prBAS EN IEC 62282-4-202:2025

Fuel cell technologies - Part 4-202: Fuel cell power systems for propulsion and auxiliary power units - Unmanned aircrafts - Performance test methods


Opšte informacije
Status:Projekt
Broj stranica:45
Metoda usvajanja:Proglašavanje
Jezik:engleski,francuski
Izdanje:1.
Datum realizacije:17.12.2024
Predviđeni datum naredne faze:23.12.2024
Tehnički komitet:BAS/TC 56, Konvencionalni i alternativni izvori električne energije
ICS:
49.020, Avioni i svemirska vozila općenito
27.070, Gorivi članci

Apstrakt
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.

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EN IEC 62282-4-202:2023, identičan
IEC 62282-4-202:2023, identičan

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