IGTC-95 Installation and Operation of the FJR710 Engine in the NAL-QSTOL "ASUKA"(Session C-7 AEROENGINE OPERATION)

この論文をさがす

説明

The Quiet STOL research aircraft "ASUKA" which has been developed by the National Aerospace Laboratory since 1977, made its first flight in October, 1985. It is powered by four Japanese FJR710/600S turbofan engines installed in an upper-surface-blowing (USB) propulsive lift system. The FJR710/600S is the latest and slightly modified version of the FJR710/600 prototype engine developed under a National Research and Development Program of MITI from 1971 to 1982. Although it was relatively immature engine, the NAL-QSTOL required a very complex engine installation with a confluent exhaust system. Extensive testing and analysis, including full-scale ground rig tests of the propulsion system, were carried out. The flight tests of the engine in a FTB aircraft were also executed. ASUKA's flight tests are now in progress. The present paper describes the installation and operation features of the FJR710/600S engine in the NAL-QSTOL ASUKA, with some detailed discussions on leading test results and improvements applied to the engine.

収録刊行物

詳細情報 詳細情報について

  • CRID
    1571135652308279680
  • NII論文ID
    110006691911
  • NII書誌ID
    AA12007658
  • 本文言語コード
    en
  • データソース種別
    • CiNii Articles

問題の指摘

ページトップへ