|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/46 ; 244/328 ; 244/329 ; 244/49|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 28 인용 특허 : 0|
A double-pivoting deployment system for aerosurfaces, such as wings or fins, for use on aerospace vehicles. Each aerosurface has an inner segment and an outer segment. The inner segment is pivotally connected at a first axis of rotation to the support structure of the aerospace vehicle. An outer side portion of the inner segment is pivotally connected at a second axis of rotation to an inner side portion of the outer segment. In operation, the outer segment is stowed adjacent to the body of the aerospace vehicle such that the surface plane of the outer s...
In combination with a support structure of an aerospace vehicle, an aerosurface deployment assembly, comprising: (a) an actuating means; (b) a plurality of aerosurfaces, each having an inner segment and an outer segment, wherein each said inner segment is pivotally connected to said support structure at an axis of rotation substantially perpendicular to the longitudinal axis of the aerospace vehicle, and wherein an outer side portion of each said inner segment is pivotally connected to an inner side portion of each said outer segment at an axis of rotati...