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:
Aug. 10, 2021

Filed:

Nov. 13, 2018
Applicant:

Airbus Operations S.a.s., Toulouse, FR;

Inventors:

Frédéric Fort, Saint Genies Bellevue, FR;

Alexandre Bellanger, Tournefeuille, FR;

Laurent Jouathel, Leguevin, FR;

Gary Benjamin Davison, Carrickfergus, GB;

Richard Edward John Lockhart, Dollingstown, GB;

Assignee:

AIRBUS OPERATIONS S.A.S., Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); B64D 29/02 (2006.01); B64D 33/04 (2006.01); F02K 1/70 (2006.01); B64D 29/00 (2006.01); B64D 29/08 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); B64D 29/00 (2013.01); B64D 29/02 (2013.01); B64D 29/08 (2013.01); B64D 33/04 (2013.01); F02K 1/70 (2013.01); F05D 2220/00 (2013.01);
Abstract

A nacelle for a jet engine having a selectively operated reverse thruster which redirects air flow to a cascade during a reverse thrust operation, the nacelle including a fancowl panel configured as a stationary partial cover for a jet engine; and a translating cowl panel configured to move transversely during a reverse thrust operation so as to expose a cascade for emitting reverse thrust airflow. In exemplary embodiments, a moveable automatic translating panel, or a rotatable hinge panel, or an extension portion of the fancowl is used to preserve clearance with an aircraft wing in a nacelle clearance area.


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