F02C 3/08

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9982676 Split axial-centrifugal compressorSep 17, 15May 29, 18Rolls-Royce North American Technologies Inc.; Rolls-Royce Corporation;
9926942 Diffuser pipe with vortex generatorsOct 27, 15Mar 27, 18PRATT & WHITNEY CANADA CORP.
9915199 Bi-directional compression fan rotor for a gas turbine engineOct 08, 12Mar 13, 18UNITED TECHNOLOGIES CORPORATION
9777698 Multiple motor gas turbine engine system with auxiliary gas utilizationNov 12, 13Oct 03, 17Schlak, Daniel Keith
9752584 Compressor arrangementSep 24, 14Sep 05, 17MAN DIESEL & TURBO SE
9752585 Gas turbine engine architecture with intercooled twin centrifugal compressorMar 13, 14Sep 05, 17UNITED TECHNOLOGIES CORPORATION
9683488 Gas turbine engine impeller system for an intermediate pressure (IP) compressorDec 20, 13Jun 20, 17ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
9650953 Gas turbineSep 05, 12May 16, 17ANSALDO ENERGIA IP UK LIMITED
9631556 Foil bearingMay 19, 16Apr 25, 17NTN CORPORATION
9624827 Thrust efficient turbofan engineApr 01, 13Apr 18, 17UNITED TECHNOLOGIES CORPORATION
9624828 Thrust efficient turbofan engineApr 26, 13Apr 18, 17UNITED TECHNOLOGIES CORPORATION
9476355 Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor sectionFeb 29, 12Oct 25, 16SIEMENS ENERGY, INC.
9409228 Method for attaching the cover of a centrifugal compressor of a turbine engine, compressor cover implementing same and compressor assembly provided with such a coverOct 20, 11Aug 09, 16TURBOMECA
9376959 Foil bearingDec 16, 13Jun 28, 16NTN CORPORATION
9366260 Spool for turbo machineryJun 18, 13Jun 14, 16ROLLS-ROYCE PLC
9334802 Gas turbine engine thermal management systemMar 13, 13May 10, 16UNITED TECHNOLOGIES CORPORATION
9255478 Reaction turbine and hybrid impulse reaction turbineOct 24, 12Feb 09, 16HYBRID TURBINE GROUP
9228497 Gas turbine engine with secondary air flow circuitDec 28, 11Jan 05, 16ROLLS-ROYCE CORPORATION, ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.,
9151501 Gas turbine centripetal annular combustion chamber and method for flow guidanceJun 14, 12Oct 06, 15ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
9051877 Thrust efficient turbofan engineApr 26, 13Jun 09, 15UNITED TECHNOLOGIES CORPORATION

Showing 1 to 20 of 43 results