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:
Jun. 03, 2025

Filed:

Dec. 18, 2023
Applicant:

Airbus Operations Gmbh, Hamburg, DE;

Inventors:

Wolfgang Ehrhard, Hamburg, DE;

Luc Andreani, Hamburg, DE;

Florian Lorenz, Hamburg, DE;

Assignee:

Airbus Operations GmbH, Hamburg, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/02 (2006.01); B64C 3/48 (2006.01); B64C 3/50 (2006.01); B64C 7/00 (2006.01); B64C 9/16 (2006.01); B64C 9/18 (2006.01);
U.S. Cl.
CPC ...
B64C 9/02 (2013.01); B64C 3/48 (2013.01); B64C 3/50 (2013.01); B64C 7/00 (2013.01); B64C 9/16 (2013.01); B64C 9/18 (2013.01);
Abstract

A fairing arrangement for an aircraft high-lift mechanism, the high-lift mechanism including a flap arranged at an aircraft wing trailing edge and a mounting and guiding mechanism for the flap. The fairing arrangement includes a flap side fairing unit and a wing side fairing unit. The flap side fairing unit includes a flap side fairing covering an aft part of the mounting and guiding mechanism and a flap side fairing mount mounting the flap side fairing to the flap. The wing side fairing unit includes a wing side fairing covering a forward part of the mounting and guiding mechanism and a wing side fairing mount mounting the wing side fairing to the wing. The wing side fairing mount is configured to connect the wing side fairing movably to the wing such that the wing side fairing is rotatable around an axis directed at least partially in a vertical direction.


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