SYSTEMS AND METHODS FOR TESTING A GAS TURBINE

Embodiments of the disclosure relate to performance testing of a gas turbine. In one embodiment, a gas turbine performance testing system (100) can include a server (200), a transducer system (110), a signal converter (115), and an automated gas chromatograph (135). The transducer system (110) acqui...

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Bibliographische Detailangaben
Hauptverfasser:	CANO, Jorge, MAGANA, Ricardo Emilio, MORALES, Benjamin Moises, CHANDRA, Dibakar, LI, Bryan, ASCENCIO, Vasanthi, HEDA, Sanjeev Shyam
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MEASURING MECHANICAL ENGINEERING PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR WEAPONS
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Beschreibung
Zusammenfassung:	Embodiments of the disclosure relate to performance testing of a gas turbine. In one embodiment, a gas turbine performance testing system (100) can include a server (200), a transducer system (110), a signal converter (115), and an automated gas chromatograph (135). The transducer system (110) acquires one or more functional parameters of the gas turbine (105) and the signal converter (115) converts the functional parameters acquired by the transducer system (110) to gas turbine operational data. The automated gas chromatograph (135) automatically analyzes a test sample of a natural gas that is used to operate the gas turbine (105). The gas turbine operational data generated by the signal converter (115) and the analysis information obtained from the test sample are provided to the server (200) for propagating via a communication network (140), to a client computer (145) where the gas turbine operational data and the analysis information can be used to obtain a gas turbine performance test result.