A feasibility study of a new ARTEX engine system of AFT-turbine configuration

Kousuke Isomura*, Junsuke Omi, Nobuhiro Tanatsugu, Tetsuya Sato, Hiroaki Kobayashi

*この研究の対応する著者

研究成果査読

6 被引用数 (Scopus)

抄録

A feasibility of ATREX (Air-Turbo-Ram Expander cycle) engine with conventional aft-turbine configuration has been studied to be developed in about 10 years, if the development project has started under enough resources. The novel tip-turbine of the original ATREX engine is replaced by a conventional aft-turbine, and the maximum turbine inlet temperature (TIT) is reduced to 1200K, to realize the engine by only using approved metal technologies of modern jet engines. The capability of the performance has been shown by parametric studies by changing components' design parameters. The study shows that the performance of the ATREX engine is not less than that of pre-cooled turbo jet. Some technical issues on developing the new ATREX engine have been addressed. The most important issue would come from the transient total temperature change due to the rapid acceleration from sea level static (SLS) condition (288K) to Mach 6 at 30km of altitude (1680K) in 6 minutes. The deformation due to transient thermal expansion has to be controlled. Especially, the change of the tip clearance and the clearance between rotors and stators are pointed out to be important design issues. The ATREX engine, which has shorter axial length and simpler rotor, has structural advantage over turbo jet.

本文言語English
ページ(範囲)153-160
ページ数8
ジャーナルActa Astronautica
51
1-9
DOI
出版ステータスPublished - 2002 7 1
外部発表はい

ASJC Scopus subject areas

  • 航空宇宙工学

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