Bypass turbojet engine nacelle

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8523516
APP PUB NO 20100040466A1
SERIAL NO

12445421

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Abstract

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The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a)which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.

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Patent Owner(s)

Patent OwnerAddress
AIRCELLEROUTE DU PONT 8 GONFREVILLE L'ORCHER 76700

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Chouard, Pierre-Alain Paris, FR 3 67
Collier, Jerome Le Havre, FR 5 123
Conte, Francois Tournefeuille, FR 2 29
Dhainault, Patrice Ste Adresse, FR 2 36
Hillereau, Nicolas Le Havre, FR 4 110
Lefort, Guillaume Paris, FR 11 142
Vauchel, Guy Bernard Le Havre, FR 118 1876

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