AIR INTAKE SYSTEM

The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	CASADO MONTERO, Carlos, FERNÁNDEZ LÓPEZ, Pio
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention provides an air intake system (10) comprising an air duct (2) suitable for providing airflow to the inside of an aircraft (18), preferably to an auxiliary power unit; an inlet (1) arranged at one end of the air duct (2); a skin (3) surrounding the inlet; a plurality of slots (4) arranged on the skin; driving means (16, 17), a flap door (5) connected to a driving means, a plurality of fins (6) connected to the driving means; wherein the driving means is configured for moving the flap door between at least two positions, said positions being a closed position wherein the flap door closes the inlet, and an opened position wherein the flap door is driven away from said closed position, and wherein the driving means is also configured for moving the plurality of fins in such a way that the plurality of fins protrudes through the slots