METHOD AND APPARATUS FOR PROVIDING FUEL TO AN AIRCRAFT ENGINE
First Claim
1. A method for adjusting a fuel-air ratio for a fuel-air mixture provided to a cylinder assembly of an engine, comprising:
- detecting a set of rich exhaust gas temperature signals corresponding to a set of rich fuel-air ratio values, each of the set of rich fuel-air ratio values having a fuel-air ratio value that is greater than a threshold fuel-air ratio value;
detecting a set of lean exhaust gas temperature signals corresponding to a set of lean fuel-air ratio values, each of the set of lean fuel-air ratio values having a fuel-air ratio value that is less than the threshold fuel-air ratio value;
detecting an intersection between the set of lean exhaust gas temperature signals and the set of rich exhaust gas temperature signals, the intersection associated with an actual peak fuel-air ratio value;
comparing the actual peak fuel-air ratio value with the threshold fuel-air ratio value; and
adjusting the fuel-air ratio in the fuel-air mixture provided to the cylinder assembly based upon the comparison of the actual peak fuel-air ratio value and threshold fuel-air ratio value.
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Accused Products
Abstract
An aircraft engine includes an aircraft engine controller configured to detect an actual peak exhaust gas temperature of a cylinder assembly. The aircraft engine controller detects an intersection between a first function representing a relationship between a set of rich exhaust gas temperature signals and a corresponding set of rich fuel-air ratio values and a second function representing a relationship between a set of lean exhaust gas temperature signals and a set of lean fuel-air ratio values. Based upon the intersection between the first and second functions, the engine controller detects an actual peak fuel-air ratio value for the cylinder assembly and can determine if a correction in the fuel-air ratio of a fuel-air mixture provided to the cylinder assembly is required. Accordingly, the engine controller provides each cylinder assembly of the aircraft engine with an accurate fuel-air mixture to allow for operation of the engine with optimal fuel economy.
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Citations
20 Claims
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1. A method for adjusting a fuel-air ratio for a fuel-air mixture provided to a cylinder assembly of an engine, comprising:
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detecting a set of rich exhaust gas temperature signals corresponding to a set of rich fuel-air ratio values, each of the set of rich fuel-air ratio values having a fuel-air ratio value that is greater than a threshold fuel-air ratio value; detecting a set of lean exhaust gas temperature signals corresponding to a set of lean fuel-air ratio values, each of the set of lean fuel-air ratio values having a fuel-air ratio value that is less than the threshold fuel-air ratio value; detecting an intersection between the set of lean exhaust gas temperature signals and the set of rich exhaust gas temperature signals, the intersection associated with an actual peak fuel-air ratio value; comparing the actual peak fuel-air ratio value with the threshold fuel-air ratio value; and adjusting the fuel-air ratio in the fuel-air mixture provided to the cylinder assembly based upon the comparison of the actual peak fuel-air ratio value and threshold fuel-air ratio value. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An engine control system, comprising:
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an exhaust gas temperature sensor, the exhaust gas temperature sensor configured to generate gas temperature signals associated with a cylinder assembly of an engine; and an engine controller disposed in electrical communication with the exhaust gas temperature sensor, the engine controller being operable to adjust a fuel-air ratio for a fuel-air mixture provided to the cylinder assembly, the engine controller configured to; detect a set of rich exhaust gas temperature signals corresponding to a set of rich fuel-air ratio values, each of the set of rich fuel-air ratio values having a fuel-air ratio value that is greater than a threshold fuel-air ratio value; detect a set of lean exhaust gas temperature signals corresponding to a set of lean fuel-air ratio values, each of the set of lean fuel-air ratio values having a fuel-air ratio value that is less than the threshold fuel-air ratio value; detect an intersection between the set of lean exhaust gas temperature signals and the set of rich exhaust gas temperature signals, the intersection associated with an actual peak fuel-air ratio value; compare the actual peak fuel-air ratio value with the threshold fuel-air ratio value; and adjust the fuel-air ratio in the fuel-air mixture provided to the cylinder assembly based upon the comparison of the actual peak fuel-air ratio value and threshold fuel-air ratio value. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification