标准解读
《GB/T 44821.2-2024 平流层飞艇通用技术要求 第2部分:推进系统》这一标准详细规定了平流层飞艇推进系统的各项技术指标和技术要求。它旨在为设计、制造、测试及使用平流层飞艇推进系统提供一套统一的技术规范,以确保该类飞行器能够安全有效地执行其预定任务。
标准首先定义了适用于本文件的关键术语和定义,明确了“推进系统”的范围包括但不限于发动机、螺旋桨、控制系统等组成部分。接着,从性能参数出发,列出了推进系统应满足的基本条件,比如功率输出、燃料效率、噪音水平以及排放标准等,并对这些参数设定了具体的数值或等级要求。
在安全性方面,《GB/T 44821.2-2024》强调了推进系统必须具备良好的可靠性和冗余设计,以应对可能出现的各种故障情况;同时,还特别关注于防火防爆措施的设计与实施,确保即使在极端条件下也能保障乘员的生命安全。
此外,该标准也涵盖了关于环境适应性的考量,指出推进系统需能够在广泛的温度范围内正常工作,并且对于湿度、振动等外界因素具有足够的抵抗能力。另外,还提到了电磁兼容性问题,要求整个推进系统在运行时不会干扰到其他电子设备的正常运作。
如需获取更多详尽信息,请直接参考下方经官方授权发布的权威标准文档。
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- 2025-05-01 实施





文档简介
ICS
49.050
CCS
V04
中华人民共和国国家标准
GB/T44821.2—2024
平流层飞艇通用技术要求
第2部分:推进系统
Technicalrequirementsforstratosphericairship—
Part2:Propulsionsystem
2024-10-26发布2025-05-01实施
国家市场监督管理总局发布
国家标准化管理委员会
GB/T44821.2—2024
目次
前言
·····································································································
Ⅲ
引言
·····································································································
Ⅳ
1
范围
··································································································
1
2
规范性引用文件
······················································································
1
3
术语和定义
···························································································
1
4
技术要求
······························································································
2
4.1
组成
······························································································
2
4.2
功能
······························································································
2
4.3
性能
······························································································
2
4.4
接口
······························································································
3
4.5
环境适应性
······················································································
4
4.6
安全性
···························································································
4
4.7
可靠性
···························································································
4
4.8
维修性
···························································································
5
4.9
测试性
···························································································
5
4.10
保障性
··························································································
5
5
验证试验
······························································································
5
5.1
试验项目
·························································································
5
5.2
试验要求
·························································································
5
6
标识、包装、运输和贮存
············································································
6
6.1
标识
······························································································
6
6.2
包装
······························································································
6
6.3
运输和贮存
······················································································
6
附录A(资料性)
环境试验项目和条件
······························································
7
参考文献
··································································································
9
Ⅰ
GB/T44821.2—2024
前言
本文件按照GB/T1.1—2020《标准化工作导则第1部分:标准化文件的结构和起草规则》的规
定起草。
本文件是GB/T44821《平流层飞艇通用技术要求》的第2部分。GB/T44821已经发布了以下
部分:
—第1部分:环境控制系统;
—第2部分:推进系统。
请注意本文件的某些内容可能涉及专利。本文件的发布机构不承担识别专利的责任。
本文件由全国航空器标准化技术委员会(SAC/TC435)提出并归口。
本文件起草单位:中国科学院空天信息创新研究院、中国特种飞行器研究所、西北工业大学、上海
微电机研究所、中国航空综合技术研究所。
本文件主要起草人:屈正宇、聂营、杨燕初、李兆杰、李永祥、才晶晶、祝榕辰、赵凯彬、崔燕香、
刘永奇、张树、安国维、李世庆、时岩、刘丽丽、王海峰、钱儿、任海涛。
Ⅲ
GB/T44821.2—2024
引言
GB/T44821《平流层飞艇通用技术要求》的制定是为了建立平流层飞艇研制、生产、使用的统一
标准,促进平流层飞艇领域健康快速发展,从而更好地满足和服务我国临近空间经济建设和安全需求。
GB/T44821拟由两个部分构成。
—第1部分:环境控制系统。目的在于针对平流层飞艇环境控制系统提出通用的技术要求、验证
试验以及标识、包装、运输和贮存要求,为平流层飞艇环境控制系统的设计与制造提供依据。
—第2部分:推进系统。目的在于针对平流层飞艇推进系统提出通用的技术要求、验证试验以及
标识、包装、运输和贮存要求,为平流层飞艇推进系统的设计与制造提供依据。
Ⅳ
GB/T44821.2—2024
平流层飞艇通用技术要求
第2部分:推进系统
1范围
本文件规定了采用纯电方式驱动的平流层飞艇推进系统的组成、功能、性能、接口、环境适应性、
安全性、可靠性、维修性、测试性、保障性等技术要求以及相应的验证试验要求。
本文件适用于采用纯电方式驱动的平流层飞艇推进系统的设计与制造,其他采用纯电方式的飞艇、
高空气球和太阳能飞机的推进系统参照使用。
2规范性引用文件
下列文件中的内容通过文中的规范性引用而构成本文件必不可少的条款。其中,注日期的引用文
件,仅该日期对应的版本适用于本文件;不注日期的引用文件,其最新版本(包括所有的修改单)适用
于本文件。
GB/T755旋转电机定额和性能
GB/T1311直流电机试验方
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