A ZERO-EMISSION JET ENGINE EMPLOYING A DUAL-FUEL MIX OF AMMONIA AND HYDROGEN USING A WAVE ROTOR REFORMER

An improved power generation system for aircraft and methods of its operation are provided, wherein the system combines a wave reformer providing a contiguous fuel supply to a jet engine, and use of ammonia as the fuel source from which hydrogen and/or a duel supply of ammonia and hydrogen will be s...

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Bibliographische Detailangaben
Hauptverfasser:	TUCHLER, STEFAN, AKBARI, PEJMAN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CHEMISTRY COLLECTION, PRODUCTION OR USE OF HEAT NOT OTHERWISE PROVIDEDFOR COMBUSTION ENGINES COMPOUNDS THEREOF CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INORGANIC CHEMISTRY LIGHTING MECHANICAL ENGINEERING METALLURGY NON-METALLIC ELEMENTS PARACHUTES PERFORMING OPERATIONS RANGES SUPPLYING COMBUSTION ENGINES IN GENERAL, WITH COMBUSTIBLEMIXTURES OR CONSTITUENTS THEREOF TRANSPORTING VENTILATING WEAPONS
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Beschreibung
Zusammenfassung:	An improved power generation system for aircraft and methods of its operation are provided, wherein the system combines a wave reformer providing a contiguous fuel supply to a jet engine, and use of ammonia as the fuel source from which hydrogen and/or a duel supply of ammonia and hydrogen will be supplied to aircraft jet engines leading to a higher thermal efficiency than existing engines with low to no direct emission footprint. L'invention concerne un système de production d'énergie amélioré pour aéronef et des procédés de fonctionnement associés, le système combinant un reformeur à ondes fournissant une alimentation en combustible continue à un moteur à réaction et l'utilisation d'ammoniac comme source de combustible à partir de laquelle de l'hydrogène et/ou une alimentation double d'ammoniac et d'hydrogène seront fournis à des moteurs à réaction d'aéronef conduisant à un rendement thermique plus élevé que les moteurs existants, l'empreinte des émissions directes étant faible ou inexistante.