140332 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
Variable area nozzle assembly
#2Gas turbine engine with axial movable fan variable area nozzle
#3System for controlling speed transition and thrust vectorisation in a multiple-shaped nozzle by secondary injection
#4Split sleeve hidden door thrust reverser
#5Control system
#6Gas turbine engine with axial movable fan variable area nozzle
#7STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS
#8Acoustic cavity tailored synthetic jet
#9Integrated fuel nozzle connection
#10Gas turbine engine bifurcation located fan variable area nozzle
#11Methods and apparatus for sealing variable area fan nozzles of jet engines
#12Thrust vectoring nozzle
#13Fan nacelle trailing edge
#14Gas turbine engine with axial movable fan variable area nozzle
#15Gas turbine engine with axial movable fan variable area nozzle
#16Gas turbine engine with axial movable fan variable area nozzle
#17Variable geometry thruster
#18Gas turbine engine with axial movable fan variable area nozzle
#19Gas turbine engine with axial movable fan variable area nozzle
#20Gas turbine engine with axial movable fan variable area nozzle
#21System and method for flow control in turbine
#22Split sleeve hidden door thrust reverser
#23Gas turbine engine with reversible fan
#24Structural frame integrated with variable-vectoring flow control for use in turbine systems
#25GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE TO REDUCE FAN INSTABILITY
#26Actively controlled cooling air exhaust door on an aircraft engine nacelle
#27Device for controlling a nozzle of variable cross-section of an aircraft
#28Methods and apparatus for passive thrust vectoring and plume deflection
#29Turbojet engine nacelle having a variable nozzle
#30Method and apparatus for variable exhaust nozzle exit area
#31Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle
#32System of support thrust from wasted exhaust
#33Turbofan with variable bypass flow
#34Methods and apparatus for passive thrust vectoring and plume deflection
#35Exhaust nozzle apparatus and method for multi stream aircraft engine
#36Primary cowl of a turbofan comprising a rotating ring having micro-jets
#37Methods and apparatus for sealing variable area fan nozzles of jet engines
#38Exhaust nozzle of a gas turbine engine
#39Integrated thermal protection and leakage reduction in a supersonic air intake system
#40Nacelle with longitudinal translating cowling and rotatable sleeves
#41Gas turbine engine with fan variable area nozzle for low fan pressure ratio
#42GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE
#43GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE FOR LOW FAN PRESSURE RATIO
#44Gas turbine engine with fan variable area nozzle to reduce fan instability
#45Gas turbine engine with fan variable area nozzle for low fan pressure ratio
#46Synthetic jet apparatus
#47Flade discharge in 2-D exhaust nozzle
#48METHOD AND APPARATUS FOR VARIABLE EXHAUST NOZZLE EXIT AREA
#49Gas turbine engine with variable area fan nozzle
#50Gas turbine engine bifurcation located fan variable area nozzle
#51Exhaust plume heat effect reducing method and apparatus
#52Gas turbine engine with axial movable fan variable area nozzle
#53Variable area fan nozzle with bypass flow
#54Thrust vector system
#55Systems and methods for passively directing aircraft engine nozzle flows
#56Actuation system for a translating variable area fan nozzle
#57Translating variable area fan nozzle providing an upstream bypass flow exit
#58Relating to air-breathing flight vehicles
#59System and apparatus for vectoring nozzle exhaust plume from a nozzle
#60Turbofan engine with variable bypass nozzle exit area and method of operation
#61Translating variable area fan nozzle with split beavertail fairings
#62Gas turbine engine having variable flow through a bifurcation having an intake with multiple louvers
#63Nacelle with a displacement device for aircraft jet engine and aircraft including such nacelle
#64Valve system for a gas turbine engine
#65Valve system for a gas turbine engine
#66PROCESS FOR REVERSING THE THRUST PRODUCED BY A PROPULSION UNIT OF AN AIRCRAFT, DEVICE FOR ITS IMPLEMENTATION, NACELLE EQUIPPED WITH SAID DEVICE
#67Bifurcation and aft vent used to vary fan nozzle exit area
#68Gas turbine engine with fan variable area nozzle having a rotational valve system
#69Gas turbine engine with axial movable fan variable area nozzle
#70Bypass turbomachine with artificial variation of its throat section
#71Systems and methods for passively directing aircraft engine nozzle flows
#72Turbofan gas turbine engine and nacelle arrangement
#73Variable area flow duct employing secondary flows, and method therefor
#74Method and system for flow control with arrays of dual bimorph synthetic jet fluidic actuators
#75Method and apparatus for supersonic and shock noise reduction in aircraft engines using pneumatic corrugations
#76Pulsed combustion fluidic nozzle
#77Mixing-enhancement inserts for pulse detonation chambers
#78Thrust vectoring missile turbojet
#79Fladed supersonic missile turbojet
#80Ventilated confluent exhaust nozzle
#81Ventilation system for a convergent divergent exhaust nozzle