Temperature adjusting method of hot gas of a gas turbine

The gas turbine (1) has an injection unit (9) for the injecting of a fluid (W) into an air flow (L) drawn in by a compressor (3). A temperature measuring device (MLU) to record the temperature of the air flow is installed in front of the injection unit. The temperature (TV1) of the air flow at the i...

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Bibliographische Detailangaben
Hauptverfasser:	TAPPEN MARCO, PELS LEUSDEN CHRISTOPH
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The gas turbine (1) has an injection unit (9) for the injecting of a fluid (W) into an air flow (L) drawn in by a compressor (3). A temperature measuring device (MLU) to record the temperature of the air flow is installed in front of the injection unit. The temperature (TV1) of the air flow at the inlet (12) to the compressor is calculated by means of the measured temperature (TU). An air moisture measuring device (MFU) in front of the injection device determines the moisture in the air flow. Independent claims are also included for the following: (a) a temperature measuring device to record the temperature of the air flow in front of the compressor of a gas turbine; and (b) a control system for the hot gas temperature of a gas turbine.