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:
Nov. 05, 2024

Filed:

Apr. 08, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Daniel-Ciprian Mincu, Moissy-Cramayel, FR;

Mathieu Patrick Jean-Louis Lallia, Moissy-Cramayel, FR;

Nicolas Joseph Sirvin, Moissy-Cramayel, FR;

Jagoda Alina Worotynska, Moissy-Cramayel, FR;

Frederic Dautreppe, Moissy-Cramayel, FR;

Anthony Binder, Moissy-Cramayel, FR;

Eva Julie Lebeault, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/042 (2006.01); F02K 1/66 (2006.01);
U.S. Cl.
CPC ...
F02C 7/042 (2013.01); F02K 1/66 (2013.01);
Abstract

A process for using an air input of a turboreactor nacelle of an aircraft, comprising an air input lip which comprises at least one fixed portion and at least one portion which can be moved between a first position, in which the air input lip has an aerodynamic profile so as to guide the internal air flow over the internal wall in order to promote a thrust phase, and a second position, in which the portion is displaced in relation to the fixed portion so that the air input lip has a second radial thickness in the second position which is less than the first radial thickness in the first position so as to promote a reverse thrust phase.


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