AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREA

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20200025128A1
SERIAL NO

16203829

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Abstract

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A dual flow jet engine comprising a core, a surrounding nacelle, delimiting, with the core, a secondary jet, and having a structure and an outer skin fixed to the structure. The nacelle comprises an annular structure through which windows delimited by the annular structure are produced between the secondary jet and the outside. Each window has a regulation system comprising at least one shutter having an outer face, a leading and a trailing edge. Each shutter is mounted articulated at the nacelle structure window at its leading edge and is mobile between a closed position wherein the trailing edge is close to the outer skin and so the shutter closes the window and an open position where the shutter trailing edge moves outwards away from the outer skin to free the window, and for each shutter, a maneuvering system to displace the shutter between the open and closed positions.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS SASTOULOUSE FRANCE

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
CALIMAN, Laurent TOULOUSE, FR 12 4
COUSIN, Antoine L'UNION, FR 9 28
GAILLARDO, Jérôme CUGNAUX, FR 4 0

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