ガスタービンエンジン出力応答性向上の研究 : 民間ヘリコプタ用小型ターボシャフトエンジンへの適用(熱工学, 内燃機関, 動力など)

抄録

The power response is a very important characteristic for the aircraft engine. Especially for the helicopter, engine power response is essential to the safety at an emergency condition. Here, a new idea of increasing the power response dramatically, with the combination of centrifugal compressor and variable inlet guide vanes, is studied and the verification test results using a small turbo shaft engine is described.