F02K 1/34

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Description

Class  F02K : JET-PROPULSION PLANTS


Subclass 1/34: Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) using fluid jets to influence the jet flow for attenuating noise

Recent Patents

Patent #TitleFiling DateIssue DatePatent Owner
12263954 MufflerJul 30, 20Apr 01, 25Orbital Australia Pty Ltd
12162618 Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methodsOct 10, 22Dec 10, 24Boom Technology, Inc.
12110841 Supersonic aircraft and method of reducing sonic booms and jet noiseFeb 22, 22Oct 08, 24Japan Aerospace Exploration Agency
12044194 Propulsion system architectureMar 06, 20Jul 23, 24General Electric Company
12030660 Systems and methods for supressing noise from an aircraft engineMay 07, 21Jul 09, 24Embry. Riddle Aeronautical University Inc.
12018838 Cowl assembly for a gas turbine engineJun 21, 22Jun 25, 24General Electric Company
12017785 Aircraft exhaust muffler with a vacuum insulationNov 15, 21Jun 25, 24AIRBUS Operations S.L.
12006855 Muffler for small enginesJun 29, 20Jun 11, 24ORBITAL AUSTRALIA PTY LTD
11867077 Acoustic structure with floating interior skinJun 07, 21Jan 09, 24Rohr Inc.
11859534 Profiled structure and associated turbomachineFeb 15, 19Jan 02, 24SAFRAN AIRCRAFT ENGINES
11788489 Thrust reverser cascade including acoustic treatmentApr 03, 20Oct 17, 23SAFRAN AIRCRAFT ENGINES
11732626 Mixer and mobile bodyDec 15, 22Aug 22, 23Honda Motor Co. Ltd.
11719192 Acoustic attenuation panel for an aircraft jet engine nacelleNov 24, 20Aug 08, 23SAFRAN NACELLES
11718403 Extremely quiet short take-off and landing (STOL) aircraftApr 15, 15Aug 08, 23Northrop Grumman Systems Corporation
11719189 Flexible sleeve for adjustable fan duct nozzleFeb 04, 21Aug 08, 23SPIRIT AEROSYSTEMS INC.
11713732 Laminates of polysilazane and carbon fiber reinforced polymerMay 16, 22Aug 01, 23THE BOEING COMPANY
11710472 In-seat active noise cancellation system for moving vehiclesJun 11, 21Jul 25, 23AVATRONICS SA
11572189 Acoustic absorption structure comprising a liquid drainage system and propulsive assembly comprising such an acoustic absorption structureNov 26, 19Feb 07, 23Airbus Operations SAS
11519302 Internal structure of a primary exhaust duct having a separator of which the geometry varies depending on the temperatureFeb 22, 21Dec 06, 22Airbus Operations SAS
11512666 Acoustic treatment structure for an aircraft propulsion unit nacelleJul 06, 20Nov 29, 22Safan Nacelles; SAFRAN CERAMICS;

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2024/0360,793 ACOUSTIC PANEL WITH ACTIVE IMPEDANCE CONTROLApr 27, 23Oct 31, 24Not available
2024/0344,487 PROPULSION SYSTEM ARCHITECTUREMay 28, 24Oct 17, 24Not available
2024/0327,017 Exhaust System for Aerial VehicleJun 13, 24Oct 03, 24Not available
2024/0253,804 ACOUSTICALLY-TREATED AIR EJECTION NOZZLE FOR A NACELLEApr 05, 24Aug 01, 24SAFRAN NACELLES
2024/0217,668 ENGINE EXHAUST CENTER BODY WITH ACOUSTIC ATTENUATIONJan 03, 24Jul 04, 24Not available
2024/0101,264 REDUCED BULK ACOUSTIC TREATMENT PANEL FOR A TURBOJET ENGINEDec 14, 21Mar 28, 24SAFRAN AIRCRAFT ENGINES
2024/0077,046 EXHAUST CENTERBODY ASSEMBLYSep 02, 22Mar 07, 24Not available
2024/0034,481 ACTIVE SOUND ATTENUATION FOR AIRCRAFT ELECTRICAL SYSTEMJul 29, 22Feb 01, 24Not available
2023/0365,246 ACOUSTIC PANEL FOR AN AIRCRAFT PROVIDING NOISE ATTENUATION OVER A WIDE FREQUENCY BAND BY COMBINING TWO RESONATORS, AND ACOUSTIC PANEL MANUFACTURING METHODMay 03, 23Nov 16, 23Not available
2023/0211,890 MULTI-CORE ACOUSTIC PANEL FOR AN AIRCRAFT PROPULSION SYSTEMJan 04, 23Jul 06, 23Not available
2022/0380,060 VARIABLE MIXING NOZZLE DESIGN FOR JET NOISE REDUCTIONMay 31, 22Dec 01, 22Not available
2022/0055,765 Exhaust System For Aerial VehicleAug 23, 21Feb 24, 22Not available
2021/0301,760 RECONFIGURABLE EXHAUST NOZZLE FOR A GAS TURBINE ENGINEMar 31, 20Sep 30, 21Not available
2021/0031,935 SUPERSONIC AIRCRAFT AND METHOD OF REDUCING SONIC BOOMSMar 25, 19Feb 04, 21Not available
2020/0400,076 ACTIVE DEVICE FOR ATTENUATING ACOUSTIC EMISSIONS FOR A TURBOJET ENGINE INCLUDING CONTROLLED TURBINESSep 08, 20Dec 24, 20SAFRAN NACELLES
2019/0152,618 RING OF TURBOJET VANES INCLUDING AN ACOUSTIC TREATMENT STRUCTURENov 09, 18May 23, 19SAFRAN AIRCRAFT ENGINES
2018/0148,187 ACOUSTIC ATTENUATION STRUCTURE WITH A PLURALITY OF ATTENUATION DEGREES FOR A PROPULSION ASSEMBLY OF AN AIRCRAFTJan 31, 18May 31, 18SAFRAN NACELLES
2017/0297,733 Unmanned HelicopterSep 28, 16Oct 19, 17Ewatt Technology Co., Ltd.
2016/0215,727 AFTERBODY FOR A MIXED-FLOW TURBOJET ENGINE COMPRISING A LOBED MIXER AND CHEVRONS WITH A NON-AXISYMMETRIC INNER SURFACESep 09, 14Jul 28, 16SNECMA
2015/0233,298 REDUCTION IN JET FLAP INTERACTION NOISE WITH GEARED TURBINE ENGINEFeb 22, 13Aug 20, 15UNITED TECHNOLOGIES CORPORATION

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Patents Issued To Date - By Filing Year

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