139207 ⎘
Features, components parts, details or accessories, not provided for in, or of interest apart form groups - ; Air intakes for jet-propulsion plants; Heat or noise insulation Fire protection or prevention
PROPULSION ASSEMBLY COMPRISING AT LEAST ONE PROTECTIVE HOUSING CONFIGURED TO ACCOMMODATE AT LEAST A PORTION OF AN ELONGATED ELEMENT SUCH AS AN ELECTRIC CABLE
#2FUEL LEAK COMBUSTION ASSEMBLY
#3METHOD FOR AUTOMATICALLY CONTROLLING AN AIRCRAFT IN THE EVENT OF A FIRE IN THE ENGINE ZONE AND AN AIRCRAFT
#4POWER TRANSMISSION SYSTEM AND TURBINE FRACTURING DEVICE HAVING SAME
#5HYDROGEN PROPULSION ASSEMBLY COMPRISING A DEVICE FOR INJECTING INERT GAS, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION ASSEMBLY
#6TURBINE ENGINE HAVING A FIRE BOX
#7VENT STACK ASSEMBLIES FOR HYDROGEN DISTRIBUTION SYSTEMS AND RELATED METHODS
#8Aircraft engine assembly for controlling engine oil flow during fire conditions and method for using same
#9EXHAUST NOZZLE ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEM
#10INTEGRATING AN EXTINGUISHER INTO A "FIRE" ZONE OF A TURBOMACHINE
#11PROPULSION ASSEMBLY FOR AN AIRCRAFT
#12AIRCRAFT NACELLE COMPRISING A SEALED BOX STRUCTURE AND A DOOR WHICH OPENS THE BOX STRUCTURE TO THE OUTSIDE
#13FIRE RETARDANT ENGINE CASING APPARATUS
#14Ducted firewall with upper bifi bleed for modulated core ventilation
#15Flammable fluid reservoir
#16ASSEMBLY FOR AN AIRCRAFT, SAID ASSEMBLY HAVING A PYLON AND A RESERVOIR CONTAINING AN EXTINGUISHING AGENT
#17BONDED DOUBLE WALL SEAL ASSEMBLY
#18ENGINE ACCESSORY FIRE SHIELD
#19FIRE SAFETY SYSTEM FOR A TURBOMACHINE COMPRISING MEANS FOR MAINTAINING A COOLING AIR SPEED AND CORRESPONDING TURBOMACHINE
#20Accessory gearbox cover with planar linking member
#21GAS TURBINE FIRE DETECTION SYSTEM INCLUDING COOLING SYSTEM UPSTREAM OF ASPIRATING SMOKE DETECTOR, AND RELATED METHOD
#22SACRIFICIAL FIRE SHIELD FOR SHIELDING AN AIRCRAFT PART
#23Gas turbine fire detection system including cooling system upstream of aspirating smoke detector, and related method
#24AIRCRAFT PROVIDED WITH AN ENGINE AND AN EXHAUST DUCT THAT IS DRAINED AROUND AN EXHAUST NOZZLE OF THE ENGINE
#25Means for handling gaseous fuel
#26Fire suppression systems
#27Cooling system of a compartment of pieces of equipment in a nacelle of an aircraft propelling assembly
#28PURGE SYSTEM FOR A HYDROGEN FUEL SYSTEM
#29FIREWALL ASSEMBLIES FOR HYBRID ELECTRIC AIRCRAFT POWERPLANTS
#30Method for quickly stopping the rotor of a helicopter after landing
#31Fire retardant engine casing apparatus
#32Device and method for stopping an electric machine for a turbine engine
#33Housing having intumescent coating and process of production
#34Means for handling gaseous fuel
#35Sweep flow structures for fuel systems
#36FIRE PROTECTION STRUCTURE
#37Aircraft propulsion assembly having a ventilation system and a fire-fighting system
#38Fire wall and method for opening same
#39Fire resistance device designed to be placed between one end of a mounting strut for an aircraft turbomachine and a cowling of the turbomachine delimiting an inter-flow compartment
#40AIRCRAFT FIREWALL FEEDTHROUGH DEVICE
#41Labyrinth barrier with members constructed of a shape memory material
#42Fire suppression systems
#43Hazardous gas monitoring system
#44RAIL AND TUBE ASSEMBLY
#45Firewall assemblies for hybrid electric aircraft powerplants
#46INSPECTION PORT FOR AN ATTRITABLE ENGINE SUPPORT STRUCTURE
#47Fire resistance device designed to be placed between one end of a mounting strut for an aircraft turbomachine and a cowling of said turbomachine delimiting an inter-flow compartment
#48Passive flame arrestor system
#49Fire resistance device intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartment
#50System and method for gas turbine engine mount with seal
#51Support arrangements, fire and overheat detection systems, and methods of making support arrangements for fire and overheat detection systems
#52Casing assembly
#53Fire seal assemblies for aircraft engines
#54Servitude passage arm for a turbo machine
#55Modulated fire extinguishing vent for a gas turbine engine
#56Engine assembly with cover member
#57Acoustic structure for gas turbine engine
#58Ventilation and extinguishing device for a gas turbine engine
#59Electrical harness
#60Air-fire seal and assembly comprising such a seal
#61Additively manufactured thermally insulating structure
#62SEAL ARRANGEMENT
#63Fire mitigation system for gas turbine engine
#64Quick connect firewall seal for firewall
#65Rear assembly of a turbojet engine nacelle including a fireproof sealing device
#66Engine nacelle heat exchanger
#67Fire suppression systems
#68Titanium alloy compressor case
#69INTERGRATED ENVIRONMENTAL CONTROL SYSTEM MANIFOLD
#70Fairings for power generation machines
#71MULTI-DIRECTIONAL FIRE EXTINGUISHING NOZZLE
#72Rail-mounted fire detection system
#73Gas turbine engine fireproofing
#74Thermal panel with a corrugated ceramic composite sheet having unequal ridge widths
#75Active clearance control for gas turbine engine
#76Device for monitoring a turbine engine of an aircraft
#77Metal fire seals system for aircraft engine mount
#78Air-fire seal and assembly comprising such a seal
#79Isolation of an aircraft turbo engine tank in case of a fire by closing a valve sensitive to the release of an extinguishing agent
#80Fire suppression system with multi-directional pass through nozzle
#81Aircraft fire seal structure and aircraft
#82Ventilation panel with panel silencer for a turbine package enclosure
#83Aircraft seal structure and aircraft
#84Aircraft fire seal structure and aircraft
#85High temperature seals for blanketless inner fixed structure
#86Fire mitigation system for gas turbine engine
#87Multi-directional fire extinguishing nozzle
#88Method for manufacturing of at least one part of an engine component by means of a blank of intumescent material
#89System and method for sealing a fluid system in a safety condition
#90Color varying random event-determining gaming objects
#91Close-out enclosure for panel of a gas turbine engine
#92Coated thermoplastic seal retainer for fire seal test
#93Fire shield integrated to fuel nozzle retaining bracket
#94Electronic module mounting to vibration isolating structure
#95Electrical and mechanical connections through firewall
#96Electronic module mounting to vibration isolating structure
#97Electronic module location for mechanical components
#98Turbine engine including a thermal protection member
#99System and method for protecting the structural integrity of an engine strut
#100Firewall mount hub
#101Test cell for an aircraft turbine engine
#102Double walled tube drainage system
#103Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine
#104Heat resistant fastening systems
#105Fire suppression systems
#106Jet engine with multiple chambers and a bearing chamber support
#107Fire seal for use with a gas turbine engine
#108Aircraft propulsion system having at least one anti-fire tank
#109Integrated environmental control system manifold
#110Casing made of organic matrix composite material that facilitates the discharge of smoke
#111Seals for gas turbine engine nacelle cowlings
#112Aircraft propulsion assembly with fire extinguishing system
#113Fire protection of a fan casing made of composite
#114Fire protection of a part made of a three-dimensional woven composite material
#115Compound engine assembly with confined fire zone
#116ON BOARD INERT GAS GENERATION SYSTEM WITH ROTARY POSITIVE DISPLACEMENT COMPRESSOR
#117Method and system for sealing an annulus
#118Electric conduction structure for jet engine
#119Fire containment apparatuses for aircraft duct assemblies
#120D5/D5A DF-42 double walled exit cone and splash plate
#121Inner bypass duct
#122TURBINE COMPONENTS WITH STEPPED APERTURES
#123Turbine leak detection system
#124Self-modulated cooling on turbine components
#125Coated articles and manufacture methods
#126Gas turbine engine component having shaped pedestals
#127Finned ignitor grommet for a gas turbine engine
#128Ventilation inlet
#129COATING SYSTEMS AND METHODS THEREFOR
#130Gas turbine engine component cooling channels
#131Lightning protection device and method of producing same
#132Articles having reduced expansion and hermetic environmental barrier coatings and methods for their manufacture
#133Fire Shield for a Gas Turbine Engine
#134Fire resistant electrical panel
#135Active clearance control for gas turbine engine
#136SYSTEM FOR DETECTING A FLASHBACK AND MITIGATING DAMAGE FROM THE FLASHBACK TO A COMBUSTION SYSTEM
#137Thrust enabling objective system
#138Flow guiding system and rotary combustion engine
#139Method for Detecting Hazardous Gas Concentrations within a Gas Turbine Enclosure
#140Hazardous gas detection system for a gas turbine enclosure
#141Primary structure for an attachment pylon with firewall and thermal layers
#142Bifurcation fire purge system for a gas turbine engine
#143Acoustic structure for a gas turbine engine
#144Gas turbine engine with a fire wall and an off-take device
#145Firewall, pylon of aircraft, and aircraft
#146Fireshield fastener hood
#147Gas turbine having fuel monitoring
#148Fire suppression systems
#149Flame resistant shield
#150Flexible shield for fluid connectors
#151Multiple piece shroud feedthru enclosure
#152LOWER FIREWALL PLATE GROMMET
#153Turbine leak detection system
#154Fire seal for a gas turbine engine
#155Anti-fire seal assembly and nacelle comprising such a seal
#156Process for producing a run-in coating
#157On board inert gas generation system with rotary positive displacement compressor
#158Mounting system for a nacelle fire detection system
#159High temperature fuel manifold for gas turbine engines
#160Electrical harnesses
#161Fireshield fastener hood
#162HEAT PROTECTION SYSTEM
#163Torque protection device for fire blanket and associated method
#164Fireproof systems in aircraft engines
#165High temperature manifolds for gas turbine engines
#166Ventilation inlet
#167Auxiliary power unit fire enclosure drain seal
#168Auxiliary power unit fire enclosure
#169FIRESEAL
#170METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED USING THIS METHOD
#171Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor
#172METHOD FOR THE MANUFACTURE OF A CIRCULAR REVOLUTION THERMOMECHANICAL PART INCLUDING A TITANIUM-BASED LOAD-BEARING SUBSTRATE LINED WITH STEEL OR SUPERALLOY, A TURBOMACHINE COMPRESSOR HOUSING WHICH IS RESISTANT TO TITANIUM FIRE OBTAINED ACCORDING TO THIS METHOD
#173Method for the manufacture of a circular revolution thermomechanical part including a titanium-based load-bearing substrate lined with steel or superalloy, a turbomachine compressor housing which is resistant to titanium fire obtained according to this method
#174Fireseal
#175Hose arrangement for a gas turbine engine
#176Method for the provision of fire protection for titanium components of an aircraft gas turbine and titanium components for an aircraft gas turbine
#177Aircraft firewall
#178Method for preventing an over temperature condition in a gas turbine engine
#179Flame prevention device
#180Fire suppression systems
#181Fire Warning System
#182Fire suppression systems
#183Fire suppression systems
#184Fire shield method
#185Fire suppression systems
#186Auxiliary power unit with integral firebox
#187Aeroengine oil tank fire protection system
#188Thermal management for aircraft auxiliary power unit compartment
#189Fire shield apparatus and method
#190Inducing windmilling to allow oil flow during fire-induced emergency state
#191Heat resistant joining line seal system
#192Systems and methods for controlling an exhaust system
#193Inert gas generating system