发明名称 PITCH ANGLE VARIABLE MECHANISM FOR DOUBLE INVERSION WING, AND FLYING DEVICE HAVING DOUBLE INVERSION WING EQUIPPED WITH THE SAME
摘要 PROBLEM TO BE SOLVED: To control a pitch angle of upper and lower rotors by a simple structure, in a pitch angle variable mechanism and a flying device having double inversion wings equipped with the same. SOLUTION: The pitch angle variable mechanism 1 adjusts an pitch angle of the double inversion wings wherein an upper rotor 5 and a lower rotor 6 are respectively fixed to an upper rotating shaft 3 and a lower rotating shaft 4. The pitch angle variable mechanism 1 comprises: a swash plate 7 in which a lower rotating shaft 4 is inserted through a ball joint 7a and to which lifting rods 10, 11, 12 are connected; a lower pitch angle changing mechanism 40 receiving tilting change of the swash plate 7 and changing the pitch angle of the lower rotor 6; a tilting transmitting mechanism 60 converting the tilting change to different direction tilting change for transmitting; and an upper pitch angle changing mechanism 30 receiving the transmitted tilting change and changing the pitch angle of the upper rotor 5. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2005289128(A) 申请公布日期 2005.10.20
申请号 JP20040103974 申请日期 2004.03.31
申请人 NAGASAKI PREFECTURE;ELECTRIC POWER DEV CO LTD;UCHU MOKEI:KK 发明人 ISHIMATSU TAKAKAZU;ZEN HEITOKU;FUJIMOTO KAZUKI;TAGUCHI YOSHINAGA;ONODERA KAZUMOTO;MIZOGAMI TAKAAKI
分类号 B64C27/605;B64C27/10;(IPC1-7):B64C27/605 主分类号 B64C27/605
代理机构 代理人
主权项
地址