F02K 1/28

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
2024/0117,828 VARIABLE GEOMETRY THRUSTERMay 03, 23Apr 11, 24Not available
2023/0184,192 TURBOMACHINE EXHAUST CASEMay 07, 21Jun 15, 23SAFRAN AIRCRAFT ENGINES
2020/0070,961 COMBUSTION-POWERED FLOW CONTROL ACTUATOR WITH HEATED WALLSAug 31, 18Mar 05, 20General Electric Company
2016/0032,863 NOZZLE FOR AN AIRCRAFT TURBOPROP ENGINE WITH AN UNDUCTED FANOct 13, 15Feb 04, 16AIRCELLE
2015/0184,615 METHOD AND THERMAL REACTOR FOR SINGLE-VALVE PROPULSION WITH MULTIPLE INJECTIONS AND COMBUSTIONS PER ROTATION CYCLEJun 05, 13Jul 02, 15Not available
2014/0182,265 Rocket Propulsion Systems, and Related MethodsJan 03, 13Jul 03, 14LASERMOTIVE, INC.
2014/0165,532 System and method for improving the efficiency of a jet engineDec 17, 12Jun 19, 14Not available
2014/0130,503 TURBOFAN ENGINE WITH CONVERGENT - DIVERGENT EXHAUST NOZZLEJul 13, 12May 15, 14Not available
2013/0313,333 SYSTEM OF SUPPORT THRUST FROM WASTED EXHAUSTMay 25, 12Nov 28, 13KING ABDULAZIZ CITY FOR SCIENCE AND TECHNOLOGY
2013/0219,858 TURBINE ENGINE WITH THRUST VECTORING EXHAUST NOZZLEFeb 23, 12Aug 29, 13UNITED TECHNOLOGIES CORPORATION
2012/0256,044 FLIGHT VEHICLE, PROPULSION SYSTEM AND THRUST VECTORING SYSTEMDec 23, 11Oct 11, 12ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
2011/0167,788 THRUST VECTORING APPARATUS FOR A JET ENGINE, CORRESPONDING JET ENGINE, THRUST VECTORING METHOD AND UPGRADING METHOD FOR A JET ENGINEJun 23, 09Jul 14, 11BAE SYSTEMS PLC
2008/0295,481 Fluidic vectoring for exhaust nozzleMay 31, 07Dec 04, 08UNITED TECHNOLOGIES CORPORATION
2008/0104,940 Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the DeviceOct 21, 05May 08, 08VOLVO AERO CORPORATION
2006/0283,188 Suppression of part of the noise from a gas turbine engineJun 26, 06Dec 21, 06Not available
2006/0230,744 Exhaust nozzle for an engine of a flying craftApr 13, 06Oct 19, 06SNECMA
2006/0090,452 Yaw vectoring for exhaust nozzleOct 28, 04May 04, 06UNITED TECHNOLOGIES CORPORATION
2006/0011,411 Acoustic compressorJul 15, 04Jan 19, 06ANEST IWATA CORPORATION
2003/0145,577 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fansFeb 07, 02Aug 07, 03LOCKHEED MARTIN CORPORATION
2002/0157,399 Rocket engine nozzle comprising a jet separation control systemMar 24, 00Oct 31, 02AGENCE SPATIALE EUROPEENNE