|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/217 ; 244/090R ; 244/089|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 8 인용 특허 : 4|
Flight controls with automatic balance for use in controlling the movement of an aircraft through a fluid system, the control system includes ailerons divided into two parts, which at lower speed adopt the shape of a conventional aileron and rotate in their entirety with the same degree, and at high speeds a first part of the flap rotates or extends to a determinated angle by an actuator while the second part of the aileron, which is hinged or articulated to the first part of the aileron, rotates with reference to the main part, where the amount of rotat...
[ What is claimed is:] [1.]1. Flight controls with automatic balance comprising: an aileron having a main part and an other part which at low speed adopts the shape of a conventional flight control surface and at high speeds, flexes to a position of least resistance with air speed pressure controlled by an actuator, and said other part is hinged to said main part of said flight control surface, whereby said other part rotates with reference to said main part as a function of air speed pressure incident on said other part; and at least one spring that opp...