发明名称 |
REMOTE CONTROL TYPE UNMANNED HELICOPTER |
摘要 |
PROBLEM TO BE SOLVED: To improve operation efficiency of a remote control type helicopter by stopping a rotor in a short time after landing, and shortening standby time up to starting replenishing work of fuel from the landing. SOLUTION: A throttle servomotor 10 is controlled by a control signal from a remote control device. When an engine speed of an engine 2 reduces, a main rotor pitch servomotor 7 is interlocked and controlled, and an arm 7-1 is rotated in the arrow 101 direction so that output of the servomotor 7 is transmitted to a motor-driven brake 6 via a wire 9 rotatably joined to the arm 7-1. The motor-driven brake 6 converts the output of the servomotor 7 into braking force to impart the braking force to a transmission input shaft 4. The motor- driven brake 6 starts braking when the engine speed of the engine 2 reduces up to an engine speed N2 not more than an engine speed N1 only for a centrifugal clutch 1 with a pulley to release the connection of the input shaft and an output shaft, and releases the braking when the engine speed of the engine 2 increases up to the N2.
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申请公布号 |
JP2001322598(A) |
申请公布日期 |
2001.11.20 |
申请号 |
JP20000143045 |
申请日期 |
2000.05.16 |
申请人 |
JAPAN AVIATION ELECTRONICS INDUSTRY LTD |
发明人 |
TANAKA MINORU;NAKAMICHI KUNIHIRO;KINUGAWA KAZUHIDE |
分类号 |
B64C27/56;B64C27/04;(IPC1-7):B64C27/56 |
主分类号 |
B64C27/56 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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