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Powder feeding in a powder engine under different gas-solid ratios

  • Chao Li
  • , Xiaofei Zhu
  • , Zhe Deng
  • , Jiangang Yang
  • , Chunbo Hu
  • , Jinjia Wei
  • Xi'an Jiaotong University
  • Shanghai Aerospace System Engineering Research Institute
  • Xi'an Modern Chemistry Research Institute
  • Northwestern Polytechnical University Xian

Research output: Contribution to journalArticlepeer-review

29 Scopus citations

Abstract

It is a key and difficult problem to find the optimal powder-feeding technique in the study of powdered engines. In this paper, the feeding of powder in powder engines at different gas-solid ratios was experimentally investigated. Working characteristics of the classic piston-driven powder feeding system were obtained. A high linear tendency between powder mass flow rate and the minimum throttle channel area is observed from the experiment. The solid-gas mass ratio to maintain a stable powder feeding is approximately valued in range of 34.4–54.6 under different throttle channel areas. The least deviation in the relative powder mass flow rate for the tests is −15% to +8%. Due to the high uncertainty of the gas-solid flow structures at different gas-solid ratios, obvious low-frequency oscillations and high-frequency oscillations exist during the powder feeding process. The frequencies of low-frequency oscillations are mainly 1–3 Hz, while those of high-frequency oscillations are 20–30 Hz and 30–45 Hz in different tests.

Original languageEnglish
Pages (from-to)712-721
Number of pages10
JournalActa Astronautica
Volume189
DOIs
StatePublished - Dec 2021

Keywords

  • Gas-solid ratio
  • Mass flow rate
  • Powder feeding
  • Powdered engine
  • Solid-gas two-phase flow

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