Modeling of the boom refueling system and simulation analysis of pressure shock peculiarity of the fuel receptacle

Xiaogang Li, Zhou Zhou, Yonglin Li, Keqiang Cao

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

There is intense pressure shock in the boom refueling system because of the fuel receptacle shutting down suddenly and the fuel flow decreasing to zero soon when the refueling process finished, which the aerial refueling system even flight security will be damaged. In this paper, the software, AMESim will be applied to establish the model of the boom refueling system of a certain type of aircraft, and the influence on the system pressure shock of the fuel receptacle is analyzed in two aspects: The closing time and the close curve.

Original languageEnglish
Title of host publicationProceedings - 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017
EditorsWei Guo, Jose Valente de Oliveira, Chuan Li, Yun Bai, Ping Ding, Juanjuan Shi
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages220-225
Number of pages6
ISBN (Electronic)9781509040209
DOIs
StatePublished - 9 Dec 2017
Event2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017 - Shanghai, China
Duration: 16 Aug 201718 Aug 2017

Publication series

NameProceedings - 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017
Volume2017-December

Conference

Conference2017 International Conference on Sensing, Diagnostics, Prognostics, and Control, SDPC 2017
Country/TerritoryChina
CityShanghai
Period16/08/1718/08/17

Keywords

  • Aerial refueling
  • Boom
  • Fuel receptacle
  • Pressure shock
  • Simulation

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