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, 2022

Filed:

Oct. 12, 2017
Applicant:

Airbus Operations Sas, Toulouse, FR;

Inventors:

Alain Porte, Colomiers, FR;

Frédéric Vinches, Larra, FR;

Assignee:

AIRBUS OPERATIONS SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); B64C 7/02 (2006.01); F02C 7/045 (2006.01); B64D 29/00 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); B64C 7/02 (2013.01); B64D 29/00 (2013.01); F02C 7/045 (2013.01); B64D 2033/0206 (2013.01); B64D 2033/0273 (2013.01); B64D 2033/0286 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2260/30 (2013.01); F05D 2260/31 (2013.01); F05D 2260/963 (2013.01); Y02T 50/60 (2013.01);
Abstract

An aircraft nacelle including a conduit rigidly connected to an air inlet and a conduit rigidly connected to an engine, a link between the conduit rigidly connected to the air inlet and the conduit rigidly connected to the engine. The link includes a sleeve that receives one end of a first conduit and is rigidly connected to a second conduit, and linking elements that link the sleeve and the first conduit and that are distributed about the entire circumference of the nacelle, each linking element having a threaded stem oriented in a radial direction and being configured to enable tightening from inside the first conduit.


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