F02K 1/12

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Description

Class  F02K : JET-PROPULSION PLANTS


Subclass 1/12: 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) by means of pivoted flaps

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12146453 Mixed flow exhaust thrust reverser with area control nozzle systems and methodsApr 12, 23Nov 19, 24Rohr Inc.
12110841 Supersonic aircraft and method of reducing sonic booms and jet noiseFeb 22, 22Oct 08, 24Japan Aerospace Exploration Agency
12031445 Variable area nozzle for aircraft propulsion systemMar 07, 22Jul 09, 24Rohr Inc.
12018628 Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing wallsNov 05, 21Jun 25, 24SAFRAN AIRCRAFT ENGINES
12006891 Propulsor wing trailing edge exhaust area controlFeb 24, 22Jun 11, 24Whisper Aero Inc.
11994087 Variable area nozzle and method for operating sameDec 06, 21May 28, 24Rohr Inc.
11988167 Plunger seal apparatus and sealing methodJan 03, 22May 21, 24General Electric Company
11867135 Vectoring exhaust nozzle for an aircraft powerplantSep 14, 22Jan 09, 24RTX CORPORATION
11867136 Variable area nozzle assembly and method for operating sameDec 17, 21Jan 09, 24Rohr Inc.
11840985 Aircraft propulsion system with variable area inletSep 10, 21Dec 12, 23Rohr Inc.
11772809 Fuselage for an aircraft with fuselage-integrated tailplaneNov 27, 21Oct 03, 23Airbus Defence and Space GmbH
11754018 Aircraft propulsion system exhaust nozzle with ejector passage(s)Dec 17, 21Sep 12, 23Rohr, Inc.
11739712 Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle, the flaps of which each comprise a cooling air circulation ductAug 27, 20Aug 29, 23SAFRAN AIRCRAFT ENGINES
11725608 Passively actuated variable area nozzle for an aircraft propulsion systemMay 02, 22Aug 15, 23Rohr, Inc.
11719191 Skirted leaf seal apparatusJun 21, 21Aug 08, 23General Electric Company
11713731 Variable area nozzle and method for operating sameDec 30, 21Aug 01, 23Rohr, Inc.
11713730 Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfacesAug 27, 20Aug 01, 23SAFRAN AIRCRAFT ENGINES
11686272 Aircraft propulsion system with variable area inletSep 10, 21Jun 27, 23Rohr, Inc.
11661905 2D variable-area plug nozzleJan 17, 22May 30, 23Florida Turbine Technologies, Inc.
11585294 High bypass ratio engine bypass duct nozzle with controlled nozzle areaFeb 21, 20Feb 21, 23RAYTHEON TECHNOLOGIES CORPORATION

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2025/0066,015 Exhaust Area and Flow Turning ControlAug 23, 24Feb 27, 25Not available
2025/0052,210 MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODSOct 21, 24Feb 13, 25Rohr Inc.
2024/0295,198 PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROLMay 01, 24Sep 05, 24Not available
2024/0278,906 ADAPTIVE FLUIDIC PROPULSIVE SYSTEMMay 19, 22Aug 22, 24JETOPTERA, INC.
2024/0229,713 AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLETSep 15, 23Jul 11, 24Not available
2024/0191,672 VARIABLE-GEOMETRY CONVERGENT-DIVERGENT EXHAUST NOZZLEAug 15, 23Jun 13, 24Rolls Royce plc
2024/0175,408 EXHAUST NOZZLE AND A METHOD OF OPERATING AN EXHAUST NOZZLEAug 15, 23May 30, 24Rolls Royce plc
2024/0141,852 TURBOJET ENGINE REAR PORTION HAVING AN AUGMENTED A9/A8 NOZZLE AREA RATIOFeb 14, 22May 02, 24SAFRAN AIRCRAFT ENGINES
2024/0092,495 AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLETSep 15, 23Mar 21, 24Not available
2024/0084,762 VECTORING EXHAUST NOZZLE FOR AN AIRCRAFT POWERPLANTSep 14, 22Mar 14, 24Not available
2024/0052,799 JET VECTORING APPARATUSDec 01, 21Feb 15, 24Not available
2023/0220,814 JET ENGINE FOR AIRCRAFTJul 13, 20Jul 13, 23Not available
2022/0325,677 ADJUSTABLE EXHAUST NOZZLE FOR DETONATION ENGINESApr 12, 21Oct 13, 22Not available
2022/0018,309 PASSIVELY ACTUATED VARIABLE AREA NOZZLE FOR AN AIRCRAFT PROPULSION SYSTEMMay 11, 21Jan 20, 22Not available
2020/0025,129 AIRCRAFT NOZZLEFeb 06, 19Jan 23, 20Rolls Royce plc
2019/0345,894 CONVERGENT-DIVERGENT NOZZLE MECHANISMMay 14, 18Nov 14, 19Not available
2019/0316,544 VARIABLE AREA EXHAUST MIXER FOR A GAS TURBINE ENGINEJun 03, 19Oct 17, 19Not available
2019/0226,424 AIRCRAFT NOZZLEJan 15, 19Jul 25, 19Rolls Royce plc
2019/0226,423 AIRCRAFT NOZZLEJan 02, 19Jul 25, 19Rolls Royce plc
2019/0170,088 SYSTEM FOR ACTUATING A PANEL OF A TURBOJET ENGINE NACELLEJan 25, 19Jun 06, 19SAFRAN NACELLES

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Patents Issued To Date - By Filing Year

Average Time to Issuance