F02C 3/045

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9995216 Disc turbine engineAug 28, 17Jun 12, 18Not available
9863319 Split-zone flow metering T-tubeMar 01, 13Jan 09, 18UNITED TECHNOLOGIES CORPORATION
9828911 Turbofan jet engine with low pressure shaft passing outside of core engineJul 09, 14Nov 28, 17ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
9777698 Multiple motor gas turbine engine system with auxiliary gas utilizationNov 12, 13Oct 03, 17Schlak, Daniel Keith
9464576 System and method for operating a power plantSep 25, 13Oct 11, 16GENERAL ELECTRIC COMPANY
9303560 Screw shaft turbine compressor and systemFeb 11, 14Apr 05, 16JACKSON, BARBARA, MRS
8104257 Tip turbine engine with multiple fan and turbine stagesDec 01, 04Jan 31, 12UNITED TECHNOLOGIES CORPORATION
6397577 Shaftless gas turbine engine spoolApr 02, 01Jun 04, 02The United States of America as represented by the Secretary of the Air Force
5241815 Heat-recovering-thrust-turbine having rotational flow pathApr 22, 92Sep 07, 93Not available
5224339 Counterflow single rotor turbojet and methodDec 19, 90Jul 06, 93ALLIED-SIGNAL INC.
4757682 Axial flow turbineFeb 03, 87Jul 19, 88Not available