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:
May. 02, 2017

Filed:

Apr. 24, 2014
Applicant:

Snecma, Paris, FR;

Inventors:

Mathieu Ange Alexis Poisson, Corbeil-Essonnes, FR;

Julien Michel Patrick Christian Austruy, Yerres, FR;

François Gallet, Paris, FR;

Mario Lambey, Paris, FR;

Assignee:

SNECMA, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/10 (2006.01); B64D 27/26 (2006.01); F02C 7/20 (2006.01);
U.S. Cl.
CPC ...
B64D 27/10 (2013.01); B64D 27/26 (2013.01); F02C 7/20 (2013.01); B64D 2027/264 (2013.01); B64D 2027/266 (2013.01);
Abstract

The invention provides a suspension structure for suspending a turboprop () having two unducted propellers on a structural element of an aircraft, the suspension structure comprising a cradle () for fastening to a structural element of the aircraft and having two lateral beams () connected to a main beam () extending parallel to a longitudinal axis () of the turboprop so as to form a V-shaped cradle structure, the cradle being fastened to the turboprop via two angle members () connecting each free end of the lateral beams of the cradle to the turboprop, via an axial link () connecting one end of the main beam of the cradle of the turboprop, and via at least one transverse link () situated in a plane extending transversely relative to the longitudinal axis of the turboprop and connecting the cradle to the turboprop.


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