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:
Mar. 26, 2024

Filed:

Jun. 09, 2020
Applicants:

Safran Nacelles, Gonfreville-l 'Orcher, FR;

Safran Aircraft Engines, Paris, FR;

Inventors:

Denis Guillois, Moissy-Cramayel, FR;

Florent Matthieu Jacques Nobelen, Moissy-Cramayel, FR;

Luigi Bisanti, Moissy-Cramayel, FR;

Assignees:

SAFRAN NACELLES, Gonfreville-L'Orcher, FR;

SAFRAN AIRCRAFT ENGINES, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/72 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/72 (2013.01); F02K 1/763 (2013.01);
Abstract

In a thrust reverser for an aircraft propulsion unit, the thrust reverser includes an internal fixed structure, a mobile cowl and blocking flaps. The thrust reverser also includes a first actuation mechanism that is configured to move the mobile cowl between a closing position and an opening position so as to cause the blocking flaps to move respectively between a retracted position and a deployed position, thus causing the thrust reverser to pass respectively between a full-thrust configuration and a thrust-reversal configuration. The thrust reverser also includes a second actuation mechanism that is configured to move the blocking flaps between the retracted position and a partially deployed position when the mobile cowl is in the closing position, so as to cause the thrust reverser to pass respectively between the full-thrust configuration and a reduced-thrust configuration.


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