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US4953351A Expired / Lapsed US ⏱️ 0.0 years remaining

Combustion control

Assignee: MT Aerospace AG
•
Filing: 1988-11-14
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Granted: 1990-09-04
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Expires: 2008-11-14
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Abstract

Abstract A method for controlling the combustion air ratios for IC engines using a three way catalyst. In known systems the control operation has been impaired by several factors, one being the aging of the lambda probe used for control. In order to allow for such factors the set point of the controller is adjusted under certain conditions or at certain intervals. For the adjustment of the set point the increase in the exhaust gas temperature as caused by the exothermic reaction in the catalyst is measured and employed for establishing a new set point.

Inventors

  • 👤 Karl Motz
  • 👤 Markus Diehl

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 20:50
CPC Classifications
F; F02; F02D; F02D41/00; F02D41/02; F02D41/14; F02D41/1438; F02D41/1444; F02D41/1446; F02D41/1439; F02D41/1441; F02D41/1477; F02D41/1479

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 194 words
A method of automatically controlling the air/fuel ratio of an IC engine having a catalyst, comprising producing a signal representative of air/fuel ratio of a combusted mixture by a lambda probe which samples exhaust gas from an IC engine upstream of the catalyst, measuring exhaust gas temperatures both upstream of the catalyst and after the exhaust gas has passed through at least a portion of the catalyst, determining in a lambda controller on the basis of the measured exhaust gas temperatures and the air/fuel ratio signal from the lambda probe a set point for controlling the air/fuel ratio of the engine, maintaining the engine at a constant load condition while the set point is determined, said determining of said set point being effected by varying the air/fuel ratio of the engine in steps which causes variation in the value of the exhaust gas temperature after the exhaust gas has traveled through at least a portion of said catalyst and establishing the value of the set point for an air/fuel ratio at which the temperature of the exhaust gas after passing through at least a portion of the catalyst is in a maximum temperature range.
Claim 2
Independent Claim 194 words
A method of automatically controlling the air/fuel ratio of an IC engine having a catalyst, comprising producing a signal representative of air/fuel ratio of a combusted mixture by a lambda probe which samples exhaust gas from an IC engine upstream of the catalyst, measuring exhaust gas temperatures both upstream of the catalyst and after the exhaust gas has passed through at least a portion of the catalyst, determining in a lambda controller on the basis of the measured exhaust gas temperatures and the air/fuel ratio signal from the lambda probe a set point for controlling the air/fuel ratio of the engine, maintaining the engine at a constant load condition while the set point is determined, said determining of said set point being effected by varying the air/fuel ratio of the engine in steps which causes variation in the value of the exhaust gas temperature after the exhaust gas has traveled through at least a portion of said catalyst and establishing the value of the set point for an air/fuel ratio at which the temperature of the exhaust gas after passing through at least a portion of the catalyst is in a maximum temperature range.
Claim 3
Dependent Claim 52 words
The method as claimed in claim 1 wherein said varying of the air/fuel ratio results in changing the set point in steps, the value established for the set point being that at which the temperature of the exhaust gas, after passing through at least a portion of the catalyst, is a maximum.
Claim 4
Dependent Claim 85 words
The method as claimed in claim 1 wherein said varying of the air/fuel ratio results in changing the set point in steps, the method further comprising allowing a preset time to elapse after each change of the set point before measuring the temperature of the exhaust gas after its passage through at least a portion of the catalyst and comparing the thus measured temperature with the previous measured temperature for ascertaining the temperature changes as a function of the air/fuel ratio of the combusted mixture.
Claim 5
Dependent Claim 52 words
The method as claimed in claim 3 wherein the value of the set point is established to correspond to the formation of a bend in the curve of temperature of the exhaust gas after passage through at least a portion of the catalyst with respect to air/fuel ratio of the combusted mixture.
Claim 6
Dependent Claim 41 words
The method as claimed in claim 4 comprising changing the value of the set point as determined on the basis of said bend by an empirically predetermined amount as a new set point for further automatic control of the air/fuel ratio.
Claim 7
Dependent Claim 43 words
The method as claimed in claim 3 comprising changing the value of the set point as determined on the basis of the maximum temperature range by an empirically predetermined amount as a new set point for further automatic control of the air/fuel ratio.
Claim 8
Dependent Claim 71 words
The method as claimed in claim 1 wherein said maximum highest temperature range for the establishment of the value of the set point is determined by measuring the difference between the exhaust gas temperature after passage through at least a portion of the catalyst and the exhaust gas temperature upstream from the catalyst, and determining changes in the temperature difference as a function of the air/fuel ratio of the combusted mixture.
Claim 9
Dependent Claim 30 words
The method as claimed in claim 1 wherein the operation of the engine under constant load conditions is monitored by measuring the exhaust gas temperature measured upstream of the catalyst.
Claim 10
Dependent Claim 20 words
The method as claimed in claim 1 wherein the determination of said set point adjustment is performed at predetermined times.

References Cited (Backward Citations)

US3696618A Cited
US3827237A Cited
US4033712A Cited
US4305364A Cited
DE3410930A1 Cited
US4729220A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-09-03 1994-03-05 1994-09-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-09-03 1998-03-05 1998-09-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-09-03 2002-03-05 2002-09-04 $7700.00 Window Closed / Lapsed

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