自适应起飞脱落的支撑式插拔连接器系统

详细信息    查看全文 | 推荐本文 |

英文篇名：Self-adaptive Take-off Supporting-feed-connector System 作者：王爱伟 ; 刘忠明 ; 胡亚涛 ; 王建秋 ; 王凤金 英文作者：Wang Ai-wei;Liu Zhong-ming;Hu Ya-tao;Wang Jian-qiu;Wang Feng-jin;Beijing Institute of Space Launch Technology; 关键词：支撑式 ; 插拔连接器 ; 支撑装置 ; 自适应调整 英文关键词：Supporting;;Air-feed connector;;Supporting equipment;;Adjusting self-adaptively 中文刊名：DDYH 英文刊名：Missiles and Space Vehicles 机构：北京航天发射技术研究所; 出版日期：2017-08-10 出版单位：导弹与航天运载技术 年：2017 期：No.354 语种：中文; 页：DDYH201704019 页数：4 CN：04 ISSN：11-3263/V 分类号：85-88

摘要

介绍一种自适应起飞脱落的支撑式插拔连接器系统,由可供气带载分离的气路插拔组合连接器及可自适应运动位置调整的支撑装置组成。该插拔连接器系统具有脱落时与箭上接口无机械解锁动作,脱落可靠性高等特点。研究表明:其平衡式接头能够降低连接器对接脱落时的供气分离力,支撑装置可实现连接器对接及脱落前后的上下、水平随动和滚转及一定角度的俯仰调整功能。
        The system includes the air-feed combined connector separated by pressure air along with the supporting equipment for adjusting self-adaptively. The feed connector system is of the characteristics of none mechanical unlocking action between the connector and the rocket during taking off along with high reliability. The results show that the balanced connector can reduce the separation force for take-off. The supporting equipment can realize the function of the connector moving and rolling in up, down and horizon direction. In addition the action of adjusting for certain angle can also be fulfilled during connecting and taking off.

引文

[1]王瑞铨.运载火箭脐带连接器研讨[J].航天发射技术,2002(3):1-15.
    [2]王瑞铨.长征系列火箭地面发射技术的成就与未来[J].导弹与航天运载技术,2002(5):55-64.
    [3]徐明俊.低温高压自动脱落冷氦连接器研制[J].导弹与航天运载技术,1999(2):26-30.
    [4]王立兴.俄罗斯火箭脐带自动对接技术评析[J].航天发射技术,2003(1):45-50.
    [5]王爱伟.一种平衡式气路插拔连接器的研制[J].导弹与航天运载技术,2015(03):104-106.
    [6]周正伐,等.航天可靠性工程[M].北京:中国宇航出版社,2006.
    [7]杨瑞刚.机械可靠性设计与应用[M].北京:冶金工业出版社,2008.