F02C 3/107

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
RE48980 Acoustic liner with varied propertiesSep 03, 20Mar 22, 22RAYTHEON TECHNOLOGIES CORPORATION
9995143 Geared axial multistage expander device, system and methodFeb 18, 15Jun 12, 18Not available
9982676 Split axial-centrifugal compressorSep 17, 15May 29, 18Rolls-Royce North American Technologies Inc.; Rolls-Royce Corporation;
9970352 Turbomachine fan clutchJan 27, 12May 15, 18United Technologies Corporation
9964033 Two-spool design for a turboshaft engine with a high-pressure compressor connected to a low-pressure turbineJun 07, 12May 08, 18Turbomeca
9951633 Reduced length transition ductsOct 20, 14Apr 24, 18United Technologies Corporation
9932892 Compound engine assembly with coaxial compressor and offset turbine sectionJul 23, 15Apr 03, 18Pratt & Whitney Canada Corp.
9915164 Geared turbofan with high speed generatorApr 16, 15Mar 13, 18UNITED TECHNOLOGIES CORPORATION
9909495 Gas turbine engine with distributed fans with drive controlJan 20, 15Mar 06, 18UNITED TECHNOLOGIES CORPORATION
9903278 Control apparatus for estimating operating parameter of a gas-turbine aeroengineApr 17, 15Feb 27, 18HONDA MOTOR CO., LTD.
9897001 Compressor areas for high overall pressure ratio gas turbine engineFeb 12, 15Feb 20, 18UNITED TECHNOLOGIES CORPORATION
9890704 Compressor systemApr 01, 14Feb 13, 18DERWENT AVIATION CONSULTING LTD.
9885313 Gas turbine engine bifurcation located fan variable area nozzleJan 05, 12Feb 06, 18UNITED TECHNOLOGIES CORPORATION
9885282 Turbofan engine bearing and gearbox arrangementMar 13, 14Feb 06, 18UNITED TECHNOLOGIES CORPORATION
9879694 Turbo-compressor with geared turbofanFeb 03, 15Jan 30, 18UNITED TECHNOLOGIES CORPORATION
9878798 Aircraft with counter-rotating turbofan enginesDec 09, 15Jan 30, 18ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
9874150 Method of assembly for gas turbine fan drive gear systemMar 24, 14Jan 23, 18UNITED TECHNOLOGIES CORPORATION
9874145 Lubrication system for gas turbine enginesApr 27, 15Jan 23, 18UNITED TECHNOLOGIES CORPORATION
9869249 Speed sensor probe location in gas turbine engineMar 15, 13Jan 16, 18UNITED TECHNOLOGIES CORPORATION
9869191 Geared low fan pressure ratio fan exit guide vane stagger angleApr 17, 13Jan 16, 18UNITED TECHNOLOGIES CORPORATION

Showing 1 to 20 of 84 results