发明名称 AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide an aircraft-mounted antenna device capable of receiving a GPS signal, even in any flying attitude including an attitude of launcher loading, while ensuring not only the directional gain around a machine axis of an aircraft body, but also the directional gains in front and behind the aircraft body. SOLUTION: An antenna device 10 to be mounted on an aircraft 1 rotating at a high speed about a machine axis P comprises: an L-shaped folded antenna 11 formed, by folding a lead wire and including two long parallel wires 12 and two short parallel wires 13 orthogonal with these two long parallel wires 12; and a ground plate 14. The two long parallel wires 12 of the L-shaped folded antenna 11 are connected to a power feeding unit 4 of the aircraft 1, in a state of fixing the two short parallel wires 13 on a top end face 2a of a body 2 of the aircraft 1 along with the machine axis P of the aircraft 1; and the ground plate 14 is fixed along with the machine axis P of the aircraft 1 in an orthogonal contact with the two short parallel wires 13 of the L-shaped folded antenna 11. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006042236(A) 申请公布日期 2006.02.09
申请号 JP20040223025 申请日期 2004.07.30
申请人 IHI AEROSPACE CO LTD 发明人 FUJIWARA EIICHIRO;TANAKA NAOHIRO;MORITA KOJI
分类号 H01Q9/30;F42B15/08;G01S19/36;H01Q1/28;H01Q9/16 主分类号 H01Q9/30
代理机构 代理人
主权项
地址