|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/3240 ; 244/329|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 0|
An apparatus for and method of depolying a movable aerosurface of an aerial vehicle from a folded position to an unfolded, operative flight position. The aerosurface, such as a fin for example, includes a pivotal base member and a control surface connected to the base member for movement relative thereto. An actuator effects pivotal movement of the aerosurface at a predetermined angular rate of deployment. During the initial depolyment cycle the control surface is deflected relative to the base member in a direction and manner imparting aerodynamic force...
An aerodynamic deployment apparatus comprising: an aerosurface mounted on an aerial vehicle for in-flight movement relative thereto from a folded position to an unfolded position; said aerosurface having a base member and a control surface; means mounting said base member on said aerial vehicle for pivotal movement relative thereto; said control surface mounted on said base member for movement relative thereto; actuating means for pivoting said base member to initiate deployment of said aerosurface at a predetermined angular rate; and means for deflectin...