33th Congress of the International Council of the Aeronautical Sciences

01.2 - Aircraft Design and Integrated System (Applications)

HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA

M. Sugiuraš, Y. Tanabeš, N. Kobikiš, H. Sugawaraš, K. Kimuraš; šJAXA, Japan

An overview on the research of a high-speed compound helicopter carried out in JAXA is presented. A distinctive configuration of a compound helicopter was proposed by JAXA. The main rotor is combined with a fixed wing to generate lift. The torque caused by the main rotor is canceled out by a couple of motor-driven propellers installed on the fixed-wing tips with differential thrusts between them.


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