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:
Mar. 11, 2025
Filed:
May. 20, 2021
General Electric Company, Schenectady, NY (US);
Safran Aircraft Engines, Paris, FR;
Michael Cline, Evendale, OH (US);
Jonathan E. Coleman, Evendale, OH (US);
Craig W. Higgins, Evendale, OH (US);
Daniel E. Mollmann, Evendale, OH (US);
Mark E. Linz, Evendale, OH (US);
Guillaume Glemarec, Paris, FR;
Valerio Capasso, Paris, FR;
Jean-Baptiste Manuel Nicolas Vignes, Paris, FR;
Nicolas Maurice Hervé Aussedat, Paris, FR;
Francois Gallet, Paris, FR;
General Electric Company, Evendale, OH (US);
Safran Aircraft Engines, Paris, FR;
Abstract
Methods, apparatus, systems and articles of manufacture for mounting a gas turbine engine are described. An apparatus for mounting a gas turbine engine to a pylon, the gas turbine including an upstream section and a downstream section, the gas turbine defining a roll axis, a yaw axis, and a pitch axis, the apparatus including: a first mount to couple the upstream section of the gas turbine engine to the pylon; a second mount to couple the upstream section of the gas turbine engine to the pylon, the second mount downstream of the first mount; a thrust linkage to couple the upstream section to the pylon, wherein the downstream section is decouplable from the upstream section without decoupling the first mount, the second mount, and the thrust linkage.