ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,374, issued on May 5, was assigned to Collins Engine Nozzles Inc. (Des Moines, Iowa). "Swirl valves" was invented by Jason A. Ryon (Carlisle,... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,375, issued on May 5, was assigned to General Electric Co. (Schenectady, N.Y.). "Systems and methods for estimating integrity and efficiency ... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,376, issued on May 5, was assigned to RTX Corp. (Farmington, Conn.). "Bleeding core air from a turbine engine core flowpath" was invented by ... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,377, issued on May 5, was assigned to SAFRAN AIRCRAFT ENGINES (Paris) and GENERAL ELECTRIC COMPANY (Schenectady, N.Y.). "Unducted propeller g... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,378, issued on May 5, was assigned to General Electric Co. (Evendale, Ohio). "Gas turbine engine" was invented by Daniel Alan Niergarth (Norw... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,379, issued on May 5, was assigned to TOYOTA JIDOSHA K.K. (Toyota, Japan). "Controller for internal combustion engine" was invented by Yuki S... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,380, issued on May 5, was assigned to RTX Corp. (Farmington, Conn.). "Variable area nozzle for an aircraft engine" was invented by Michael G.... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,381, issued on May 5, was assigned to General Electric Co. (Evendale, Ohio). "Gas turbine exhaust nozzle noise abatement" was invented by Kis... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,383, issued on May 5, was assigned to SAFRAN NACELLES (Gonfreville-L'Orcher, France). "Assembly for an exhaust cone of an aircraft turbomachi... Read More
ALEXANDRIA, Va., May 5 -- United States Patent no. 12,618,384, issued on May 5, was assigned to General Electric Co. (Evendale, Ohio). "Gas turbine engine having a bypass passage, a fan duct, and a c... Read More