ALEXANDRIA, Va., Oct. 8 -- United States Patent no. 12,435,672, issued on Oct. 7, was assigned to SAFRAN AIRCRAFT ENGINES (Paris).
"Flexibilities in a gas turbine engine with speed reducer" was invented by Julien Fabien Patrick Becoulet (Moissy-Cramayel, France), Maxime Paul Numa Givert (Moissy-Cramayel, France) and Alexandre Jean-Marie Tan-Kim (Moissy-Cramayel, France).
According to the abstract* released by the U.S. Patent & Trademark Office: "Disclosed is an assembly for a turbomachine that includes connection elements having respective radial flexibilities, wherein a ratio of a first of the respective radial flexibilities to a third of the respective radial flexibilities is strictly lower than 10% and/or a ratio of the first of the re...