The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 10, 2016

Filed:

Jun. 14, 2013
Applicant:

Aircelle, Gonfreville l'Orcher, FR;

Inventors:

Patrick Gonidec, Bretx, FR;

Alexandre Bellanger, Le Havre, FR;

Assignee:

AIRCELLE, Gonfreville l'Orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 29/06 (2006.01); B64D 33/02 (2006.01); F02K 1/76 (2006.01); F02K 1/70 (2006.01); F02K 1/72 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F02K 1/766 (2013.01); B64D 29/06 (2013.01); F01D 25/24 (2013.01); F02K 1/70 (2013.01); F02K 1/72 (2013.01); Y02T 50/671 (2013.01);
Abstract

A nacelle for an aircraft bypass turbofan engine includes an upstream section via which an airflow enters, a middle section surrounding the fan of the turbofan and a downstream section having an inner structure and an outer structure delimiting a flow duct in which the air flows. The outer structure includes one cowling movably mounted on the inner fixed structure. The nacelle also has a top to accept a pylon for attaching a wing of the aircraft. The nacelle further includes one first panel mounted on the inner structure on one side of the nacelle and one second panel mounted on the other side of the nacelle. The first panel undergoes a physical interference with a part of the wing. The second panel increases the air removed from this other side of the nacelle during thrust reversal.


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