Fluid Mechanics and Flight Mechanics

A ramjet based on solid-liquid phase change fuels

  • SUN Weiguo ,
  • SHI Ruihua ,
  • LIN Zuoming ,
  • LIU Daijun ,
  • ZHANG Wenshan ,
  • CAO Junwei ,
  • FAN Zhongguo ,
  • MA Conghui ,
  • FU Zechuan ,
  • LIU Aihua ,
  • TIAN Peng ,
  • QIAN Qinjian ,
  • CHEN Fei ,
  • DUAN Lei ,
  • CUI Jinping ,
  • LIANG Xiaojia
Expand
  • 1. China Airborne Missile Academy, Luoyang 471009, China;
    2. Chinese Aeronautical Establishment, Beijing 100029, China;
    3. Chinese Society of Aeronautics and Astronautics, Beijing 100000, China

Received date: 2018-11-09

  Revised date: 2018-12-11

  Online published: 2019-01-28

Abstract

A novel ramjet based on solid-liquid phase change fuels is proposed. The fuels are solid before operation or during storage conditions and are driven from solid to liquid at operation state through microwave radiation. It improves some of the disadvantages of liquid ramjet. The principle of solid-liquid phase change ramjet is described, the concept of solid-liquid phase change fuels is established, and the index of this kind of ramjet evaluation system is put forward. The design technology of this kind of ramjet, the drive technology of phase change, the characteristics of phase change fuels,and the possible fields of application are described and analyzed. A double lower inlet ramjet based on solid-liquid phase change fuels has been demonstrated at ground tests. The phase change fuels mainly based on straight chain alkane can be stored safely with lower cost, are not afraid of glass transition, and are more suitable to be stored and used in extremely low temperature environments.

Cite this article

SUN Weiguo , SHI Ruihua , LIN Zuoming , LIU Daijun , ZHANG Wenshan , CAO Junwei , FAN Zhongguo , MA Conghui , FU Zechuan , LIU Aihua , TIAN Peng , QIAN Qinjian , CHEN Fei , DUAN Lei , CUI Jinping , LIANG Xiaojia . A ramjet based on solid-liquid phase change fuels[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019 , 40(5) : 122780 -122780 . DOI: 10.7527/S1000-6893.2019.22780

References

[1] FRY R S. A century of ramjet propulsion technology evolution[J]. Journal of Propulsion and Power, 2004, 20(1):27-58.
[2] STECHMAN R C, ALLEN R C. History of ramjet propulsion development at the marquardt company-1944 to 1970:AIAA-2005-3538[R]. Reston, VA:AIAA, 2005.
[3] HEWITT P W. Status of ramjet programs in the United States:AIAA-2008-5265[R]. Reston, VA:AIAA, 2008.
[4] FALEMPIN F. Ramjet/scramjet technology-French capabilities:AIAA-1999-2377[R]. Reston, VA:AIAA, 1999.
[5] MINARD J P, HALLAIS M, FALEMPIN F. Low cost ramjet technology for tactical missile application:AIAA-2002-3765[R]. Reston, VA:AIAA, 2002.
[6] BESSER H L. History of ducted rocket development at Bayern-Chemie:AIAA-2008-5261[R]. Reston, VA:AIAA, 2008.
[7] BESSER H L, WEINREICH H L, KURTH G. Fit for mission-Design tailoring aspects of throttleable ducted rocket propulsion systems:AIAA-2008-5262[R]. Reston, VA:AIAA, 2008.
[8] 巩伦昆, 陈雄, 李唯暄, 等. 固体燃料冲压发动机自持燃烧的影响因素[J]. 航空学报, 2017, 38(7):120821. GONG L K, CHEN X, LI W X, et al. Influencing factors for self-sustained combustion of solid fuel ramjet[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(7):120821(in Chinese).
[9] 单睿子, 曹军伟, 莫展, 等. 基于试验设计的固体火箭冲压发动机燃烧效率规律研究[J]. 航空学报, 2015, 36(9):2859-2868. SHAN R Z, CAO J W, MO Z, et al. Research of solidducted rocket combustion efficiency based on design of experiment methodology[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9):2859-2868(in Chinese).
[10] FAKHRI S, LEE J G, YETTER R A. Atomization and spray characteristics of gelled-propellant simulants formed by two impinging jets:AIAA-2009-5241[R]. Reston, VA:AIAA, 2009.
[11] 张文刚, 王春华, 庞爱民. 膏体富燃料推进剂配方研究[J]. 固体火箭技术, 2008, 31(2):154-156. ZHANG W G, WANG C H, PANG A M. Research on pasty fuel-rich propellant formulation[J]. Journal of Solid Rocket Technology, 2008, 31(2):154-156(in Chinese).
[12] 刘爱华, 崔金平, 孙振华, 等. 膏体推进剂冲压发动机一次燃烧试验[J]. 推进技术, 2012, 33(2):227-231. LIU A H, CUI J P, SUN Z H, et al. Experiment on primary combustion of pasty propellant ramjet[J]. Journal of Propulsion Technology, 2012, 33(2):227-231(in Chinese).
Outlines

/