GAS TURBINE ENGINE WITH AN OFFTAKE

An apparatus and method for a turbine engine 10 including an offtake 84 located within the airflow of the engine 10. The offtake 84 has an inlet 90 and a louver covering the inlet 90. The louver 92 has multiple airfoils 94, 96, 98, 100 arranged to direct the air flow into the inlet 90 of the offtake...

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Bibliographic Details
Main Authors GUIJARRO VALENCIA, Antonio, MICHELASSI, Vittorio
Format Patent
LanguageEnglish
French
German
Published 13.09.2017
Subjects
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
MECHANICAL ENGINEERING
WEAPONS
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Summary:An apparatus and method for a turbine engine 10 including an offtake 84 located within the airflow of the engine 10. The offtake 84 has an inlet 90 and a louver covering the inlet 90. The louver 92 has multiple airfoils 94, 96, 98, 100 arranged to direct the air flow into the inlet 90 of the offtake 84.
Bibliography:Application Number: EP20170159440