ALEXANDRIA, Va., Aug. 12 -- United States Patent no. 12,704,095, issued on Aug. 11, was assigned to General Electric Co. (Evendale, Ohio).
"Gas turbine engine defining a rotor cavity" was invented by Narendra Anand Hardikar (Bengaluru, India).
According to the abstract* released by the U.S. Patent & Trademark Office: "A gas turbine engine includes a compressor section, a combustion section, and a turbine section arranged in serial flow order and defining a working gas flowpath, a compressor of the compressor section comprising an aft-most compressor stage; a stage of stator vanes located downstream of the aft-most compressor stage; a stator case including a seal pad; and a spool drivingly coupled to the compressor, the spool and the stato...