|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/006; 244/007.R; 244/007.A; 244/012.4; 244/023.B|
|발명자 / 주소|
|인용정보||피인용 횟수 : 43 인용 특허 : 4|
A single-tilt-rotor VTOL airplanes have a tiltable rotor attached to an elongated power pod containing the collective and cyclical pitch mechanism, and transmission. The power pod is pivotably attached to a base that is slidably mounted on a pair of slotted guide beams attached on top of the roof of the fuselage. The guide beams run longitudinally from the front of the aircraft to past the center of gravity (CG) of the aircraft in order to transport the power pod from the front section to the center section when converting from the horizontal cruising mo...
1. In a VTOL airplane capable of a vertical takeoff and landing mode (VTOL), an autorotation mode wherein the airplane is capable of a steep but controlled and safe descent by means of a large-diameter lift rotor in an absence of engine power, as well as an efficient high-speed horizontal cruising mode, the combination comprising:a pair of wings disposed on opposing lateral sides of the airplane for supporting the airplane in the horizontal mode, said wing having a wing tip and a wing root,a horizontal stabilizing surface and a vertical fin disposed at a...