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. 02, 2020

Filed:

Apr. 25, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/06 (2006.01); F01D 5/02 (2006.01); F01D 7/00 (2006.01); B64D 27/10 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/06 (2013.01); B64D 27/10 (2013.01); F01D 5/021 (2013.01); F01D 7/00 (2013.01); B64D 2027/005 (2013.01); Y02T 50/66 (2013.01);
Abstract

The invention relates to an unducted-fan aircraft engine comprising a generally cylindrical nacelle through which a primary jet flows, the nacelle bearing a fan rotor comprising variable-pitch vanes () located radially outside the nacelle in order to be traversed by a secondary jet () flowing longitudinally around the nacelle. The rotor comprises a hub bearing variable-pitch vane supports each carrying one vane (), each vane () comprising a blade extending from a root that is used to removably attach same to a base of the associated support (). Each base () is located radially outside the nacelle so that it is in the secondary jet, and each assembly formed by a base () and the vane root supported by the base () is surrounded and covered by a detachable aerodynamic cover ().


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