ADMISSION D'AIR DANS UN MOTEUR D'AVION EQUIPEE D'UN SEPARATEUR DE CORPS ETRANGERS

The present invention comprises a method and apparatus for separating foreign objects from airflow channelled to an aircraft engine. An air intake including a foreign object separator includes an inlet duct having a pressure side 34 which inlet duct is effective for channelling airflow to the engine...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	MARTIN GEORGE RAY, MICHAEL CHARLES HARROLD ET LOUIS ERNEST VARADI
Format:	Patent
Sprache:	fre
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 LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention comprises a method and apparatus for separating foreign objects from airflow channelled to an aircraft engine. An air intake including a foreign object separator includes an inlet duct having a pressure side 34 which inlet duct is effective for channelling airflow to the engine, a separator aperture 36 disposed in the pressure side of the inlet duct and a separator receptacle 38 which extends from the inlet duct and is in flow communication with the separator aperture. The separator receptacle includes a turning wall which is substantially arcuate in a transverse plane, and is substantially closed for preventing the flow of airflow therethrough while being effective for receiving and capturing foreign objects which enter the inlet duct and pass through the separator aperture.