|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/00324; 244/00321; 244/049|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 11 인용 특허 : 13|
A locking and unlocking mechanism for moveable control fins extending from the surface of a missile. The locking mechanism includes a pin extending thru the outer surface of the missile into an opening provided in the movable fin. A link is pivotally connected between each of the pins and a slide member disposed internally of the missile and carried by a guide. The links are in a close to dead center position when the pins are extended into the openings in each of the fins. A striker assembly is disposed within the slide member and includes a rod carryin...
1. A locking and unlocking mechanism for use on a missile having a plurality of movable control fins extending from an outer surface thereof, said mechanism comprising:a locking pin for each movable control fin adapted to extend through said outer surface into an opening in said control fin to retain said control fin in a fixed position prior to said missile being activated; a slide member movable between a pin extend and a pin retract position; a plurality of links, one for each locking pin, coupling each said pin to said slide member; each of said link...