F02K 1/00

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Class  F02K : JET-PROPULSION PLANTS


Subclass 1/00: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97)

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
10563613 Coanda device for a round exhaust nozzleJul 26, 16Feb 18, 20Rolls-Royce North American Technologies Inc.
10527000 Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sectionsNov 30, 16Jan 07, 20AIRBUS HELICOPTERS DEUTSCHLAND GMBH
10501197 Fluidic propulsive systemJul 27, 16Dec 10, 19JETOPTERA, INC.
10451007 Enhanced operability dual mode ramjet and scramjet engine ignition systemFeb 21, 17Oct 22, 19Northrop Grumman Systems Corporation
10414481 Method for forming a structural panelFeb 14, 17Sep 17, 19Rohr, Inc.
10414518 Vehicle attitude control using movable massNov 07, 16Sep 17, 19The Aerospace Corporation
10407177 Convertible engine exhaust for rotocraftMay 22, 15Sep 10, 19Sikorsky Aircraft Corporation
10406729 Compression molding assembly and methods for molding a thermoplastic blocker doorAug 29, 16Sep 10, 19The Boeing Company
10385805 Thrust vectoring nozzleOct 04, 17Aug 20, 19Rolls Royce plc
10378479 Variable effective area fan nozzleOct 19, 15Aug 13, 19General Electric Company
10371092 Convergent divergent exit nozzle for a gas turbine engineAug 04, 15Aug 06, 19United Technologies Corporation
10316792 Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applicationsJul 23, 13Jun 11, 19The Boeing Company
10246544 Method for producing an ablative resinJan 20, 16Apr 02, 19ArianeGroup SAS; Centre National De La Recherche Scientifique (CNRS);
10221720 Structural frame integrated with variable-vectoring flow control for use in turbine systemsSep 03, 14Mar 05, 19Honeywell International Inc.
10197008 Gas turbine engine including a third flowpath exhaust nozzleFeb 14, 14Feb 05, 19United Technologies Corporation
10145336 Translating outer cowl flow modulation device and methodOct 24, 14Dec 04, 18United Technologies Corporation
10132181 Impingement cooled nozzle linerJan 22, 18Nov 20, 18United Technologies Corporation
10087885 Gas turbine engine with axial movable fan variable area nozzleOct 11, 17Oct 02, 18United Technologies Corporation
10082106 Propellant feed circuit and a cooling methodJan 10, 14Sep 25, 18ArianeGroup SAS
10041445 Nozzle having a movable divergent section with a thermal protection systemFeb 13, 14Aug 07, 18ArianeGroup SAS

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2020/0025,128 AIRCRAFT JET ENGINE COMPRISING MEANS FOR VARYING ITS OUTPUT SURFACE AREANov 29, 18Jan 23, 20Not available
2019/0195,169 TWO-DIMENSIONAL SUPERSONIC NOZZLE THRUST VECTORING USING STAGGERED RAMPSDec 12, 18Jun 27, 19The Regents of the University of California
2019/0170,087 THRUST VECTOR CONTROLLERDec 29, 17Jun 06, 19Not available
2019/0017,468 Gimballed Augmentation ShroudJul 12, 18Jan 17, 19Not available
2018/0266,394 Generalized Jet-Effect and Generalized GeneratorMay 17, 18Sep 20, 18Not available
2015/0315,998 GENERATION OF A PULSED JET BY JET VECTORING THROUGH A NOZZLE WITH MULTIPLE OUTLETSJul 10, 15Nov 05, 15SOUTHERN METHODIST UNIVERSITY

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Patents Issued To Date - By Filing Year

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