ALEXANDRIA, Va., May 26 -- United States Patent no. 12,637,986, issued on May 26, was assigned to Pratt & Whitney Canada Corp. (Longueuil, Canada).
"Gas turbine acceleration limit biasing for premature asymmetric operating regime exits" was invented by Louis Duranleau-Hendrickx (Montreal) and Andrea Henning (London, Canada).
According to the abstract* released by the U.S. Patent & Trademark Office: "A method includes sending a first control signal, wherein the first control signal causes a turbine engine of a plurality of turbine engines of an aircraft to initiate an entry into an asymmetric operating regime. The method further includes receiving, a control input for an exit from the asymmetric operating regime, determining, a progression...