An aircraft may include a plurality of electrical power systems requiring electrical power, at least one hydraulic power system requiring hydraulic power, at least two main engines, and at least two non-propulsive utility power (NPUP) generation systems. The NPUP generation systems are configured to provide secondary power during operation of the aircraft. The NPUP generation systems are configured to provide at least a portion of the electrical power required by the electrical power system.
NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT
NICHT ANTRIEBSFÄHIGES VERSORGUNGSLEISTUNGSERZEUGUNGSSYSTEM ZUR BEREITSTELLUNG VON SEKUNDÄRER LEISTUNG IN EINEM FLUGZEUG
SYSTÈME DE GÉNÉRATION DE PUISSANCE UTILITAIRE NON-PROPULSIVE (NPUP) POUR LA FOURNITURE DE PUISSANCE SECONDAIRE DANS UN AÉRONEF
2017-02-22
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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