Patent 12123314 was granted and assigned to Pratt & Whitney Canada on October, 2024 by the United States Patent and Trademark Office.
A gas turbine engine has a service tube assembly including an adjustable joint having a flange axially movable along an end fitting having a male/female connection with a mating part. The flange is threadably engaged with the end fitting to provide for the adjustment of the position of the flange along the end fitting.