Apparatus for monitoring gas turbine engine operation
First Claim
1. A method for identifying trends in engine operation, the engine having a plurality of sensors responsive to engine operations, said method comprising the steps of:
- obtaining outputs from at least some of the sensors when the engine is operating;
obtaining ambient flight condition data; and
generating normalized engine trend parameters using the engine sensor data and ambient flight condition data.
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Accused Products
Abstract
A model-based trending process for a gas turbine engine that generates, in real-time, engine trend parameters from engine sensor data and ambient flight condition data to assess engine condition is described. The engine includes a plurality of sensors that are responsive to engine operations. The trending process is implemented using a commercially available processor coupled to the engine to monitor the engine operations, and having the desired processing speed and capacity. Engine health parameters are estimated and adjusted in a model for component diagnostics and fault detection and isolation. The trend parameters generated are retained.
19 Citations
19 Claims
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1. A method for identifying trends in engine operation, the engine having a plurality of sensors responsive to engine operations, said method comprising the steps of:
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obtaining outputs from at least some of the sensors when the engine is operating;
obtaining ambient flight condition data; and
generating normalized engine trend parameters using the engine sensor data and ambient flight condition data. - View Dependent Claims (2, 3, 4, 5, 6)
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7. Apparatus for trending gas turbine engine operation, the engine having a plurality of sensors responsive to engine operations, said apparatus comprising a processor programmed to:
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obtain engine sensor data and ambient flight condition data; and
generate and normalize engine trend parameters using the engine sensor data and ambient flight condition data. - View Dependent Claims (8, 9, 10, 11, 12, 13, 15, 16, 17, 18, 19)
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14. A trending system for trending operation of a gas turbine engine, the engine having a plurality of sensors responsive to engine operations, said system comprising:
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an engine model unit coupled to receive engine sensor data and ambient flight condition data input from the sensors; and
a processor programmed to generate and normalize engine trend parameters using the engine sensor data and ambient flight condition data obtained.
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Specification