A compound helicopter (1) includes a fuselage (2), a fixed wing (4), a rotary wing (3), and a barrier member 6). The fixed wing (4) is fixed to the fuselage (2). The rotary wing (3) is rotatably coupled to the fuselage (2). The barrier member 6) is attached to a part, of the fuselage (2), that is above the fixed wing (4) and is between the rotary wing (3) and the fixed wing (4). The barrier member 6) is configured to generate no lift upon forward flight.
複合ヘリコプタ
2024-07-03
Patent
Elektronische Ressource
Japanisch
IPC: | B64C AEROPLANES , Flugzeuge |