Gas turbine engine air intake in a nacelle

The present invention relates to an assembly comprising a gas turbine engine (10) and a nacelle (26) in which the engine is housed, the nacelle including an air intake fairing (26a) that forms an air inlet and includes: a member for deflecting (40) foreign objects, which, together with said fairing,...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	YVON DIDIER JEAN-LOUIS, MABBOUX GAETAN JEAN, MINOT PHILIPPE GILLES, VINCENT THOMAS ALAIN CHRISTIAN, CHANEZ PHILIPPE GERARD
Format:	Patent
Sprache:	chi ; eng
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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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