ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Analysis and design of leading edge using metallic thermal protection system
Received date: 2016-05-13
Revised date: 2016-06-02
Online published: 2016-07-22
Leading edge using metallic thermal protection system consists of super alloy honeycomb and thermal insulation felt, duct fastening, which has the function of loading and thermal insulation capacity. The leading edge is easy to be disassembled and maintained, with economic efficiency and safety. The leading edge's loading and thermal insulation capacity are analyzed, then the final structure design is obtained. Super alloy honeycomb has good thermal insulation effect, and has high temperature resistance at 1 200℃. The material of thermal insulation felt maintains excellent thermal insulation effect in high temperature test, so the correctness of heat transfer analysis method is verified. By modeling local heat transfer analysis structure, the leading edge design parameters can be iteratively fixed to achieve the leading edge structure-thermal integrative design.
WANG Man , YANG Jiayong , HE Erfeng , TU Bing . Analysis and design of leading edge using metallic thermal protection system[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(S1) : 53 -58 . DOI: 10.7527/S1000-6893.2016.0176
[1] WILLIAMSEN J, MAHRER K, BOHL W, et al. Meteoroid/orbital debris risk assessment for reusable launch vehicles using metallic TPS:AIAA-2003-1553[R]. Reston:AIAA, 2003.
[2] 姚草根, 吕宏军, 贾新潮, 等. 金属热防护系统材料与结构研究进展[J]. 宇航材料工艺, 2005, 35(2):10-13. YAO C G, LU H J, JIA X C, et al. Development of metallic thermal protection system[J]. Aerospace Materials & Technology, 2005, 35(2):10-13(in Chinese).
[3] BLOSSER M L, CHEN R R, SCHMIDT I H, et al. Advanced metallic thermal protection system development:AIAA-2002-0504[R]. Reston:AIAA, 2002.
[4] 解维华, 张博明, 杜善义. 重复使用飞行器金属热防护系统的有限元分析与设计[J]. 航空学报, 2006, 27(4):650-656. XIE W H, ZHANG B M, DU S Y. Analysis and design of metallic thermal protection systems for reusable launch vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(4):650-656(in Chinese).
[5] 陈战辉, 万小朋, 何林涛, 等. ARMOR热防护系统蜂窝夹层板结构参数设计[J]. 上海航天, 2009, 26(5):56-60. CHEN Z H, WAN X P, HE L T, et al. Design of structural parameters about honeybomb sandwich on ARMOR thermal protection systems[J]. Aerospace Shanghai, 2009, 26(5):56-60(in Chinese).
[6] 南京航空学院. 传热学[M]. 北京:国防工业出版社, 1982:45-80. Nanjing University of Aeronautics and Astronautics. Heat transfer[M]. Beijing:National Defense Industry Press, 1982:45-80(in Chinese).
[7] POTEET C C, ABU-KHAJEEL H, HSU S Y. Preliminary thermal mechanical sizing of metallic TPS process development and sensitivity studies:AIAA-2002-0505[R]. Reston:AIAA, 2002.
/
〈 | 〉 |