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GB/T 43367-2023: General requirements for civil large and medium unmanned helicopter system
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General requirements for civil large and medium unmanned helicopter system
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GB/T 43367-2023
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PDF similar to GB/T 43367-2023
Standard similar to GB/T 43367-2023 GB/T 36258 GB/T 45678 GB/T 35853.4 Basic data | Standard 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 contents
Preface 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 19
Foreword
This 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 systems
1 Scope
This 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 documents
The 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 definitions
The terms and definitions defined in GB/T 35018 and GB/T 38152 apply to this document:
4 General requirements
4:1 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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