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高超声速飞行器的动态热密封技术研究进展

罗艺 牛波 张亚运 龙东辉

宇航材料工艺2024,Vol.54Issue(3):11-21,11.
宇航材料工艺2024,Vol.54Issue(3):11-21,11.DOI:10.12044/j.issn.1007-2330.2024.03.002

高超声速飞行器的动态热密封技术研究进展

Research Progress of Dynamic Thermal Sealing Technology For Hypersonic Vehicle

罗艺 1牛波 1张亚运 1龙东辉1

作者信息

  • 1. 华东理工大学,上海 200237
  • 折叠

摘要

Abstract

Aerodynamic heating caused by high Mach number flight has always been the major factor that restricts the development of aircrafts to higher speed ranges and airspaces.In particular,parts with large dynamic clearance between the engine nozzle and fuselage,and the control rudder of the tail wing,pose a technical challenge for dynamic thermal sealing more difficult than fuselage surface heat protection.Hence,dynamic thermal sealing technology is a critical bottleneck for developing new hypersonic space vehicles.This paper surveys the foreign dynamic thermal sealing technology with examples of X-38 and other aircrafts,reviews its main technical categories and key performance test methods,and finally offers a summary and future outlook on the development of dynamic thermal sealing technology.

关键词

动态热密封/弹簧管密封/陶瓷片密封/密封件测试/热防护技术/高超声速飞行器

Key words

Dynamic thermal sealing/Spring tube sealing/Ceramic sealing/Sealing testing/Thermal protection technology/Hypersonic vehicle

分类

航空航天

引用本文复制引用

罗艺,牛波,张亚运,龙东辉..高超声速飞行器的动态热密封技术研究进展[J].宇航材料工艺,2024,54(3):11-21,11.

宇航材料工艺

OA北大核心CSTPCD

1007-2330

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