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:
Feb. 18, 2020

Filed:

Jul. 20, 2017
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Frederic Paul Eichstadt, Moissy-Cramayel, FR;

Nora El Ghannam, Moissy-Cramayel, FR;

Romain Jean-Claude Ferrier, Moissy-Cramayel, FR;

Antoine Elie Hellegouarch, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 27/12 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/12 (2013.01); B64D 33/02 (2013.01); B64D 2027/264 (2013.01); B64D 2033/0293 (2013.01);
Abstract

The invention relates to a cradle () for an aircraft turbopropeller engine () of a substantially axial orientation, comprising a front arch () and a rear arch () extending transversely relative to said axial direction (A), said arches () being open at their lower ends and connected to each other by at least one axial longeron () extending between said arches (), characterised in that the longeron () is arranged in an upper portion of the cradle () and is formed in a single piece with the front arch ().


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