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Delivery: <= 5 days. True-PDF full-copy in English will be manually translated and delivered via email. GB/T 43367-2023: General requirements for civil large and medium unmanned helicopter system Status: Valid
Basic dataStandard ID: GB/T 43367-2023 (GB/T43367-2023)Description (Translated English): General requirements for civil large and medium unmanned helicopter system Sector / Industry: National Standard (Recommended) Classification of Chinese Standard: V36 Classification of International Standard: 49.020 Word Count Estimation: 25,242 Date of Issue: 2023-11-27 Date of Implementation: 2024-03-01 Issuing agency(ies): State Administration for Market Regulation, China National Standardization Administration GB/T 43367-2023: General requirements for civil large and medium unmanned helicopter system---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.ICS 49:020 CCSV36 National Standards of People's Republic of China General requirements for civil large and medium-sized unmanned helicopter systems Published on 2023-11-27 2024-03-01 Implementation State Administration for Market Regulation Released by the National Standardization Administration Committee Table of contentsPreface III 1 Scope 1 2 Normative references 1 3 Terms and Definitions 1 4 General requirements 1 4:1 Purpose of use 1 4:2 System composition 1 4:3 System technical indicators 2 4:4 Flight quality 3 4:5 Environmental adaptability 3 4:6 Reliability, maintainability, testability, support and safety 4 4:7 Electromagnetic compatibility 5 4:8 Service life 5 4:9 External colors and markings 5 4:10 Materials 5 4:11 Standard parts 5 4:12 Platform task integration and expansion capabilities 5 4:13 Airworthiness 5 5 Unmanned Helicopter Platform 6 5:1 General characteristics 6 5:2 Body structure 7 5:3 Landing gear 8 5:4 Rotor system 8 5:5 Drive system 9 5:6 Power system 9 5:7 Fuel system 11 5:8 Hydraulic and pneumatic devices 11 5:9 Flight control and management system 11 5:10 Electrical system 13 5:11 Auxiliary take-off and landing equipment (only applicable to ship-borne unmanned helicopters) 14 6 data link 14 6:1 Installation 14 6:2 Performance14 6:3 Antenna and feeder15 6:4 Radio remote control equipment15 6:5 Radio telemetry equipment15 6:6 Radiolocation equipment16 6:7 Information transmission equipment16 6:8 Relay and forwarding equipment 16 7 Task load 16 8 Control Station 16 8:1 General requirements16 8:2 Flight control and management equipment17 8:3 Integrated display system 17 8:4 Map and track display system 17 8:5 Mission planning equipment 17 8:6 Real-time data processing and recording and playback equipment 17 8:7 Communication equipment18 8:8 Human-computer interaction 18 9 Maintenance and maintenance equipment18 9:1 General requirements18 9:2 Line-level support and maintenance equipment18 9:3 Workshop-level support and maintenance equipment18 9:4 Base-level support and maintenance equipment18 10 Storage and transportation requirements 19 11 Test verification 19 11:1 Test purpose 19 11:2 Test category 19 11:3 Test Project 19ForewordThis document complies with the provisions of GB/T 1:1-2020 "Standardization Work Guidelines Part 1: Structure and Drafting Rules of Standardization Documents" Drafting: Please note that some content in this document may be subject to patents: The publisher of this document assumes no responsibility for identifying patents: This document is proposed and coordinated by the National Aircraft Standardization Technical Committee (SAC/TC435): This document was drafted by: China Helicopter Design Institute, China Aviation Comprehensive Technology Institute, China Flight Test Institute, Beijing China Hangzhi Technology Co:, Ltd:, Chinese People's Liberation Army Unit 32370, State Grid Intelligent Technology Co:, Ltd: The main drafters of this document: Wang Peng, Fang Yonghong, Shu Zhenjie, Shen Huanping, Tang Tang, Li Yuqiang, Zhang Zejing, Tu Tianjia, Jiang Taiyu, Hu Yingdong, Liu Fangguo, Fang Yi, Zhou Feihua, Liu Li, Zhang Yang, Zhong Hai, Zhang Fei, Gao Shaonan, Wang Jiuyuan: General requirements for civil large and medium-sized unmanned helicopter systems1 ScopeThis document specifies the purpose, composition, performance, and general quality of civil large and medium-sized unmanned helicopters (hereinafter referred to as "unmanned helicopters") systems: Characteristic requirements, unmanned helicopter platform, data link, mission load, control station requirements, as well as support and maintenance, storage and transportation, test verification Require: This document is applicable to single-rotor unmanned helicopter systems with tail rotors and dual-rotor unmanned helicopter systems with a maximum take-off weight of not less than 150kg: system, other unmanned helicopter systems can be used as reference:2 Normative reference documentsThe contents of the following documents constitute essential provisions of this document through normative references in the text: Among them, the dated quotations For undated referenced documents, only the version corresponding to that date applies to this document; for undated referenced documents, the latest version (including all amendments) applies to this document: GB/T 17626:2 Electromagnetic compatibility test and measurement technology electrostatic discharge immunity test GB/T 17626:3 Electromagnetic compatibility testing and measurement technology Radio frequency electromagnetic field radiation immunity test GB 17799:4 General standard for electromagnetic compatibility Part 4: Emissions in industrial environments GB/T 35018 Classification and classification of civil unmanned aircraft systems GB/T 38152 Unmanned aircraft system terminology HB6490 General specifications for aircraft navigation lights and anti-collision lights HB8591-2020 General requirements for civil light and small fixed-wing unmanned aerial vehicle systems HB20045 General requirements for aerodynamic design of helicopter rotor system blades Aircraft Airworthiness Certification Department of the Civil Aviation Administration of China: Airworthiness Standards for Medium and High Risk Unmanned Helicopter Systems (Trial) [Z]: Regarding the Release of Medium and High Risk Unmanned Helicopter Systems Notice of Helicopter System Airworthiness Standards (Trial) (Civil Aviation Suitability Issue [2020] No: 7): Aircraft Airworthiness Certification Department of the Civil Aviation Administration, 2020-5-11:3 Terms and definitionsThe terms and definitions defined in GB/T 35018 and GB/T 38152 apply to this document:4 General requirements4:1 Purpose of use The purpose of use shall be as specified in 3:1 of HB8591-2020: 4:2 System composition The unmanned helicopter system should consist of the following parts: a) Unmanned helicopter platform, including body structure, landing device, rotor system, transmission system, power system, fuel system, hydraulic and Pneumatic devices, flight control and management systems, electrical systems, auxiliary take-off and landing equipment and other equipment; 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