Patent 10927687 was granted and assigned to Raytheon Technologies on February, 2021 by the United States Patent and Trademark Office.
A gas turbine engine blade containment system is disclosed. The blade containment system may include a generally cylindrical casing being made of a first material, and a generally cylindrical ring being made of a second material coaxially surrounding the casing, at least some portion of the ring metallurgically bonded to the casing.