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. 14, 2024

Filed:

Jun. 04, 2020
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Albert Josse, Moissy-Cramayel, FR;

Lois Pierre Denis Vive, Moissy-Cramayel, FR;

Jean-Maurice Casaux-Bic, Moissy-Cramayel, FR;

Yvan Ludovic Lameignere, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F01D 25/162 (2013.01); F01D 25/28 (2013.01); F05D 2220/323 (2013.01); F05D 2240/50 (2013.01); F05D 2250/141 (2013.01); F05D 2250/184 (2013.01); F05D 2250/291 (2013.01); F05D 2250/61 (2013.01); F05D 2260/30 (2013.01);
Abstract

A component () for supporting at least one bearing () for a turbine engine () comprising: two coaxial walls, internal () and external () walls respectively, defining a gas flow vein () between them and interconnected by a row of arms (); an external ferrule () comprising an internal peripheral edge () connected to the external wall () and an external peripheral edge () connected to an external mounting flange (); an internal ferrule () comprising an external peripheral edge () connected to the internal wall () and an internal peripheral edge () comprising an internal mounting flange (); at least one of the ferrules (), which at the peripheral edge () thereof is connected to the corresponding wall (), having a general shape which is corrugated about an axis (X-X) of the component ().


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