GAS TURBINE AND METHOD FOR OPERATING THE GAS TURBINE

• Main Authors: SÜSELBECK, KAI, GUTERMUTH, MANUEL, SAVILIUS, NICOLAS, TERTILT, MARC, ENGLER, THORSTEN, GORYNSKI, MARKUS, LINK, MARCO, KREUTZER, PHILIPP
• Format: Patent
• Language: English; French; German
• Published: 23.12.2015
• Subjects: 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; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04; LIGHTING; MACHINES OR ENGINES IN GENERAL; MECHANICAL ENGINEERING; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES; STEAM ENGINES; WEAPONS

The turbine has an air intake (14), and a compressor (1) comprising a compressor flow channel (4). The compressor has a pre-conducting blade row (3) with pre-conducting blades. A freezing-up sensor unit (17) has a sensor e.g. temperature sensor (8) and pressure sensor (7), arranged a compressor moving blade row (5) and a compressor guide vane row (6). The moving blade row is arranged in the flow channel directly downstream of the pre-conducting blade row, and the guide vane row is arranged directly downstream of the moving blade row. An independent claim is also included for a method for operating a gas turbine.