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. 19, 2024

Filed:

Oct. 12, 2020
Applicants:

Safran, Paris, FR;

Safran Helicopter Engines, Bordes, FR;

Inventors:

Jean-Louis Robert Guy Besse, Moissy-Cramayel, FR;

Ye-Bonne Karina Maldonado, Moissy-Cramayel, FR;

Assignees:

SAFRAN, Paris, FR;

SAFRAN HELICOPTER ENGINES, Bordes, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/00 (2006.01); F01D 5/02 (2006.01); F01D 25/00 (2006.01); F02K 1/00 (2006.01);
U.S. Cl.
CPC ...
B64D 29/00 (2013.01); F01D 5/02 (2013.01); F01D 25/005 (2013.01); F02K 1/002 (2013.01); F05D 2220/90 (2013.01); F05D 2240/20 (2013.01); F05D 2300/505 (2013.01);
Abstract

A propulsion system for an aircraft includes a rotor and a nacelle fairing that extends around the rotor in relation to an axis. The nacelle fairing includes an upstream portion forming an inlet section of the nacelle fairing as well as a downstream portion, a downstream end of which forms an outlet section of the nacelle fairing. The downstream portion includes radially inner and outer walls, both of which are made of a deformable shape memory material. The wall has independently actuatable piston actuator mechanisms, each actuator mechanism being actuatable independently of the others and being designed to cooperate with means built into an inner surface of the wall to deform the wall in a radial direction in relation to the axis under the effect of a predetermined displacement command.


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