US Patent Issued to GENERAL ELECTRIC on Feb. 17 for "Gas turbine engine having a thrust reverser system with drag link connectors at inter-compressor frame structure" (Ohio, Massachusetts Inventors)

ALEXANDRIA, Va., Feb. 17 -- United States Patent no. 12,553,403, issued on Feb. 17, was assigned to GENERAL ELECTRIC COMPANY (Evendale, Ohio).

"Gas turbine engine having a thrust reverser system with drag link connectors at inter-compressor frame structure" was invented by Brandon W. Miller (Middletown, Ohio), Stephen G. Matava (Andover, Mass.) and Eric Barre (Cincinnati).

According to the abstract* released by the U.S. Patent & Trademark Office: "A gas turbine engine includes a fan assembly, a turbo-engine encased within a turbo-engine cowl structure, a nacelle, and a thrust reverser system arranged, at least in part, in the nacelle. The turbo-engine includes a low-pressure compressor, a high-pressure compressor, an inter-compressor fram...