F02K 1/36

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9863366 Exhaust nozzle apparatus and method for multi stream aircraft engineMar 10, 14Jan 09, 18ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
9758254 Jet noise suppressorNov 11, 14Sep 12, 17THE BOEING COMPANY
9714608 Reduced noise gas turbine engine system and supersonic exhaust nozzle system using elector to entrain ambient airSep 05, 12Jul 25, 17ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
9611807 Gas ejection cone for aircraft turbojet enginesSep 12, 14Apr 04, 17AIRCELLE
9567942 Centrifugal turbomachines having extended performance rangesDec 02, 11Feb 14, 17CONCEPTS NREC, LLC
9239029 Nozzle arrangement for a gas turbine engineJul 31, 08Jan 19, 16AIRBUS DEFENCE AND SPACE GMBH
8887484 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engineJun 23, 09Nov 18, 14BAE SYSTEMS PLC
8844264 Gas turbine engine with ejectorJul 26, 11Sep 30, 14ROLLS-ROYCE CORPORATION
8782896 Method for the manufacture of an ejector nozzle tubeSep 25, 09Jul 22, 14ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
7500353 Eductor swirl busterOct 25, 05Mar 10, 09HONEYWELL INTERNATIONAL INC.
6295805 Exhaust induced ejector nozzle system and methodSep 14, 00Oct 02, 01LOCKHEED MARTIN CORPORATION
6164059 Multi-expansion ejector nozzle with diverging wallsNov 17, 95Dec 26, 00UNITED TECHNOLOGIES CORPORATION
5908159 Aircraft chute ejector nozzleFeb 24, 97Jun 01, 99THE BOEING COMPANY
5435127 Method and apparatus for boosting ram airflow to an ejection nozzleNov 15, 93Jul 25, 95GENERAL ELECTRIC COMPANY
5417057 Thermodynamic driveSep 01, 93May 23, 95Not available
5216879 Propulsion system assemblyAug 30, 91Jun 08, 93UNITED TECHNOLOGIES CORPORATION
5101623 Rocket motor containing improved oxidizer injectorFeb 06, 90Apr 07, 92PRATT & WHITNEY ROCKETDYNE, INC., UNITED TECHNOLOGIES CORPORATION,