F02K 1/17

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Class  F02K : JET-PROPULSION PLANTS


Subclass 1/17: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) Varying effective area of jet pipe or nozzle (F02K 1/3 takes precedence) Control or regulation conjointly with another control with control of fuel supply

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12071942 Variable displacement pumpsOct 22, 21Aug 27, 24HAMILTON SUNDSTRAND CORPORATION
11421607 Fiber optic exit area sensing for gas turbine engine nozzlesJun 10, 21Aug 23, 22RAYTHEON TECHNOLOGIES CORPORATION
11236683 Control systemMay 24, 19Feb 01, 22Rolls Royce plc
10823113 Method and system for limiting power of an engineAug 21, 17Nov 03, 20PRATT & WHITNEY CANADA CORP.
10787995 Control device of a variable section nozzle and the implementation method thereofJun 12, 17Sep 29, 20SAFRAN AIRCRAFT ENGINES
10711734 Optimal thrust control of an aircraft engineApr 08, 19Jul 14, 20RAYTHEON TECHNOLOGIES CORPORATION
10253725 Optimal thrust control of an aircraft engineOct 23, 15Apr 09, 19United Technologies Corporation
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
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

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2020/0025,130 OPTIMAL THRUST CONTROL OF AN AIRCRAFT ENGINEApr 08, 19Jan 23, 20Not available
2017/0276,092 CONTROL DEVICE OF A VARIABLE SECTION NOZZLE AND THE IMPLEMENTATION METHOD THEREOFJun 12, 17Sep 28, 17SAFRAN AIRCRAFT ENGINES

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Patents Issued To Date - By Filing Year

Average Time to Issuance