SYSTEM AND METHOD FOR 0N-WING ENGINE TRIM VERIFICATION
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United States of America Patent
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Issued Date -
Aug 28, 2014
app pub date -
Feb 22, 2013
filing date -
Feb 22, 2013
priority date (Note) -
Abandoned
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Abstract
Devices and methods relating to gas turbine engines and engine temperature trim verification are disclosed. An exemplary method comprises acquiring signals representing a plurality of engine parameters measured while the engine is operating and determining a recommended trim thermocouple resistance based at least partly on the measured parameters. The engine parameters may comprise at least an engine inlet temperature and an exhaust temperature.
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