An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system.


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    Title :

    Non-propulsive utility power (NPUP) generation system for providing secondary power in an aircraft


    Contributors:

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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    DAVID S KRUG / KAMIAR J KARIMI / THOMAS F CURRIER et al. | European Patent Office | 2015

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    NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT

    KRUG DAVID S / KARIMI KAMIAR J / CURRIER THOMAS F et al. | European Patent Office | 2017

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    NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT

    KRUG DAVID S / KARIMI KAMIAR J / CURRIER THOMAS F et al. | European Patent Office | 2019

    Free access

    NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT

    KRUG DAVID S / KARIMI KAMIAR J / CURRIER THOMAS F et al. | European Patent Office | 2019

    Free access

    NON-PROPULSIVE UTILITY POWER(NPUP)GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT

    KRUG DAVID S / KARIMI KAMIAR J / CURRIER THOMAS F et al. | European Patent Office | 2018

    Free access