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Technical requirements for stratospheric airship - Part 2: Propulsion system
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GB/T 44821.2-2024
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Basic data | Standard ID | GB/T 44821.2-2024 (GB/T44821.2-2024) | | Description (Translated English) | Technical requirements for stratospheric airship - Part 2: Propulsion system | | Sector / Industry | National Standard (Recommended) | | Classification of Chinese Standard | V04 | | Classification of International Standard | 49.050 | | Word Count Estimation | 15,112 | | Date of Issue | 2024-10-26 | | Date of Implementation | 2025-05-01 | | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration |
GB/T 44821.2-2024: Technical requirements for stratospheric airship - Part 2: Propulsion system---This is an excerpt. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.), auto-downloaded/delivered in 9 seconds, can be purchased online: https://www.ChineseStandard.net/PDF.aspx/GBT44821.2-2024
Technical requirements for stratospheric airship - Part 2.Propulsion system
General technical requirements for stratospheric airships
Part 2.Propulsion System
Technical requirements for stratospheric airship-
Part 2.Propulsion system
ICS 49.050
CCS V 04
National Standard of the People's Republic of China
Released on October 26, 2024
Implementation on May 1, 2025
State Administration for Market Regulation
The National Standardization Administration issued
Table of Contents
Preface... Ⅲ
Introduction Ⅳ
1 Scope... 1
2 Normative references... 1
3 Terms and Definitions 1
4 Technical Requirements... 2
4.1 Composition 2
4.2 Function... 2
4.3 Performance 2
4.4 Interface... 3
4.5 Environmental Adaptability 4
4.6 Security... 4
4.7 Reliability 4
4.8 Maintainability 5
4.9 Testability 5
4.10 Security 5
5 Verification test... 5
5.1 Test Items 5
5.2 Test requirements 5
6 Labeling, packaging, transportation and storage... 6
6.1 Identification 6
6.2 Packaging 6
6.3 Transportation and storage 6
Appendix A (Informative) Environmental Test Items and Conditions 7
References... 9
Preface
This document is in accordance with the provisions of GB/T 1.1-2020 "Guidelines for standardization work Part 1.Structure and drafting rules for standardization documents"
Drafting is required.
This document is Part 2 of GB/T 44821 "General Technical Requirements for Stratospheric Airships". GB/T 44821 has been published as follows
part.
Part 1.Environmental control systems;
Part 2.Propulsion systems.-
Please note that some of the contents of this document may involve patents. The issuing organization of this document does not assume the responsibility for identifying patents.
This document was proposed and coordinated by the National Technical Committee for Aircraft Standardization (SAC/TC 435).
This document was drafted by. Aerospace Information Innovation Research Institute of the Chinese Academy of Sciences, China Special Aircraft Research Institute, Northwestern Polytechnical University, Shanghai
Micromotor Research Institute, China Aviation Technology Research Institute.
The main drafters of this document are. Qu Zhengyu, Nie Ying, Yang Yanchu, Li Zhaojie, Li Yongxiang, Cai Jingjing, Zhu Rongchen, Zhao Kaibin, Cui Yanxiang,
Liu Yongqi, Zhang Shu, An Guowei, Li Shiqing, Shi Yan, Liu Lili, Wang Haifeng, Qian Er, and Ren Haitao.
introduction
GB/T 44821 "General Technical Requirements for Stratospheric Airships" was formulated to establish a unified system for the development, production and use of stratospheric airships.
Standards will promote the healthy and rapid development of the stratospheric airship field, so as to better meet and serve the economic construction and security needs of my country's near-space.
GB/T 44821 is intended to consist of two parts.
Part 1.Environmental Control System. The purpose is to propose general technical requirements and verification for the environmental control system of stratospheric airships.
The testing as well as labeling, packaging, transportation and storage requirements provide a basis for the design and manufacture of stratospheric airship environmental control systems.
Part 2.Propulsion System. The purpose is to propose general technical requirements, verification tests and
Labeling, packaging, transportation and storage requirements provide a basis for the design and manufacture of stratospheric airship propulsion systems.
General technical requirements for stratospheric airships
Part 2.Propulsion System
1 Scope
This document specifies the composition, function, performance, interface, environmental adaptability,
Technical requirements such as safety, reliability, maintainability, testability, and security, as well as corresponding verification test requirements.
This document is applicable to the design and manufacture of propulsion systems for stratospheric airships driven by pure electric means, and other airships driven by pure electric means,
The propulsion systems of high-altitude balloons and solar-powered aircraft are used for reference.
2 Normative references
The contents of the following documents constitute the essential clauses of this document through normative references in this document.
For referenced documents without a date, only the latest version (including all amendments) applies to this document.
In this document.
GB/T 755 Ratings and performance of rotating electrical machines
GB/T 1311 DC motor test methods
GB/T 2423.27 Environmental testing Part 2.Test methods Test methods and guidance. Temperature/low pressure or temperature/humidity/low
Comprehensive air pressure test
GB/T 2900.25 Electrical terminology - Rotating electrical machines
GB/T 2900.27 Electrical terminology - Small power motors
GB/T 13384 General technical requirements for packaging of electromechanical products
GB/T 43328 Terminology of Aerostats
3 Terms and Definitions
GB/T 755, GB/T 1311, GB/T 2423.27, GB/T 2900.25, GB/T 2900.27, GB/T 13384 and
The terms and definitions defined in GB/T 43328 and the following apply to this document.
3.1
propulsion system
A general term for all devices that provide the propulsion required for the flight of stratospheric airships.
3.2
design airspeed
The airspeed at which a stratospheric airship flies at peak cruising efficiency.
3.3
Rated power
The maximum continuous output power of the propulsion system under nominal conditions.
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