|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-009/00 B64C-009/02 B64C-005/06 B64C-009/12|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 2|
A supplementary control surface structure for airplanes is installed atop the fuselage of an airplane to enhance the roll rate of the airplane and thereby assists in reducing bending loads on the wings by enabling a smaller aileron deflection for a given roll rate. The supplementary control surface structure desirably includes a moveable vertically oriented roll control surface member desirably installed in a vertically oriented fin or strake that extends atop the fuselage from the flight deck to the vertically oriented tail fin. The supplementary contro...
1. A supplementary control surface structure for an airplane, the airplane including a fuselage with wings extending laterally therefrom, the fuselage having a longitudinal axis, a length, and a height relative to the longitudinal axis, and roll control surfaces respectively disposed with the wings, the supplementary control surface structure for an airplane comprising: a moveable vertically oriented roll control surface member for roll control adapted to be disposed atop the fuselage of the airplane along the longitudinal axis thereof, and is adapted to...