| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a movable lug having a simple, small and lightweight structure and being capable of safely and reliably reducing air resistance by the lug. <P>SOLUTION: The movable lug includes: a pair of lugs 13, which is mounted on an outer surface of a missile, as rotatable around an axial line extending in a direction B perpendicular to the missile axis, which has an opening to receive a hook of an airplane and which is disposed as spaced from each other in the missile axis direction L; a housing section 15 disposed in front or behind each lug 13 in the axis direction L, for housing the lug 13 so as not to protrude from the outer surface of the missile; a coil spring 17 for the lug, which always biasing the lug 13 to rotate toward the housing section 15; a stopper member having a stopper section which engages with a lug projection provided in the lug 13 and holds the lug 13 in a protruding state from the outer surface; and a wire member 23 with one end attached to an airplane and moving the stopper member by the tension so as to allow the stopper section to release the engagement with the lug projection. <P>COPYRIGHT: (C)2012,JPO&INPIT |
