US4714067A
Expired / Lapsed
US
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Electronic fuel injection circuit with altitude compensation
Assignee: Brunswick Corp
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Filing: 1986-12-23
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Granted: 1987-12-22
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Expires: 2006-12-23
Abstract
Abstract A resistance switching circuit is toggled immediately prior to cranking but subsequent to power application by the output of a manifold absolute pressure sensor effectively responding to ambient atmospheric pressure as indicative of altitude. The switching circuit is connected in series with the resistance element of the potentiometer which serves as the throttle control and alters the transfer characteristic of the control circuit. The gain of the system is such that the output operational amplifier saturates at an intermediate throttle setting such that the response for slow throttle is y=nx over the entire range of manifold pressure, while for fast throttle the response is y=nx for low manifold pressure and changes to y=mx+b for higher manifold pressure.
Inventors
- 👤 Richard E. Staerzl
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 03:51
CPC Classifications
F; F02; F02D; F02D41/00; F02D41/24; F02D41/26; F02D41/28; F02D41/02; F02D41/04
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
86 words
In an electronic fuel-injection control circuit for an internal-combustion engine, wherein a manifold absolute pressure sensor and a manifold absolute temperature sensor feed signals through a combining network to the resistance element of a potentiometer having a variable tap from which a control voltage is derived as a function of desired throttle setting, the improvement wherein compensation means are provided coupled to said potentiometer for altering the relationship between said control voltage and said manifold absolute pressure sensor signal as a function of ambient atmospheric pressure.
Claim 2
Dependent Claim
86 words
In an electronic fuel-injection control circuit for an internal-combustion engine, wherein a manifold absolute pressure sensor and a manifold absolute temperature sensor feed signals through a combining network to the resistance element of a potentiometer having a variable tap from which a control voltage is derived as a function of desired throttle setting, the improvement wherein compensation means are provided coupled to said potentiometer for altering the relationship between said control voltage and said manifold absolute pressure sensor signal as a function of ambient atmospheric pressure.
Claim 3
Dependent Claim
29 words
An electronic fuel-injection control circuit according to claim 1, wherein said compensation means comprises a circuit connected to both said manifold absolute pressure sensor and said potentiometer resistance element.
Claim 4
Dependent Claim
57 words
An electronic fuel-injection control circuit according to claim 1, wherein said compensation means comprises means coupled to said manifold absolute pressure sensor and said potentiometer resistance element for increasing the slope of the response curve relating output signal voltage to manifold absolute pressure signal, said slope being increased in proportion to decrease in said ambient atmospheric pressure.
Claim 5
Dependent Claim
56 words
An electronic fuel-injection control circuit according to claim 3, wherein said slope increasing means is related to said combining network such that for small throttle settings said response curve is a substantially straight line of constant slope over the entire range of manifold absolute pressure sensed by said sensor, said slope being directly proportional to altitude.
Claim 6
Dependent Claim
132 words
An electronic fuel-injection control circuit according to claim 4, wherein said slope increasing means is related to said combining network such that for throttle settings in excess of some intermediate setting said response curve comprises a first part operative for low manifold absolute pressure signals and a second part operative for manifold absolute pressure signals above a predetermined value, said second part following a substantially straight line corresponding to y=mx+b where y is said control voltage, x is said manifold absolute pressure signal, and b is the intercept on the y axis, b and m being substantially constant over the range of altitude compensation, and said first part following a substantially straight line corresponding to y=nx where y and x are as previously defined and n varies as a function of altitude.
Claim 7
Dependent Claim
25 words
An electronic fuel-injection control circuit according to claim 5, wherein said slope increasing means comprises means for altering n stepwise as a function of altitude.
Claim 8
Dependent Claim
32 words
An electronic fuel-injection control circuit according to claim 6, wherein said slope stepwise altering means comprises means responsive to the manifold absolute pressure signal at the instant immediately prior to engine cranking.
Claim 9
Dependent Claim
64 words
An electronic fuel-injection control circuit according to claim 1, wherein said compensation means comprises a variable resistance network connected in series with said potentiometer resistance element between the latter and a point of reference potential, and means for selecting the resistance of said resistance network from a range of resistance as a function of the manifold absolute pressure existing immediately prior to engine cranking.
Claim 10
Dependent Claim
92 words
An electronic fuel-injection control circuit according to claim 8, wherein said variable resistance network comprises a plurality of resistors each in series with a separate voltage controlled switch, the plurality of resistors each having a terminal remote from the corresponding voltage controlled switch which terminals are connected together and to an end of said potentiometer resistance element, a separate voltage comparator circuit coupled in controlling relation to each voltage controlled switch, and an ignition switch controlled sampling circuit interconnecting said manifold absolute pressure sensor with an input of each said comparator circuit.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-12-21 | 1991-06-22 | 1991-12-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-12-21 | 1995-06-22 | 1995-12-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-12-21 | 1999-06-22 | 1999-12-22 | $7700.00 | Window Closed / Lapsed |