AIR INLET FOR A TURBOFAN ENGINE

AIR INLET FOR A TURBOFAN ENGINE

The present invention relates to an air inlet for a nacelle of a jet engine with a front fan, comprising an upper part ( 115 S), a lower part ( 115 I), an inner lateral part ( 115 int) and an outer lateral part (ext), defining a leading edge ( 115 ) between an external wall ( 111 ) of the nacelle an...

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Hauptverfasser: CHANEZ PHILIPPE GERARD, LOHEAC PIERRE PHILIPPE MARIE
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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creator CHANEZ PHILIPPE GERARD
LOHEAC PIERRE PHILIPPE MARIE
description The present invention relates to an air inlet for a nacelle of a jet engine with a front fan, comprising an upper part ( 115 S), a lower part ( 115 I), an inner lateral part ( 115 int) and an outer lateral part (ext), defining a leading edge ( 115 ) between an external wall ( 111 ) of the nacelle and an internal wall ( 113 ) forming the air supply channel of the jet engine. According to the invention, the air inlet is characterized in that the leading edge of the outer lateral part ( 115 ext) is to the rear with respect to the leading edge of the inner lateral part ( 115 int). Preferably, the leading edge of the upper part ( 115 S) is likewise to the rear with respect to the leading edge of the lower part ( 115 I).
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According to the invention, the air inlet is characterized in that the leading edge of the outer lateral part ( 115 ext) is to the rear with respect to the leading edge of the inner lateral part ( 115 int). 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According to the invention, the air inlet is characterized in that the leading edge of the outer lateral part ( 115 ext) is to the rear with respect to the leading edge of the inner lateral part ( 115 int). 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According to the invention, the air inlet is characterized in that the leading edge of the outer lateral part ( 115 ext) is to the rear with respect to the leading edge of the inner lateral part ( 115 int). Preferably, the leading edge of the upper part ( 115 S) is likewise to the rear with respect to the leading edge of the lower part ( 115 I).</abstract><oa>free_for_read</oa></addata></record>
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subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title AIR INLET FOR A TURBOFAN ENGINE
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