发明名称 AUTOMATIC FLIGHT CONTROL SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide an automatic flight control system for an airplane capable of greatly simplifying the modifying operation when the system is to be installed in the airplane. SOLUTION: The automatic flight control system 1 is equipped with a navigation device 2 designed to be mounted in an airplane for guiding it following the specified flying route, actuators 3a-3d for driving the control surface of the airplane, and a flight computer 4 to control the actuators 3a-3d. The arrangement further includes a casing 10 to accommodate the navigation device 2, the actuators 3a-3d, and the flight computer 4, a fixing means to fix the casing 10 to the pilot seat S of the airplane, and additional rods 30a-30d for transmitting the driving forces of the actuators 3a-3d to the control surface. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005008059(A) 申请公布日期 2005.01.13
申请号 JP20030175088 申请日期 2003.06.19
申请人 FUJI HEAVY IND LTD 发明人 NAGAYAMA TAKASHI;YONEDA HIROSHI
分类号 B64C13/18;B64C13/16;G05D1/00;(IPC1-7):B64C13/18 主分类号 B64C13/18
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