发明名称 Rotor blade operating device in airplane and flaperon operating device in airplane
摘要 A flaperon operating device having a center pulley and a slider supported on a center shaft. When the center pulley and the slider are rotated about the center shaft, left and right driving pulleys are rotated in the same direction, whereby left and right flaperons are operated in opposite directions to provide aileron functions. When the slider is slid rearwards on the center shaft by an actuator, the left and right driving pulleys are rotated in opposite directions, whereby both the left and right flaperons are lowered to provide flap functions. If the left and right flaperons are lifted or lowered by a very small angle in the same phase by the actuator, boundary layers on main wings can be controlled to reduce the drag.
申请公布号 US6464175(B2) 申请公布日期 2002.10.15
申请号 US20010903872 申请日期 2001.07.13
申请人 HONDA GIKEN KOGYO KABUSHIKI KAISHA 发明人 YADA WATARU;YAMANOUCHI HIROSHI;UCHIDA MINORU;TADA KATSUTOSHI
分类号 B64C9/00;B64C9/18;(IPC1-7):B64C13/04 主分类号 B64C9/00
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