaneous altitude.

7. An arrangement as defined in claim 6, wherein the measuring means includes an altimeter generating a signal for cooperating with the second circuit so that the maximum amount of supplied fuel is reduced depending on the altitude of the motor vehicle above mean sea level.