{"id":445522,"date":"2024-10-20T08:42:14","date_gmt":"2024-10-20T08:42:14","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-en-iec-62282-4-2022023\/"},"modified":"2024-10-26T16:11:57","modified_gmt":"2024-10-26T16:11:57","slug":"bs-en-iec-62282-4-2022023","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-en-iec-62282-4-2022023\/","title":{"rendered":"BS EN IEC 62282-4-202:2023"},"content":{"rendered":"
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.<\/p>\n
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2<\/td>\n | undefined <\/td>\n<\/tr>\n | ||||||
5<\/td>\n | Annex ZA (normative)Normative references to international publicationswith their corresponding European publications <\/td>\n<\/tr>\n | ||||||
6<\/td>\n | English CONTENTS <\/td>\n<\/tr>\n | ||||||
8<\/td>\n | FOREWORD <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | INTRODUCTION <\/td>\n<\/tr>\n | ||||||
11<\/td>\n | 1 Scope 2 Normative references 3 Terms and definitions <\/td>\n<\/tr>\n | ||||||
13<\/td>\n | 4 Fuel cell power system requirements for UAs 4.1 System configuration <\/td>\n<\/tr>\n | ||||||
14<\/td>\n | 4.2 Appearance and structure 4.3 General technical requirements Figure 1 \u2013 General configuration of a fuel cell power system for UAs <\/td>\n<\/tr>\n | ||||||
15<\/td>\n | 5 Test preparation 5.1 General 5.2 Test environment 5.3 Test equipment and accuracy Table 1 \u2013 Test equipment and accuracy <\/td>\n<\/tr>\n | ||||||
16<\/td>\n | 6 Test methods 6.1 Start-up time 6.2 Time to achieve rated power output 6.3 Rated power output 6.4 Continuous running duration 6.5 Peak power output <\/td>\n<\/tr>\n | ||||||
17<\/td>\n | 6.6 Output voltage range 6.7 Electric efficiency 6.8 Start-up and shutdown methods 6.9 Shutdown time <\/td>\n<\/tr>\n | ||||||
18<\/td>\n | 6.10 Acoustic noise level 6.11 Data transmission Figure 2 \u2013 Acoustic noise measurement points for fuel cell power system Table 2 \u2013 Acoustic noise level correction <\/td>\n<\/tr>\n | ||||||
19<\/td>\n | 6.12 Enclosure H2 concentration 6.13 H2 concentration in fuel exhaust 6.14 Enclosure IP code 6.15 H2 leakage rate <\/td>\n<\/tr>\n | ||||||
20<\/td>\n | 6.16 Warning and monitoring <\/td>\n<\/tr>\n | ||||||
21<\/td>\n | Annex A (informative)Suggested aging test procedure for a fuel cell power system for a UA Table A.1 \u2013 Suggested aging test procedure for a fuel cell power system for a UA <\/td>\n<\/tr>\n | ||||||
22<\/td>\n | Annex B (informative)Guidelines for test reports B.1 General B.2 Title page B.3 Table of contents B.4 Summary report <\/td>\n<\/tr>\n | ||||||
23<\/td>\n | B.5 Detailed report B.6 Full report <\/td>\n<\/tr>\n | ||||||
24<\/td>\n | Bibliography <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Fuel cell technologies – Fuel cell power systems for propulsion and auxiliary power units. Unmanned aircrafts. Performance test methods<\/b><\/p>\n |