F02K 1/38

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Class  F02K : JET-PROPULSION PLANTS


Subclass 1/38: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) Introducing air inside the jet (F02K 1/28 takes precedence)

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12163486 Exhaust mixer with protrusionsJan 10, 23Dec 10, 24PRATT & WHITNEY CANADA CORP.
12163488 Selectable inlet for aircraft propulsion system heat exchangerSep 07, 23Dec 10, 24RTX CORPORATION
12162618 Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methodsOct 10, 22Dec 10, 24Boom Technology, Inc.
12110840 Turbine engine separate flow mixer with lobesApr 03, 20Oct 08, 24SAFRAN AIRCRAFT ENGINES
12000336 Variable geometry thrusterJun 29, 22Jun 04, 24JETOPTERA, INC.
11913405 Turbine engine with a flow splitter having a profile with inclined serrationsMar 14, 23Feb 27, 24SAFRAN AIRCRAFT ENGINES
11828248 Rotatably driven exhaust mixerJun 27, 22Nov 28, 23PRATT & WHITNEY CANADA CORP.
11802511 Internal structure for a turbomachine nacelleAug 06, 20Oct 31, 23SAFRAN AIRCRAFT ENGINES
11754018 Aircraft propulsion system exhaust nozzle with ejector passage(s)Dec 17, 21Sep 12, 23Rohr, Inc.
11746726 Aircraft propulsion system nozzle with internal flow passageMay 04, 21Sep 05, 23Rohr, Inc.
11629664 Turbine engine with a flow splitter having a profile with inclined serrationsFeb 15, 19Apr 18, 23SAFRAN AIRCRAFT ENGINES
11585291 Tail cone ejector for power cable cooling system in a gas turbine engineSep 11, 20Feb 21, 23RAYTHEON TECHNOLOGIES CORPORATION
11506143 Flow mixer with a changing thicknessJan 11, 18Nov 22, 22SAFRAN AIRCRAFT ENGINES
11448160 High temperature gradient gas mixerSep 23, 19Sep 20, 22General Electric Company
11415079 Turbo-shaft ejector with flow guide ringDec 20, 18Aug 16, 22PRATT & WHITNEY CANADA CORP.
11396896 Variable geometry thrusterAug 24, 17Jul 26, 22JETOPTERA, INC.
11286878 Variable area nozzle exhaust system with integrated thrust reverserMar 31, 20Mar 29, 22Rolls-Royce North American Technologies Inc.; Rolls-Royce Cornoration;
11286814 Exhaust duct of gas turbine engineSep 17, 20Mar 29, 22PRATT & WHITNEY CANADA CORP.
11274632 Nozzle of a turbomachine provided with chevrons with a non-axisymmetric inner faceApr 11, 19Mar 15, 22SAFRAN AIRCRAFT ENGINES
11255239 Exhaust systems and methods for gas turbine engineDec 11, 18Feb 22, 22Honeywell International, Inc.

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2025/0035,068 HIGH-POWER HYBRID-ELECTRIC PROPULSION SYSTEMS AND METHODSDec 02, 22Jan 30, 25ePropelled Inc.
2024/0229,739 AIRCRAFT ENGINE EXHAUST MIXERJan 09, 23Jul 11, 24Not available
2024/0117,828 VARIABLE GEOMETRY THRUSTERMay 03, 23Apr 11, 24Not available
2023/0399,996 Pressure Drag Jet EngineJun 11, 22Dec 14, 23Not available
2021/0088,000 HIGH TEMPERATURE GRADIENT GAS MIXERSep 23, 19Mar 25, 21Not available
2021/0003,095 JET TUBE FOR A TURBOMACHINEJun 30, 20Jan 07, 21Not available
2020/0400,069 TURBINE ENGINE WITH A FLOW SPLITTER HAVING A PROFILE WITH INCLINED SERRATIONSFeb 15, 19Dec 24, 20SAFRAN AIRCRAFT ENGINES
2020/0025,132 GAS TURBINE ENGINE EJECTORDec 20, 18Jan 23, 20Not available
2020/0025,131 FLOW MIXER STIFFENER RING SEGMENTED SPRINGSNov 29, 18Jan 23, 20Not available
2019/0390,631 CMC OXIDE-OXIDE MIXER DESIGNSep 09, 19Dec 26, 19Not available
2019/0218,998 ENGINE ASSEMBLY WITH COMBINED ENGINE AND COOLING EXHAUSTMar 20, 19Jul 18, 19Not available
2019/0203,620 TURBOPROP ENGINE ASSEMBLY WITH COMBINED ENGINE AND COOLING EXHAUSTMar 05, 19Jul 04, 19Not available
2018/0347,421 EXHAUST SYSTEMS AND METHODS FOR GAS TURBINE ENGINEAug 07, 18Dec 06, 18Honeywell International Inc.
2018/0135,556 MIXER FOR AN ENGINE MANUFACTURED FROM AT LEAST ONE COMPOSITE MATERIAL, MANUFACTURING METHOD AND MANUFACTURING DEVICENov 03, 17May 17, 18Not available
2018/0066,604 INTEGRATED TURBINE EXHAUST STRUTS AND MIXER OF TURBOFAN ENGINEAug 09, 17Mar 08, 18PRATT & WHITNEY CANADA CORP.
2017/0328,303 GAS TURBINE ENGINE EXHAUST EJECTOR/MIXERJul 20, 17Nov 16, 17PRATT & WHITNEY CANADA CORP.
2016/0153,398 GAS TURBINE ENGINE EXHAUST MIXERFeb 09, 16Jun 02, 16PRATT & WHITNEY CANADA CORP.
2015/0075,169 INTEGRATED TURBINE EXHAUST STRUTS AND MIXER OF TURBOFAN ENGINEMay 26, 14Mar 19, 15PRATT & WHITNEY CANADA CORP.

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Patents Issued To Date - By Filing Year

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