140316 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto; Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#2ARTICULATABLE DUCTING SYSTEMS
#3MIXED FLOW EXHAUST THRUST REVERSER WITH AREA CONTROL NOZZLE SYSTEMS AND METHODS
#4TURBOJET ENGINE REAR PORTION HAVING AN AUGMENTED A9/A8 NOZZLE AREA RATIO
#5Vectoring exhaust nozzle for an aircraft powerplant
#6Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing walls
#7Mixed flow exhaust thrust reverser with area control nozzle systems and methods
#8Fuselage for an aircraft with fuselage-integrated tailplane
#9Mixed flow exhaust thrust reverser with area control nozzle systems and methods
#10SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#11Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfaces
#12Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle, the flaps of which each comprise a cooling air circulation duct
#13Exhaust nozzle
#14Convergent-divergent nozzle mechanism
#15Composite wear pad for exhaust nozzle
#16Asymmetric load compensation system
#17Nozzle with variable throat and exit areas
#18Impingement cooled nozzle liner
#19Gas turbine engine convergent/divergent exhaust nozzle divergent seal with preloaded dovetail interface background
#20Composite wear pad for exhaust nozzle
#21Asymmetric load compensation system
#22Divergent flap
#23Stepped fairing modulated exhaust cooling
#24Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle
#25Variable nozzle for aeronautic gas turbine engine
#26Variable area nozzle for gas turbine engine
#27Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle
#28Gas turbine engine convergent/divergent exhaust nozzle divergent seal with dovetail interface
#29Compact actuation system for flow nozzle
#30Three stream, variable area, vectorable nozzle
#31Three stream, variable area fixed aperture nozzle with pneumatic actuation
#32Nacelle for an aircraft bypass turbojet engine
#33Engine for use in an aerial vehicle
#34Turbine engine exhaust nozzle flap
#35Convergent-divergent gas turbine nozzle comprising movable flaps having a variable thickness in a lateral direction
#36Linked ring petal actuation for variable area fan nozzle
#37Impingement cooled nozzle liner
#38Variable area fan nozzle and thrust reverser
#39Noise reduction of supersonic jet engines
#40Variable area fan nozzle and thrust reverser
#41Nozzle-area ratio float bias
#42Multifunctional propulsive system for an airplane
#43Variable area fan nozzle and thrust reverser
#44Exhaust nozzle seal with segmented basesheet
#45Aircraft configuration, gas turbine engine, controller and trim system for neutralizing pitching moments with power changes
#46Convergent divergent nozzle with edge cooled divergent seals
#47Nozzle-area ratio float bias
#48Convergent divergent nozzle with slot cooled nozzle liner
#49Rollertrack pivoting axi-nozzle
#50Quick change fastener system for attaching liner bracket to convergent flap and seal in turbine nozzle
#51Pressure balance control for gas turbine engine nozzle
#52Method and device for reducing engine noise
#53Convergent divergent nozzle with interlocking divergent flaps
#54Convergent divergent nozzle with supported divergent seals
#55Turbine engine nozzle
#56Turbine engine nozzle
#57Gas turbine engine and method of operating same
#58System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
#59Turbine engine nozzle
#60Method and device for reducing engine noise
#61Ejector cooled nozzle
#62Turbine engine nozzle
#63Device for supplying cooling air to exhaust nozzle flaps
#64Axial divergent section slot nozzle
#65Convergent/divergent nozzle with modulated cooling
#66Methods and apparatus to reduce turbine engine nozzle basesheet stresses
#67Ventilation system for a convergent divergent exhaust nozzle
#68Convergent-divergent turbojet nozzle
#69Turbine engine nozzle
#70Seal for gimbaling and/or fixed rocket engine nozzles, and associated systems and methods