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. 23, 2015

Filed:

Nov. 29, 2011
Applicants:

Nicolas Boulet, Toulouse, FR;

Sébastien Affortit, Brax, FR;

Inventors:

Nicolas Boulet, Toulouse, FR;

Sébastien Affortit, Brax, FR;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 33/02 (2006.01); F02C 7/04 (2006.01); F02C 7/045 (2006.01);
U.S. Cl.
CPC ...
B64D 33/02 (2013.01); Y10T 29/49229 (2015.01); F02C 7/04 (2013.01); B64D 2033/0206 (2013.01); F02C 7/045 (2013.01); B64D 2033/0286 (2013.01);
Abstract

An air inlet for nacelle of an aircraft propulsion unit comprising an inner envelope provided with a plurality of orifices for passage of fluid passing through the envelope, and a lip connected to the upstream edge of the inner envelope, and having a portion devoid of orifices for passage of fluid with an axial span of between 20% and 90% of the span of the inner envelope, and a circumferential span a of between 60° and 150° about a longitudinal axis of the air inlet. A process for repairing an air inlet comprising cutting out a recess in an upstream edge of an inner envelope of the air inlet, then arranging and fixing an impermeable panel in the recess so as to create an air inlet of the type described above.


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