Conducto de sangrado de aeronave en material compuesto

Un conducto no recto para conducir fluidos a temperaturas superiores a 280ºC y presiones superiores a 4 bares hecho de un material compuesto que comprende capas de un tejido de fibra de carbono y una resina de alta temperatura inyectada o infundida en dichas capas, caracterizado por que el tejido de...

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Bibliographische Detailangaben
Hauptverfasser:	DELGADO, Sofía, NOGUEROLES VINES, Pedro, BAUTISTA DE LA LLAVE, César, MARTIN MORENO, Zulima, REDONDO CARRACEDO, Francisco José, TEJEDOR FOGUET, Sergio, LOPEZ ROMANO, Bernardo
Format:	Patent
Sprache:	spa
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CHEMISTRY COMBUSTION ENGINES COMPOSITIONS BASED THEREON CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JOINTS OR FITTINGS FOR PIPES LIGHTING MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONSONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS MEANS FOR THERMAL INSULATION IN GENERAL MECHANICAL ENGINEERING METALLURGY ORGANIC MACROMOLECULAR COMPOUNDS PARACHUTES PERFORMING OPERATIONS PIPES SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING THEIR PREPARATION OR CHEMICAL WORKING-UP THERMAL INSULATION IN GENERAL TRANSPORTING USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES ASCOMPOUNDING INGREDIENTS WEAPONS
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