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. 10, 2024
Filed:
Sep. 25, 2020
Safran Aircraft Engines, Paris, FR;
Regis Eugene Henri Servant, Moissy-Cramayel, FR;
Didier Gabriel Bertrand Desombre, Moissy-Cramayel, FR;
Christophe Paul Jacquemard, Moissy-Cramayel, FR;
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Abstract
The invention concerns an aircraft turbine engine (), comprising a gas generator comprising at least one annular gas flow duct (), the duct () being defined by two annular housings, respectively an external housing () and an internal housing (), extending one around the other and connected together by at least one tubular arm () for the passage of a lubricating oil line (). According to the invention, the line () comprises a first fixed section () secured to the external housing (), a second fixed section () secured to a piece of equipment () of the turbomachine capable of moving or vibrating during operation relative to the housings (), and an intermediate section () connecting the first and second sections (), this intermediate section () having a generally elongate shape and comprising longitudinal ends engaged and capable of swiveling and/or sliding in ends of the first and second sections ().