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US4452207A
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Fuel/air ratio control apparatus for a reciprocating aircraft engine
Assignee: Bendix Corp
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Filing: 1982-07-19
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Granted: 1984-06-05
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Expires: 2002-07-19
Abstract
Abstract A fuel/air ratio control apparatus for a reciprocating engine used in light aircraft including a fuel metering apparatus (32) and a fuel/air ratio controller (40). The controller (40) generates an electrical signal (Wf/Wa) indicative of a desired fuel/air ratio based upon the flight condition of the aircraft and the metering apparatus (32) meters fuel flow (Wf) according to the mass airflow ingested into the engine. The desired fuel/air ratio is a best power ratio (Wf/Wa (2)) for takeoff and climb conditions and a best economy ratio (Wf/Wa (3)) for cruise conditions as derived from the exhaust gas temperature. These ratios are limited by a ratio (Wf/Wa (1)) based upon the maximum cylinder head temperature tolerable for a particular flight condition.
Inventors
- 👤 Robert G. Moore, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 23:10
CPC Classifications
F; F02; F02D; F02D41/00; F02D41/02; F02D41/14; F02D41/1438; F02D41/1444; F02D41/1446
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
238 words
Fuel/air ratio control apparatus for a reciprocating aircraft engine having a cylinder head and generating exhaust gas during engine operation, said apparatus comprising a fuel metering device for regulating fuel flow to the engine as a function of the air flow through the engine and a fuel ratio control signal which varies as a function of a desired fuel/air ratio, and means for generating said fuel ratio control signal, said fuel ratio control signal generating means including exhaust gas temperature sensing means for generating an exhaust gas temperature signal which varies as a function of the temperature of the exhaust gas, first signal generating means for generating a first temperature signal representing an exhaust gas temperature at which optimum power is produced by the engine, second signal generating means for generating a second temperature signal representing an exhaust gas temperature at which optimum fuel economy is obtained from the engine, means for generating a first control signal as a function of the difference between said exhaust gas temperature signal and the first temperature signal, means for generating a second control signal as a function of the difference between said exhaust gas temperature signal and the second temperature signal, means for generating an engine speed signal as a function of the speed of the engine, and means responsive to said engine speed signal for selecting one of said first or second control signals as said fuel ratio control signal.
Claim 2
Dependent Claim
238 words
Fuel/air ratio control apparatus for a reciprocating aircraft engine having a cylinder head and generating exhaust gas during engine operation, said apparatus comprising a fuel metering device for regulating fuel flow to the engine as a function of the air flow through the engine and a fuel ratio control signal which varies as a function of a desired fuel/air ratio, and means for generating said fuel ratio control signal, said fuel ratio control signal generating means including exhaust gas temperature sensing means for generating an exhaust gas temperature signal which varies as a function of the temperature of the exhaust gas, first signal generating means for generating a first temperature signal representing an exhaust gas temperature at which optimum power is produced by the engine, second signal generating means for generating a second temperature signal representing an exhaust gas temperature at which optimum fuel economy is obtained from the engine, means for generating a first control signal as a function of the difference between said exhaust gas temperature signal and the first temperature signal, means for generating a second control signal as a function of the difference between said exhaust gas temperature signal and the second temperature signal, means for generating an engine speed signal as a function of the speed of the engine, and means responsive to said engine speed signal for selecting one of said first or second control signals as said fuel ratio control signal.
Claim 3
Dependent Claim
135 words
Fuel/air ratio control apparatus as claimed in claim 1, and second temperature sensing means for generating a cylinder head temperature signal as a function of the temperature of the cylinder head, means for generating a cylinder head reference signal representing a predetermined maximum cylinder head temperature, means for generating a difference signal which varies as a function of the difference between the cylinder head temperature signal and said cylinder head reference signal, and means for overriding said first control signal generating means and said second control signal generating means to generate said first and second control signals as functions of said difference signal when the valve of the difference signal exceeds the valve of said first or second control signal generated by said first control signal generating means and said second control signal generating means.
Claim 4
Dependent Claim
23 words
Fuel/air ratio control apparatus as claimed in claim 2, wherein said cylinder head reference signal is varied as a function of engine speed.
Claim 5
Dependent Claim
81 words
Fuel/air ratio control apparatus as claimed in claim 3, wherein said engine speed signal generating means includes comparator means for generating a first reference signal when the speed of the engine exceeds a predetermined speed and a second reference signal when the speed of the engine is below said predetermined speed, the cylinder head reference signal being set at a first valve in response to the first reference signal and at a second valve in response to the second reference signal.
Claim 6
Dependent Claim
63 words
Fuel/air ratio control apparatus as claimed in claim 2, wherein said overriding means includes means for selecting the greater of the difference signal and the output of said first control signal generating means as said first control signal, and means for selecting the greater of said difference signal and the output of said second control signal generating means as said second control signal.
Claim 7
Dependent Claim
82 words
Fuel/air control apparatus as claimed in claim 1, wherein said engine speed signal generating means includes comparator means for generating a first reference signal when the speed of the engine exceeds a first predetermined speed and a second reference signal when the speed of the engine is below said predetermined speed, said engine speed signal responsive means selecting said first control signal in response to said first reference signal and selecting said second control signal in response to the second reference signal.
Claim 8
Dependent Claim
41 words
Fuel/air ratio control apparatus as claimed in claim 4, wherein said engine speed signal responsive means selects said first control signal in response to said first reference signal and selects said second control signal in response to the second reference signal.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-06-05 | 1987-12-05 | 1988-06-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-06-05 | 1991-12-05 | 1992-06-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-06-05 | 1995-12-05 | 1996-06-05 | $7700.00 | Window Closed / Lapsed |