F02K 1/30

Technology



back to "F02K 1/30" profile

More Results

Showing 1 to 20 of 37 results

Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9989009 Methods and apparatus for sealing variable area fan nozzles of jet enginesOct 31, 12Jun 05, 18The Boeing Company
9970387 Variable area fan nozzle with bypass flowAug 07, 08May 15, 18Rohr Inc.; GOODRICH ACTUATION SYSTEMTS LIMITED;
9957900 System and method for flow control in turbineMay 11, 15May 01, 18General Electric Company
9885313 Gas turbine engine bifurcation located fan variable area nozzleJan 05, 12Feb 06, 18UNITED TECHNOLOGIES CORPORATION
9879636 System of support thrust from wasted exhaustJul 01, 15Jan 30, 18KING ABDULAZIZ CITY FOR SCIENCE AND TECHNOLOGY
9863366 Exhaust nozzle apparatus and method for multi stream aircraft engineMar 10, 14Jan 09, 18ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.
9822732 Gas turbine engine with axial movable fan variable area nozzleNov 23, 16Nov 21, 17UNITED TECHNOLOGIES CORPORATION
9783315 Nacelle with longitudinal translating cowling and rotatable sleevesFeb 24, 12Oct 10, 17ROHR, INC.
9784212 Gas turbine engine with axial movable fan variable area nozzleNov 23, 16Oct 10, 17UNITED TECHNOLOGIES CORPORATION
9771893 Gas turbine engine with axial movable fan variable area nozzleNov 23, 16Sep 26, 17UNITED TECHNOLOGIES CORPORATION
9759133 Turbofan with variable bypass flowMar 06, 14Sep 12, 17ROLLS-ROYCE CORPORATION
9732700 Methods and apparatus for passive thrust vectoring and plume deflectionSep 25, 14Aug 15, 17THE BOEING COMPANY
9701415 Gas turbine engine with axial movable fan variable area nozzleDec 08, 11Jul 11, 17UNITED TECHNOLOGIES CORPORATION
9657685 Device for controlling a nozzle of variable cross-section of an aircraftMay 05, 14May 23, 17AIRBUS OPERATIONS SAS
9617954 Primary cowl of a turbofan comprising a rotating ring having micro-jetsSep 24, 12Apr 11, 17SNECMA
9587583 Turbojet engine nacelle having a variable nozzleFeb 05, 14Mar 07, 17AIRCELLE
9546618 Methods and apparatus for passive thrust vectoring and plume deflectionOct 24, 13Jan 17, 17THE BOEING COMPANY
9494084 Gas turbine engine with fan variable area nozzle for low fan pressure ratioDec 30, 11Nov 15, 16UNITED TECHNOLOGIES CORPORATION
9403600 Integrated thermal protection and leakage reduction in a supersonic air intake systemMay 01, 12Aug 02, 16LOCKHEED MARTIN CORPORATION
9297334 Exhaust nozzle of a gas turbine engineMay 25, 12Mar 29, 16KING ABDULAZIZ CITY FOR SCIENCE AND TECHNOLOGY

Showing 1 to 20 of 37 results