GB/T 38924.1-2020 English PDF

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GB/T 38924.1-2020: Environmental test methods for civil small and light unmanned aircraft system - Part 1: General principles
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Standard ID	USD	BUY PDF	Lead-Days	Standard Title (Description)	Status
GB/T 38924.1-2020	189	Add to Cart	3 days	Environmental test methods for civil small and light unmanned aircraft system - Part 1: General principles	Valid

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GB/T 36258   GB/T 38924.3   GB/T 38924.4   GB/T 38924.2   

Basic data

Standard ID: GB/T 38924.1-2020 (GB/T38924.1-2020)
Description (Translated English): Environmental test methods for civil small and light unmanned aircraft system - Part 1: General principles
Sector / Industry: National Standard (Recommended)
Classification of Chinese Standard: V35
Classification of International Standard: 49.020
Word Count Estimation: 10,171
Date of Issue: 2020-07-21
Date of Implementation: 2021-02-01
Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration

GB/T 38924.1-2020: Environmental test methods for civil small and light unmanned aircraft system - Part 1: General principles

---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
Environmental test methods for civil small and light unmanned aircraft system--Part 1.General principles ICS 49.020 V35 National Standards of People's Republic of China Environmental test method for civil light and small UAV system Part 1.General 2020-07-21 released 2021-02-01 implementation State Administration for Market Regulation Issued by the National Standardization Management Committee

Table of contents

Preface Ⅲ 1 Scope 1 2 Normative references 1 3 Terms and definitions 1 4 General requirements 2 4.1 Normal test atmospheric conditions 2 4.2 Test condition tolerance 2 4.3 Stability of test temperature 2 4.4 Test equipment calibration requirements 2 4.5 Installation of the device under test 3 4.6 State of the device under test 3 4.7 Equipment test composed of multiple units 3 4.8 Test sequence 3 4.9 Performance requirements of the equipment under test 3 4.10 Collection of test information 3 4.11 Handling of test interruption 4 4.12 Result analysis 5 4.13 Applicability analysis of test results 5

Foreword

GB/T 38924 "Civil Light and Small UAV System Environmental Test Method" is divided into the following parts. ---Part 1.General Provisions; ---Part 2.Low temperature test; ---Part 3.High temperature test; ---Part 4.Temperature and altitude test; ---Part 5.Impact test; ---Part 6.Vibration test; ---Part 7.Damp heat test; ---Part 8.Salt spray test; ---Part 9.Water resistance test; ---Part 10.Sand and dust test; This part is Part 1 of GB/T 38924. This section was drafted in accordance with the rules given in GB/T 1.1-2009. This part was proposed and managed by the National Aircraft Standardization Technical Committee (SAC/TC435). Drafting organizations of this section. China Institute of Aviation Technology, Northwestern Polytechnical University, Shenzhen Corbet Aviation Technology Co., Ltd., Shenzhen DJI Innovation Technology Co., Ltd., Guangdong Taiyi High-tech Development Co., Ltd., State Grid Intelligent Technology Co., Ltd., State Grid Shandong Province Electric Power Company, Ewatt Technology Co., Ltd., Xi'an Aisheng Technology Group Company. The main drafters of this section. Ren Zhanyong, Sun Ruifeng, Jia Wei, Fu Yun, Lu Zhihui, Li Minwei, Shu Zhenjie, Zhu Shu, Zhang Xiaolin, Che Jiaxing, Zhao Guocheng, He Zhikai, Cao Guojie, Yang Yang, Jia Jia, Yang Bo, Huang Shan, Yu Qingsong, Zhou Dazhou, Ye Chuan. Environmental test method for civil light and small UAV system Part 1.General

1 Scope

This part of GB/T 38924 specifies the civil light and small unmanned aerial vehicle (take-off weight between 0.25kg and 150kg) system (including flying And ground station) general requirements for laboratory environmental testing. This section applies to laboratory environmental tests of civil light and small UAV systems.

2 Normative references

The following documents are indispensable for the application of this document. For dated reference documents, only the dated version applies to this article Pieces. For undated references, the latest version (including all amendments) applies to this document. GB/T 35018-2018 Classification and classification of civil unmanned aircraft systems GB/T 38152-2019 Unmanned Aircraft System Terminology HB6167.1-2014 Civil Aircraft Airborne Equipment Environmental Conditions and Test Methods Part 1.General

3 Terms and definitions

GB/T 35018-2018, GB/T 38152-2019 and HB6167.1-2014 defined and the following terms and definitions apply to This document. For ease of use, some terms and definitions in HB6167.1-2014 are listed repeatedly below. 3.1 Maximum duty cycle maximumdutycycle Periodically working equipment is between the longest working time under the maximum rated capacity and the non-working (or in the lowest working capacity) time Relationship. [HB6167.1-2014, definition 3.1] 3.2 Temperature controlled or partially controlled temperature locations The air temperature inside the equipment depends on the environmental control system to keep the space within the specified temperature range. 3.3 Performancestandard Meet the minimum performance requirements of product specifications. 3.4 Totalexcursion The offset of the parameter from the positive maximum value to the negative maximum value. [HB6167.1-2014, definition 3.4] 3.5 Equipment The product that correctly performs the predetermined function is determined by the manufacturer. ......

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