F02K 1/40

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2025/0012,233 GAS TURBINE ENGINES COMPRISING PITCHED NOSE SPLITTER STRUCTURES AND AIRCRAFT COMPRISING THE SAMEAug 21, 23Jan 09, 25Honeywell International, Inc.
2024/0254,942 EXHAUST DUCT FOR GAS TURBINE ENGINEMar 01, 24Aug 01, 24Not available
2024/0124,121 AVIATION TURBOFAN ENGINE AND FAN DUCT NOZZLEDec 26, 23Apr 18, 24Not available
2024/0084,763 THRUST ENHANCING DEVICEJan 28, 22Mar 14, 24Not available
2021/0215,121 EXHAUST DUCT AND EXHAUST DUCT ASSEMBLY AND AIRCRAFT USING THE EXHAUST DUCTMar 30, 20Jul 15, 21HANWHA AEROSPACE CO., LTD
2017/0082,062 NOZZLE AND NOZZLE ASSEMBLY FOR GAS TURBINE ENGINESep 23, 15Mar 23, 17GENERAL ELECTRIC COMPANY
2016/0177,872 EXHAUST DUCTDec 17, 15Jun 23, 16PRATT & WHITNEY CANADA CORP.
2016/0169,155 DEVICE FOR CONNECTING TWO SEGMENTS OF A PROPELLING NOZZLEJul 02, 14Jun 16, 16ARIANEGROUP SAS
2016/0131,077 FAIRING FOR A MIXER OF A NOZZLE OF A DUAL-FLOW TURBOMACHINENov 03, 15May 12, 16SNECMA
2016/0076,483 Gas Turbine NozzleSep 11, 14Mar 17, 16GENERAL ELECTRIC COMPANY
2015/0240,745 ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLEApr 30, 14Aug 27, 15UNITED TECHNOLOGIES CORPORATION
2013/0232,949 PRESSURE BALANCED AREA CONTROL OF HIGH ASPECT RATIO NOZZLEMar 09, 12Sep 12, 13UNITED TECHNOLOGIES CORPORATION
2012/0011,828 PROPULSION SYSTEMSep 23, 11Jan 19, 12Not available
2010/0251,724 Aircraft jet engine provided with a device for reducing propulsion jet noiseJan 04, 07Oct 07, 10CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE, UNIVERSITE DE POITIERS,
2010/0205,930 EXHAUST SYSTEM FOR GAS TURBINEMay 07, 08Aug 19, 10HERAKLES
2007/0295,860 Propulsion System, Aircraft Comprising the Propulsion System and an Outlet Device for a Jet EngineOct 20, 05Dec 27, 07VOLVO AERO CORPORATION
2007/0266,712 EXHAUST ASSEMBLY FORMING A HORIZONTAL PROPULSION GAS ELBOW IN AN AIRCRAFTApr 27, 07Nov 22, 07SNECMA
2007/0000,233 THRUST ORIENTING NOZZLEJun 29, 06Jan 04, 07SNECMA