F02K 1/17

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9822731 Control scheme using variable area turbine and exhaust nozzle to reduce dragMar 27, 15Nov 21, 17UNITED TECHNOLOGIES CORPORATION
9488131 Device for controlling a variable section nozzle of an aircraftApr 17, 13Nov 08, 16AIRBUS OPERATIONS SAS
9222418 Fuel feed circuit with hydraulic actuator and fuel metering unit for an aeroengineSep 30, 10Dec 29, 15SNECMA
9206746 Method of controlling speed transients in a turbine engineJul 02, 12Dec 08, 15SNECMA
7647776 Fluid flow control systemJul 31, 87Jan 19, 10GOODRICH CONTROL SYSTEMS
6353790 Gas turbine aeroengine control systemAug 11, 00Mar 05, 02Honda Giken Kogyo Kabushiki Kaisha
6000215 Method of operating a gas turbine engineDec 23, 97Dec 14, 99UNITED TECHNOLOGIES CORPORATION
5303545 Pressure based close loop thrust control in a turbofan engineOct 05, 92Apr 19, 94UNITED TECHNOLOGIES CORPORATION
4947643 Active geometry control system for gas turbine enginesSep 20, 88Aug 14, 90UNITED TECHNOLOGIES CORPORATION
4809500 Transient control system for gas turbine engineFeb 03, 87Mar 07, 89UNITED TECHNOLOGIES CORPORATION
4501117 Device for controlling and regulating the cross section of a variable area propulsive nozzleNov 16, 83Feb 26, 85SNECMA
4414807 Method and apparatus for controlling a gas turbine engineDec 08, 80Nov 15, 83UNITED TECHNOLOGIES CORPORATION