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.:
Date of Patent:
Sep. 02, 2025
Filed:
Apr. 15, 2022
General Electric Company, New York, NY (US);
Safran Aircraft Engines, Paris, FR;
Safran Nacelles, Gonfreville-l'Orcher, FR;
Guillaume Glemarec, Moissy-Cramayel, FR;
Nicolas Maurice Herve Aussedat, Moissy-Cramayel, FR;
Pierre Charles Caruel, Moissy-Cramayel, FR;
Mathieu Marc Christian Gaillot, Moissy-Cramayel, FR;
Jean-Baptiste Manuel Nicolas Vignes, Moissy-Cramayel, FR;
GENERAL ELECTRIC COMPANY, Schenectady, NY (US);
SAFRAN AIRCRAFT ENGINES, Paris, FR;
SAFRAN NACELLES, Gonfreville-l'Orcher, FR;
Abstract
A triple-flow turbine engine for an aircraft, this turbine engine having a longitudinal axis and including upstream suspension elements which are located in a first plane perpendicular to the axis and are connected or fixed to the gas generator of the turbine engine; downstream suspension elements which are located in a second plane perpendicular to the axis and are connected or fixed to the gas generator; and thrust-absorbing rods which include first ends which are connected or fixed to the gas generator and opposing second ends which are located in a third plane perpendicular to the axis, wherein the first, second and third planes are located at a cold compartment of the gas generator.