140314 ⎘
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 one series of flaps hinged at their upstream ends on a fixed structure
TURBOPROP WITH A VARIABLE AREA NOZZLE EJECTOR
#2PROPULSION MACHINE COMPRISING A SEALING MODULE
#3SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#4VARIABLE AREA NOZZLE ASSEMBLY
#5PROPULSOR WING TRAILING EDGE EXHAUST AREA CONTROL
#6VARIABLE-GEOMETRY CONVERGENT-DIVERGENT EXHAUST NOZZLE
#7EXHAUST NOZZLE AND A METHOD OF OPERATING AN EXHAUST NOZZLE
#8Vectoring exhaust nozzle for an aircraft powerplant
#9JET VECTORING APPARATUS
#10Variable area nozzle for aircraft propulsion system
#11Jet engine for aircraft
#12Variable area nozzle and method for operating same
#13Skirted leaf seal apparatus
#14Passively actuated variable area nozzle for an aircraft propulsion system
#15SEAL FOR GIMBALING AND/OR FIXED ROCKET ENGINE NOZZLES, AND ASSOCIATED SYSTEMS AND METHODS
#16Propulsor wing trailing edge exhaust area control
#17ADJUSTABLE EXHAUST NOZZLE FOR DETONATION ENGINES
#18PASSIVELY ACTUATED VARIABLE AREA NOZZLE FOR AN AIRCRAFT PROPULSION SYSTEM
#19High bypass ratio engine bypass duct nozzle with controlled nozzle area
#20Gas turbine engine bifurcation located fan variable area nozzle
#21Linkage assembly preventing axial rotation of the link rod for a gas turbine engine
#22Supersonic aircraft turbofan
#23Stiffening of the connection between flaps in a nozzle of variable cross section
#24Two-dimensional supersonic nozzle thrust vectoring using staggered ramps
#25System for actuating a panel of a turbojet engine nacelle
#26Linkage assembly preventing axial rotation of the link rod
#27Gas turbine engine bifurcation located fan variable area nozzle
#28Methods and apparatus for sealing variable area fan nozzles of jet engines
#29Thrust vectoring nozzle
#30Telescoping electrical cable
#31Variable area nozzle assisted gas turbine engine restarting
#32Controlling nozzle areas of variable area fan nozzles
#33Variable fan nozzle using shape memory material
#34Nacelle for a turbojet engine with a variable nozzle
#35Thrust reverse variable area fan nozzle
#36Actively controlled cooling air exhaust door on an aircraft engine nacelle
#37Gas turbine engine including a third flowpath exhaust nozzle
#38Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle
#39Aircraft vapour trail control system
#40Thrust deflecting device and aircraft engine
#41FLAP DRIVING DEVICE IN PARTICULAR FOR AN ADAPTIVE NOZZLE
#42Compact actuation system for flow nozzle
#43Three stream, variable area, vectorable nozzle
#44Fan nozzle drive systems that lock thrust reversers
#45Linkage to control and restrain flap movement
#46Pivoting ring petal actuation for variable area fan nozzle
#47Shape memory alloy actuation system for variable area fan nozzle
#48Fan variable area nozzle with cable actuator system
#49Gas turbine exhaust noise reduction
#50Three stream, variable area fixed aperture nozzle with pneumatic actuation
#51Gas turbine engine with compressor inlet guide vane positioned for starting
#52GAS TURBINE ENGINE EXHAUST NOZZLE
#53Methods and apparatus for sealing variable area fan nozzles of jet engines
#54Nacelle for an aircraft bypass turbojet engine
#55Linked ring petal actuation for variable area fan nozzle
#56Assembly including a reverse thrust device and system for actuating said device
#57GAS TURBINE ENGINE WITH COMPRESSOR INLET GUIDE VANE POSITIONED FOR STARTING
#58Integrated thrust reverser actuator and variable area fan nozzle actuator
#59Fan case thrust reverser
#60NACELLE FOR VARIABLE SECTION NOZZLE PROPULSION UNIT
#61Holonomic motion vehicle for travel on non-level surfaces
#62Cable-actuated variable area fan nozzle with elastomeric seals
#63Gas turbine engine exhaust nozzle including a plurality of flaps movable over a flow control surface
#64REDUCED DRAG AFTERBURNER NOZZLE ACTUATION SYSTEM
#65Morphing structure and method
#66Integrated variable geometry flow restrictor and heat exchanger
#67Method of varying a fan duct nozzle throat area of a gas turbine engine
#68Gas turbine engine bifurcation located fan variable area nozzle
#69GAS TURBINE ENGINE HAVING CORE AUXILIARY DUCT PASSAGE
#70Modulating flow through gas turbine engine cooling system
#71Dilating fan duct nozzle
#72Turbofan engine having inner fixed structure including ducted passages
#73TURBOFAN ENGINE
#74Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
#75Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle
#76Bladder type variable area fan nozzle
#77Pivoting fan nozzle nacelle
#78Shape memory alloy actuated adaptive exhaust nozzle for jet engine
#79Gas turbine engine variable area exhaust nozzle
#80System and apparatus for vectoring nozzle exhaust plume from a nozzle
#81CONTROLLING THE AERODYNAMIC DRAG OF A GAS TURBINE ENGINE DURING A SHUTDOWN STATE
#82Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system
#83Operational line management of low pressure compressor in a turbofan engine
#84Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
#85Variable fan nozzle using shape memory material
#86Dilating fan duct nozzle
#87Morphing structure and method
#88Turbofan engine operation control
#89LOW NOISE AIRCRAFT
#90Fan variable area nozzle with cable actuator system
#91FAN VARIABLE AREA NOZZLE WITH ELECTROMECHANICAL ACTUATOR
#92Reduced take-off field length using variable nozzle
#93Method and device to avoid turbo instability in a gas turbine engine
#94Gas turbine engine systems involving variable nozzles with flexible panels
#95Variable area nozzle assisted gas turbine engine restarting
#96Low-leakage seal system for pivot door type thrust reverser
#97Gas turbine engine having core auxiliary duct passage
#98Fan variable area nozzle positional measurement system
#99Aircraft configuration
#100Mode strut and divergent flap interface
#101Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
#102Morphing structure
#103Gas turbine engine nozzle liner with thermally compliant attachment brackets
#104Thermal management system with thrust recovery for a gas turbine engine fan nacelle assembly
#105Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
#106Fan variable area nozzle for a gas turbine engine fan nacelle
#107Adjustment assembly
#108Nozzle assembly for rocket and ramjet applications
#109Gas turbine engine and method of operating same
#110Convergent turbojet exhaust nozzle
#111Reduced radar cross section exhaust nozzle assembly
#112Shape memory alloy actuated adaptive exhaust nozzle for jet engine
#113Thrust vector control
#114Shape changing structure
#115Morphing structure
#116Variable-section turbomachine nozzle
#117Variable-section turbomachine nozzle with a one-piece control lever support
#118Turbo rocket with real carnot cycle
#119Rotary adjustable exhaust nozzle
#120Variable cam exhaust nozzle
#121Flexible flap for a variable-section turbomachine nozzle
#122Long life nozzle flap for aircraft turbojets
#123Propulsion machine comprising a sealing module
#124Vectoring exhaust nozzle for an aircraft powerplant
#125Seal for gimbaling and/or fixed rocket engine nozzles, and associated systems and methods