SYSTEM AND METHOD FOR GEAR ASSEMBLY LUBRICANT SYSTEM FAILURE DETECTION
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United States of America
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May 29, 2019
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May 29, 2019
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Abstract
A lubricant system for a gear assembly of an aircraft is presented. The lubricant system includes a main lubricant conduit and an emergency lubricant conduit joined with a valve, and further wherein the valve defines a closed position disposing lubricant through the emergency lubricant conduit when an engine is at rest, and wherein the valve defines an open position disposing lubricant through the main lubricant conduit when the engine is in operation.
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