PATR发动机关键技术与性能提升途径初探

推进技术 ›› 2018, Vol. 39 ›› Issue (9): 1921-1927.

• 综述 • 下一篇

PATR发动机关键技术与性能提升途径初探

张蒙正,刘典多,马海波,李光熙,南向谊

西安航天动力研究所，陕西西安 710100,西安航天动力研究所，陕西西安 710100,西安航天动力研究所，陕西西安 710100,西安航天动力研究所，陕西西安 710100,西安航天动力研究所，陕西西安 710100

发布日期:2021-08-15
作者简介:张蒙正，男，博士，研究员，研究领域为组合推进技术。E-mail: zhmzh1101@163.com 通讯作者:刘典多，男，硕士，工程师，研究领域为组合推进技术。

Preliminary Analysis on Critical Technology and Performance Improvement of PATR Engine

Xi’an Aerospace Propulsion Institute，Xi’an 710100，China,Xi’an Aerospace Propulsion Institute，Xi’an 710100，China,Xi’an Aerospace Propulsion Institute，Xi’an 710100，China,Xi’an Aerospace Propulsion Institute，Xi’an 710100，China and Xi’an Aerospace Propulsion Institute，Xi’an 710100，China

Published:2021-08-15

摘要/Abstract

摘要： PATR发动机是针对临近空间高速投放平台、水平起降两级入轨重复使用航天运输器之一级而提出的一种组合发动机。此发动机具有工作速域宽、模态简捷、推质比高及性能优等优点，是组合发动机发展方向之一。介绍了PATR发动机及其特点，分析了影响系统研发的系统设计、高效换热、高效涡轮机、材料及工艺等关键技术。在此基础上，提出了优化系统方案和部件参数等提高发动机性能的途径。

关键词: 预冷空气涡轮火箭；关键技术；性能；途径

Abstract: PATR engine is a combined propulsion system which aims at high speed delivery platform in near space and TSTO horizontal take-off launcher. Because of wide working range, less modal conversion, high thrust weight ratio and superior performance, PATR is a important research direction of combined cycle. The PATR propulsion system and it’s characteristic are introduced, the critical technologies affecting system development are analyzed, including system design, efficient heat transfer, high performance turbomachinery, materials and processes. On this basis, the ways to improve the performance are proposed, such as optimizing system scheme and component parameters.

Key words: Pre-cooling air turbo rocket；Critical technology；Performance；Approach

张蒙正,刘典多,马海波,李光熙,南向谊. PATR发动机关键技术与性能提升途径初探[J]. 推进技术, 2018, 39(9): 1921-1927.

ZHANG Meng-zheng ,LIU Dian-duo,MA Hai-bo,LI Guang-xi,NAN Xiang-yi. Preliminary Analysis on Critical Technology and Performance Improvement of PATR Engine[J]. Journal of Propulsion Technology, 2018, 39(9): 1921-1927.

参考文献

[1] Hendrick P, Saint-Mard M. S.S.T.O. Sizing Analysis with in-Flight LOX Collection[R]. AIAA 96-4492.
[2] Bond W H, Yi A C. Prospects for Utilization of Air Liquefaction and Enrichment System (ALES) Propulsion in Fully Reusable Launch Vehicles[R]. AIAA 93-2025.
[3] Crocker A, White S, Andrews J, et al. Alchemist ACES: Enabling Technology for 2nd and Future Generation Space Transportation[R]. AIAA 2002-4327.
[4] Gubertov A M, Borisov N N, Pritumanov S N, et al. A Compressor LACE as an Engine for a Reusable Single Stage to Orbit Space Transportation System[R]. AIAA 96-4520.
[5] Balepin V V, Cipriano J, Berthus M. Combined Propulsion for SSTO Rocket-From Conceptual Study to Demonstrator of Deep Cooled Turbojet[R]. AIAA 96-4497.
[6] Balepin V, Maita M, Murthy S N B. “Third Way” of Development of SSTO Propulsion[R]. AIAA 96-4495.
[7] Sato T, Tanatsugu N, Hatta H, et al. Development Study of the ATREX Engine for TSTO Spaceplane[R]. AIAA 2001-1839.
[8] Hideyuki Taguchi, Tetsuya Sato. Design Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments[R]. AIAA 2005-3419 .
[9] Mark Hempsell. Progress on SKYLON and SABRE[R]. IAC-13, D2.4, 6x19609, 2013.
[10] Victor F V, Guillermo P. Simulation of a Variable-Combined-Cycle Engine for Dual Subsonic and Supersonic Cruise[R]. AIAA 2011-6110.
[11] 芮长胜, 张超, 越冬峰. 射流预涡轮发动机技术研究及发展[J]. 航空科学技术, 2015, 26(10): 53-59.
[12] 廖孟豪. 英国技术美国“佩刀”——美公布基于“佩刀”发动机两级入轨飞行器概念[J]. 环球飞行, 2016, (9): 64-65.
[13] 刘晓明. BAE系统公司发布高超声速快速响应飞行器作战概念[EB/OL]. http: //www.sohu.com/a/110323100_465915, 2016-08-12.
[14] 廖孟豪. DAPRA授予反作用发动机公司“佩刀”空天发动机预冷器高温考核试验合同[EB/OL]. http: //www.sohu.com/a/194860703_613206, 2017-09-27.
[15] 周军. 佩刀发动机缩比验证机地面试验将在2020年前进行[J]. 飞航导弹, 2016, (8): 2-2.
[16] 邓帆, 谭慧俊, 董昊, 等. 预冷组合动力高超声速空天飞机关键技术研究进展[J]. 推进技术, 2018, 39(1): 1-13. (DENG Fan, TAN Hui-jun, DONG Hao, et al. Progress on Key Technologies of Hypersonic Aerospace Plane with Pre-Cooled Combined Propulsion[J]. Journal of Propulsion Technology, 2018, 39(1): 1-13.)
[17] 张蒙正, 南向谊, 刘典多. 预冷空气涡轮火箭组合动力系统原理与实现途径[J]. 火箭推进, 2016, 42(1):6-12.
[18] Richard V. Heat Exchanger Development at Reaction Engine Ltd[R]. LAC-08, C4.5.2, 2008.
[19] 张友法, 张文文, 郑日恒, 等. 高超声速组合发动机预冷器抗结霜涂层技术研究[J]. 推进技术, 2017, 38(2):463-470. (ZHANG You-fa, ZHANG Wen-wen, ZHENG Ri-heng, et al. Research of Anti-Frosting Coating for Pre-Cooler[J]. Journal of Propulsion Technology, 2017, 38(2): 463-470.)　　　　　　　　　　　　　*　收稿日期:2017-12-11；修订日期:2018-03-09。作者简介:张蒙正,男,博士,研究员,研究领域为组合推进技术。E-mail: zhmzh1101@163.com通讯作者:刘典多,男,硕士,工程师,研究领域为组合推进技术。E-mail: wfl261987@163.com(编辑:梅瑛)

PATR发动机关键技术与性能提升途径初探

Preliminary Analysis on Critical Technology and Performance Improvement of PATR Engine

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 0

编辑推荐

Metrics

本文评价