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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/013; 244/036; 244/117.R|
|§371/§102 date||20030814 (20030814)|
|발명자 / 주소|
|인용정보||피인용 횟수 : 21 인용 특허 : 8|
The “Tailed Flying Wing Aircraft” idea represents new aerodynamic concepts for large high subsonic aircraft. Large high subsonic aircraft based on these new aerodynamic concepts are having a significantly higher lift capacity and longer range, as well as a significantly lower fuel consumption of at least two times less than the aircraft based on classical fuselage concept with the same external dimensions. In addition, the aircraft based on the new concepts are having a significantly better longitudinal stability and maneuverability, as well as aerodynam...
1. A large subsonic aircraft having a plane of symmetry and a transverse axis, said transverse axis being perpendicular to said plane of symmetry, said plane of symmetry including a longitudinal and a vertical axis, said longitudinal axis being perpendicular to said vertical axis, said longitudinal axis coinciding with the direction of airflow, said large subsonic aircraft comprising:a) a main body extending along said transverse axis, said main body being composed of a central section, two symmetrical transition sections and two symmetrical external win...