US 6,000,384 AGranted

Method for balancing the air/fuel ratio to each cylinder of an engine

AssigneeCaterpillar Inc.

InventorsScott C. Brown, Martin L. Willi

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Abstract

A method for controlling delivery of fuel to each cylinder of an engine by adjusting the appropriate fuel valve duration times to each such cylinder based upon either a desired cylinder exhaust port temperature, or a predetermined detonation level. By using the exhaust port temperature measurements and/or detonation level measurements from each individual cylinder as a controlling parameter, the delivery of fuel to that particular cylinder can be trimmed to achieve the desired exhaust port temperature and/or predetermined detonation level. Balancing the exhaust port temperature and/or detonation level for each such cylinder to a common desired exhaust port temperature and/or detonation level likewise produces a substantially identical air/fuel ratio in each such cylinder. Both the exhaust port temperature control loop and the detonation control loop can be initiated at predetermined intervals so as to continuously maintain a balanced air/fuel ratio to each cylinder in any particular engine and, in certain situations, both control loops can operate simultaneously with respect to any particular cylinder.

Claims3

Dependent claims

A method for controlling the delivery of fuel to each cylinder associated with a dual fuel engine operating in a dual fuel mode wherein each cylinder includes at least one associated gaseous fuel admission valve, the method comprising the steps of:

(a) selecting one of the cylinders of said dual fuel engine;
(b) sensing an actual exhaust port temperature for said selected cylinder;
(c) comparing the actual exhaust port temperature of step (b) to a desired exhaust port temperature;
(d) determining a first control signal duration trim value based upon the comparison of step (c);
(e) sensing an actual detonation level for said selected cylinder;
(f) comparing the actual detonation level of step (e) to a predetermined detonation level;
(g) determining a second control signal duration trim value based upon the comparison of step (f);
(h) comparing the first control signal duration trim value determined at step (d) with the second control signal duration trim value determined at step (g) and selecting one of said compared control signal duration trim values;
(i) applying the control signal duration trim value selected at step (h) to a determined gaseous fuel admission valve control signal duration for said selected cylinder to establish a trimmed gaseous fuel admission valve control signal duration;
(j) delivering fuel to said selected cylinder utilizing a gaseous fuel admission valve control signal having the trimmed gaseous fuel admission valve control signal duration of step (i);
and
(k) controlling the delivery of fuel to each of the remaining cylinders of the dual fuel engine in accordance with steps (a) through (j) for each successive cylinder.

9 more elements

Dependencies are inferred from the claim text.

Facts

Application: 09/036,348Filed 6 Mar 1998
Granted: 14 Dec 1999
Term ends: Not estimatedThe source records don’t support an estimate.

Classification11 codes

F02D 41/0085
Controlling each cylinder individually: balancing of cylinder outputs, e.g. speed, torque or air-fuel ratio
F02D 19/061
To adjust the fuel mass or volume flow: by controlling fuel injectors
F02D 19/0631
Determining the fuel pressure, temperature or flow, the fuel tank fill level or a valve position: by estimation, i.e. without using direct…
F02D 19/105
Peculiar to compression-ignition engines in which the main fuel is gaseous: operating in a special mode, e.g. in a liquid fuel only mode for starting