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1 发明目的为了避免搭载在直升机上的有线制导导弹被发射后,因飞机的移动使得光纤断线及光信号传输衰减,本发明谋求增大飞机移动的容许范围。 2 发明的构成如图1所示,将光纤导线14的一端连接在安装于导弹12上的储线装置中的叠绕线圈上,另一端连接在飞机搭载的储线装置22上(见图2)。随着导弹发射后飞行方向的改变,利用导弹上的储线装置和飞机上的储线装置双向放线来减少作用在光纤导线上的张力。例如垂直安
OBJECT OF THE INVENTION In order to prevent a cable guided missile mounted on a helicopter from being emitted and attenuating optical fiber breakage and optical signal transmission due to the movement of the aircraft, the present invention seeks to increase the allowable range of aircraft movement. 1, one end of an optical fiber lead 14 is connected to a winding coil in a stocker mounted on a missile 12, and the other end is connected to a stocker 22 on which an aircraft is mounted (see FIG. 2 ). As the direction of flight changes after the launch of a missile, the tension on the fiber optic conductor is reduced by means of bi-directioning of the reservoir device on the missile and the reservoir device on the aircraft. For example, vertical security