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:
Dec. 26, 2023

Filed:

Oct. 04, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Quentin Matthias Emmanuel Garnaud, Moissy-Cramayel, FR;

Guillaume Glemarec, Moissy-Cramayel, FR;

Hervé Jean Albert Mouton, Moissy-Cramayel, FR;

Guilhem Seize, Moissy-Cramayel, FR;

Benoit Bernard René Leclerc, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/26 (2006.01); B64D 27/16 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/16 (2013.01); B64D 2027/262 (2013.01);
Abstract

The invention relates to a turbomachine () extending along an axis (X), comprising a high-pressure body with a high-pressure compressor () coupled in rotation to a high-pressure turbine (), and a low-pressure body including a low-pressure compressor () coupled in rotation to a low-pressure turbine (), an upstream casing () located upstream of the high-pressure compressor (), and means of suspension () for the turbomachine (), intended for attaching the turbomachine () to an aircraft pylon ().


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