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An aircraft that includes backup power.

机译:包括备用电源的飞机。

摘要

An aircraft that includes backup power.The aircraft (1) comprises a main power supply (12), a propulsion motor (m, M1... M4) and a standby power supply (14). It includes a pressurized air source (15) and a generator (19) coupled to a turbine (18) connected to the pressurized air source (15).The aircraft includes a controller (10) configured to monitor the operation of the main power supply (12). During normal operation, the controller controls the off state of standby power supply (14) and motor power supply (m, M1... M4) through main power supply (12). If the main power supply (12) fails,The controller controls the activation state of the standby power supply (14) and the motor power supply (m, M1... M4) through the standby power supply (14).Abstract figure: Figure 2
机译:包括备用电源的飞机。飞机(1)包括主电源(12),推进电动机(M,M1 ... M4)和备用电源(14)。它包括加压空气源(15)和连接到连接到加压空气源(15)的涡轮机(18)的发电机(19)。该飞机包括控制器(10),该控制器(10)被配置为监视主电源(12)的操作。在正常操作期间,控制器通过主电源(12)控制备用电源(14)和电动机电源(M,M1 ... M4)的OFF状态。如果主电源(12)发生故障,则控制器通过备用电源(14)控制备用电源(14)和电动机电源(M,M1 ... M4)的激活状态。抽象图:图2

著录项

  • 公开/公告号FR3104333A1

    专利类型

  • 公开/公告日2021-06-11

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (S.A.S.);

    申请/专利号FR20190014085

  • 发明设计人 ALEXANDRE CABOT;ALEXANDRE LESTRUHAUT;

    申请日2019-12-10

  • 分类号H02J9/08;F02C6;B64D41;

  • 国家 FR

  • 入库时间 2022-08-24 19:09:44

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