|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/003.27; 244/003.28; 244/003.29; 102/384|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 14|
Actuators already present as an integral part of the control systems of missiles and the like are used to activate and control the deployment of fins and the like without the need for separate explosively or mechanically driven fin deployment systems. Springs located in hinges on the fins accomplish the complete deployment of the fins after proper orientation by the actuators.
1. A system for the deployment of guidance devices from the body of guided ordnance comprising:A) a missile body having a longitudinal dimension;B) a plurality of actuators in % aid body;C) a plurality of fins about the periphery of said body each comprising:I) a main body;II) a first end proximate connected to one of said actuators via a shaft; andIII) a distal end remote from said first end;each of said fins being capable of longitudinal rotation by the action one of said actuators on one of said shafts;D) a plurality of slots equal in number to said f...