Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir
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United States of America Patent
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app pub date -
Jun 30, 2016
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Mar 29, 2011
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Abstract
A process for testing a compressor of a gas turbine engine, where a large volume of compressed air is stored in a large reservoir of at least 10,000 m3 such as an underground storage cavern, compressed air from the storage reservoir is passed through an air turbine to drive a compressor to produce high pressure and temperature compressed air, and where the compressed air can be discharged into a combustor and burned with a fuel for testing of the combustor under simulated conditions of a real gas turbine engine.
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