72605 ⎘
Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for jet engines
FLUIDIC PROPULSIVE SYSTEM
#2AVIATION EQUIPMENT PROTECTION SYSTEM
#3REMOTE MOUNTED ACCESSORY GEARBOX
#4FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#5CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES
#6FLUIDIC PROPULSIVE SYSTEM
#7Fluidic propulsive system and thrust and lift generator for aerial vehicles
#8Aircraft performance optimization based on engine performance monitoring
#9EJECTOR AND AIRFOIL CONFIGURATIONS
#10Configuration for vertical take-off and landing system for aerial vehicles
#11METHOD FOR REPAIRING AN AIR INTAKE LIP
#12Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel
#13Tail cone mounted generator input shaft for an aircraft
#14Aircraft engines with a fuel cell
#15Air direction arrangement for an aircraft with integrated heat exchanger
#16AIRCRAFT PERFORMANCE OPTIMIZATION BASED ON ENGINE PERFORMANCE MONITORING
#17FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
#18Nacelle air intake and nacelle comprising such an air intake
#19Nacelle air intake and nacelle comprising such an air intake
#20Method for preparing a support and for acoustic management on a turbine engine or a nacelle
#21Aircraft engine nacelle with an aft end major axis substantially parallel to the leading edge of a wing
#22Aircraft Structure Having An Inlet Opening For Engine Air
#23AIRCRAFT NACELLE AND ASSOCIATED AIR INTAKE
#24Electrical power generation from turbine engines
#25Diffuser for rotating detonation engine
#26Aircraft comprising a gas turbine engine having an axially adjustable intake and a nacelle
#27Assembly and method for handling an aircraft propulsion unit
#28Airplane providing enhanced aviation and a method to enhance aviation thereof
#29Turbo engine with cooler for cooling inlet air and turbine for expanding cryogenic fuel
#30FLUIDIC PROPULSIVE SYSTEM
#31Winglet ejector configurations
#32Configuration for vertical take-off and landing system for aerial vehicles
#33ACOUSTIC LINER PANEL AND CONTAINMENT FOR A GAS TURBINE ENGINE
#34Acoustic treatment device for an aircraft turbojet engine nacelle
#35Supersonic jet aircraft
#36Fluidic propulsive system and thrust and lift generator for aerial vehicles
#37PULSE COMBUSTOR PERFORMANCE IMPROVEMENT WITH AIRSPEED
#38PROPULSION SYSTEM FOR AN AIRCRAFT, A NOZZLE FOR USE WITH THE PROPULSION SYSTEM, AND A METHOD OF MANUFACTURING A PROPULSION SYSTEM FOR AN AIRCRAFT
#39Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines
#40ACOUSTIC ATTENUATION SYSTEM FOR NACELLE STRUCTURES AND METHOD THEREFOR
#41Fluidic propulsive system and thrust and lift generator for aerial vehicles
#42Airplane without wings
#43Fluidic propulsive system and thrust and lift generator for aerial vehicles
#44Fluidic propulsive system and thrust and lift generator for aerial vehicles
#45Ejector and airfoil configurations
#46Modular aircraft
#47Flight vehicle air breathing engine with isolator having bulged section
#48EJECTOR AND AIRFOIL CONFIGURATIONS
#49Aircraft with multiple fan propulsion assembly fixed under the wing
#50STRUCTURE FOR PROPULSIVE AIRCRAFT ASSEMBLY, ASSOCIATED PROPULSIVE SYSTEM AND ASSEMBLY
#51Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engine
#52Inlet guide vane control for aircraft single engine operation
#53Acoustically-Enhanced Separators for Aircraft Engines
#54System for repairing a fastener equipping a reactor wall
#55WINGLET EJECTOR CONFIGURATIONS
#56Configuration for vertical take-off and landing system for aerial vehicles
#57Nacelle short inlet for fan blade removal
#58Aircraft with a propulsion unit comprising a fan at the rear of the fuselage
#59Ejector and airfoil configurations
#60Fluidic propulsive system
#61Fluidic propulsive system and thrust and lift generator for aerial vehicles
#62Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditions
#63Supersonic caret inlet system
#64Blended Wing Body Boundary Layer Ingesting Inlet Design Integration
#65Air inlet arrangement and method of making the same
#66Nacelle for an aircraft turbojet engine with an extended front lip
#67Bifurcated air inlet housing for a miniature gas turbine engine
#68Aircraft propelled by a turbojet engine with contrarotating fans
#69Rotatable fairing and engine inlet system for high-speed aircraft
#70Gas turbine engine inlet wall design
#71NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE
#72NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE
#73Low shock strength propulsion system
#74Gas turbine engine access panel
#75Airplane including means for taking at least a portion of the boundary layer of the flow of air over a surface
#76Low shock strength propulsion system
#77Air inlet arrangement and method of making the same
#78COUPLING FOR INDUCING HIGH TEMPERATURE DROPS BETWEEN CONNECTED PARTS ON AN AIRCRAFT
#79Low shock strength propulsion system
#80Low shock strength inlet
#81Aircraft engine nacelle inlet having access opening for electrical ice protection system
#82Aircraft engine nacelle inlet having access opening for electrical ice protection system
#83NACELLE WITH ARTICULATING LEADING EDGE SLATES
#84Boundary-layer-ingesting inlet flow control system
#85Aircraft thermal management system with reduced exhaust re-ingestion
#86Aircraft engine nacelle inlet having electrical ice protection system
#87Aircraft engine nacelle inlet having access opening for electrical ice protection system