To improve operability, in a locking device for detachably locking a shaft member on a locking position against energizing force.
When moving a stopper pin 26A backward in a straight line shape along a shaft member introducing passage 34 formed in a deck side trim 32, the stopper pin 26A slides with a first abutting surface 42 of a cam 38, and the cam 38 rocks upward with a shaft 40 as the center, and the stopper pin 26A is locked on a locking groove 44. When further moving the stopper pin 26A, the stopper pin 26A slides with a second abutting surface 46 of the cam 38, and the cam 38 rocks upward with the shaft 40 as the center, and the stopper pin 26A is inserted into an inlet part 50A of a separating passage 50. Next, when a worker weakens force for gripping a cover or releasing a hand from the cover, the stopper pin 26A is pulled back forward in a straight line shape along the shaft member introducing passage 34 together with the cover by the energizing force of a winding device arranged on a winding shaft of a tono-cover, and slips out of an outlet part 50B of the separating passage 50.
| WO/2010/091845 | FASTENING DEVICE FOR A MODULE ELEMENT IN AN AIRPLANE |
| JPS5869107 | 【考案の名称】締結構造 |
Kato Kazunori
Hiroshi Fukuda
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