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:
Apr. 09, 2024

Filed:

Mar. 04, 2021
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Romain Truco, Moissy-Cramayel, FR;

Claire Marie Figeureu, Moissy-Cramayel, FR;

Paul Ghislain Albert Levisse, Moissy-Cramayel, FR;

Pierre-Alain Jean Philippe Reigner, Moissy-Cramayel, FR;

Michel Gilbert Roland Brault, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F01D 21/04 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F01D 21/045 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2220/76 (2013.01); F05D 2260/311 (2013.01); F05D 2270/09 (2013.01);
Abstract

A fan module for an aircraft turbomachine includes a fan with a disc carrying fan blades and a rotor of an electric machine. The rotor has an annular shape and is mounted coaxially downstream of the fan. The module further includes an annular support for the rotor with a downstream end fixed to the rotor and with an upstream end fixed to the fan disc. The support is fixed to the disc by shear bolts configured to break when a torque transmitted by the disc to the support exceeds a predetermined threshold.


Find Patent Forward Citations

Loading…