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.

Patent No.:

US 11440670 B1

Date of Patent:

Sep. 13, 2022

Filed:

Dec. 14, 2018

Suspension device

Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Antoine Elie Hellegouarch, Moissy-Cramayel, FR;

Marc Patrick Tesniere, Moissy-Cramayel, FR;

Assignee:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

Attorney:

Lathrop GPM LLP

Primary Examiner:

Richard R Green

Assistant Examiner:

Steven J Shur

Int. Cl.

CPC ...

B64D 27/26 (2006.01); B64D 27/10 (2006.01); B64D 27/16 (2006.01);

U.S. Cl.

CPC ...

B64D 27/26 (2013.01); B64D 27/10 (2013.01); B64D 27/16 (2013.01); B64D 2027/266 (2013.01); B64D 2027/268 (2013.01);

Abstract

The invention concerns a suspension device () for a turbomachine comprising a body () intended to be fixed to a fixed part of an aircraft, extending along a longitudinal axis (A) intended to be parallel to a driving shaft axis of the turbomachine once the suspension device () is connected to the turbomachine, a first connecting rod () and a second connecting rod () located in the same transverse plane (P) perpendicular to the longitudinal axis (A) of the body, each comprising a first end articulated with respect to the body (), and a second end intended to be articulated to a first part of the turbomachine, a third connecting rod () articulated on the body () between the first ends of the first and second connecting rods () and intended to be articulated on a first part of the turbomachine between the second ends of the first and second connecting rods (), the suspension device () being characterised in that it further comprises a rudder () articulated on the body () and a fourth connecting rod () and a fifth connecting rod () each extending along an axis of extension (L, L) and each comprising a first end () articulated on the rudder () and a second end () intended to be articulated on a second part of the turbomachine.

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