140345 ⎘
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT
#2EXHAUST DUCT FOR HYBRID AIRCRAFT POWERPLANT
#3TURBOJET ENGINE NOZZLE RING FOR AN AIRCRAFT
#4Aviation turbofan engine and fan duct nozzle
#5APPARATUS AND METHOD FOR FLUID MANIPULATION
#6Thrust efficient gas turbine engine
#7Aircraft propulsion system nozzle with internal flow passage
#8Exhaust nozzle with vane support structure for a gas turbine engine
#9Exhaust nozzle of a gas turbine engine
#10Aircraft engine exhaust systems enabling reduced length aft strut fairings
#11Method to re-loft a redesigned jet engine primary exhaust nozzle for an existing airplane to provide clearance to aircraft heat shield structure to prevent contact, fracture, and liberation of portions of the nozzle which might cause hazard to continued safe flight
#12Thrust efficient turbofan engine
#13Aerospike Rocket Engine
#14Jet noise suppressor
#15Gas turbine engine exhaust component
#16Drive system for an aircraft
#17Apparatus and method for fluid manipulation
#18Convergent divergent exit nozzle for a gas turbine engine
#19Aircraft with multiple fan propulsion assembly fixed under the wing
#20Aircraft comprising two contra-rotating fans to the rear of the fuselage, with spacing of the blades of the downstream fan
#21Translating nacelle wall for an aircraft tail mounted fan section
#22TURBOFAN ENGINE COMPRISING AN OVERPRESSURE FLAP AT A FAIRING BEING LOCATED AT THE SECONDARY FLOW CHANNEL
#23Turbofan engine comprising a fairing being located in the secondary flow channel and having a separate end element
#24Exhaust duct for turbine forward of fan
#25Turbine engine air guide assembly with improved aerodynamic performance
#26JET ENGINES AND THEIR ARRANGEMENT IN THE REAR SECTION OF AN AIRCRAFT
#27Propulsion assembly for an aircraft, comprising a gas generator and two offset fans
#28Thrust reverser with forward positioned blocker doors
#29Track fairing assembly for a turbine engine nacelle
#30Thrust efficient turbofan engine
#31Convergent divergent exit nozzle for a gas turbine engine
#32Reverse flow single spool core gas turbine engine
#33Twin target thrust reverser module
#34Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion
#35Conjoined reverse core flow engine arrangement
#36Thrust efficient turbofan engine
#37Thrust efficient turbofan engine
#38Thrust efficient turbofan engine
#39De-couple geared turbo-fan engine and aircraft
#40Threaded rod for system for deploying a deployable divergent segment of a thruster
#41Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method
#42Gas turbine engine fan variable area nozzle with swivable insert system
#43Noise reduction system
#44Noise reduction system with chamber
#45Engine exhaust system with directional nozzle
#46Engine exhaust system
#47Exhaust system for gas turbine
#48Variable slope exhaust nozzle
#49METHOD AND APPARATUS FOR SUPPRESSING AEROENGINE CONTRAILS
#50Gas turbine engine fan variable area nozzle with swivalable insert system
#51Hybrid missile propulsion system with reconfigurable multinozzle grid
#52Exhaust nozzle seal with segmented basesheet disposed between side rails
#53Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
#54Turbofan exhaust system