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

SERIAL NO

15198440

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Abstract

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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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Patent Owner(s)

Patent OwnerAddress
FLORIDA TURBINE TECHNOLOGIES INC1701 MILITARY TRAIL SUITE 110 JUPITER FL 33458-7887

International Classification(s)

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  • 2016 Application Filing Year
  • G01M Class
  • 1447 Applications Filed
  • 1062 Patents Issued To-Date
  • 73.40 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances201620172018201920202021202220230255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Brostmeyer, Joseph D Jupiter, US 45 437
Memmen, Robert L Stuart, US 34 385

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges904284757331201 - 1011 - 2021 - 3031 - 4041 - 5051 - 6061 - 70100 +0255075100125150175200225250275300325350375400425450

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