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FR3049583A1
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PRESSURE AIR SUPPLY UNIT FOR AIRCRAFT
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FR3047768A1
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DEVICE FOR CONNECTING AND SEALING BETWEEN TWO MODULES OF AN EXHAUST DUCT FROM A TURBOMACHINE
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FR3041607A1
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Pressurized air supply unit for aircraft
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FR3033602A1
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REALIZATION OF SEMI-MONOBLOCK RECTIFIER STAGES, BY ADDITIVE MANUFACTURE
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CA2932936A1
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Suspension of a tubular element in an aircraft compartment
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CA2931771A1
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Adjustable engine suspension for positioning the engine relative to the mount thereof
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FR3027840A1
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PROCESS FOR MANUFACTURING A CERAMIC TURBINE BLADE
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US2016264252A1
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Method and system for generating auxiliary power in an aircraft
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FR3025252A1
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Device and method for starting a gas turbine, method for regulating the rotation speed of a gas turbine, and gas turbine and turbomoteur therefor
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FR3021359A1
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Device and method for preheating fuel in a turbomachine
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FR3020406A1
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DEVICE AND METHOD FOR STARTING AN AUXILIARY GROUP
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FR3017452A1
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HEAT EXCHANGER SYSTEM
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BR112015017917A2
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architecture for providing emergency electrical power for an aircraft, aircraft and method for providing emergency electrical power for an aircraft
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CN104968565A
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Structure for feeding air to an auxiliary power unit in an aircraft
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US2015360630A1
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Method and system for supplying an aircraft with electrical power
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BR112015015441A2
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management process of an aircraft's power grid
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FR3013683A1
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METHOD AND SYSTEM FOR OPTIMIZED PRODUCTION OF NON-PROPULSIVE ENERGY
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CN104781508A
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Device and method for protecting aircraft turbomachine computer against speed measurement errors
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CA2801083A1
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Turbine engine shaft
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FR2998128A1
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TURBO-AIRCRAFT MACHINE CALCULATOR
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