IEC 62282-4-202-ed.1.0

Detail information

Designation: IEC 62282-4-202-ed.1.0

Publication date: 17/10/2023

Pages: 41

Country: International technical standard

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Anotation

IEC 62282-4-202:2023 covers performance test methods of fuel cell power systems intended to be used to power unmanned aircrafts, including general requirements, start-up, shutdown, power output, continuous running time, electric efficiency, data transmission, warning and monitoring, environmental compatibility, etc. The scope of this document is limited to electrically powered unmanned aircrafts with a maximum take-off mass not exceeding 150 kg (i.e. level 5 or lower unmanned aircrafts (UAs)). This document applies to fuel cell power systems with a rated output voltage not exceeding 220 V DC for outdoor use. This document applies only to compressed gaseous hydrogen-fuelled fuel cell power systems. IEC 62282-4-202:2023 couvre les methodes d’essai des performances des systemes a piles a combustible a utiliser pour alimenter des aeronefs sans pilote et comporte les exigences generales, le demarrage, l’arret, la puissance de sortie, la duree de fonctionnement continu, le rendement electrique, la transmission de donnees, les avertissements et la surveillance, la compatibilite environnementale, etc. Le domaine d’application du present document est limite aux aeronefs sans pilote a propulsion electrique dont la masse maximale au decollage ne depasse pas 150 kg (c’est-a-dire les aeronefs sans pilote de niveau 5 ou inferieur). Le present document s’applique aux systemes a piles a combustible d’une tension de sortie assignee d’au maximum 220 V en courant continu pour utilisation a l’exterieur. Le present document s’applique uniquement aux systemes a piles a combustible utilisant de l’hydrogene gazeux comprime.