|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/045.A; 244/036; 244/117.0R|
|발명자 / 주소|
|인용정보||피인용 횟수 : 2 인용 특허 : 3|
Canarded deltoid main wing aircraft idea allows for design of large supersonic civil and military aircraft with cruising speeds of up to Mach 3 at the altitude of over 25,000 meters. The fuel consumption per unit of payload of such aircraft would be at least twice lower with a longer range of over 50% when compared to existing supersonic aircraft of the same size. Simultaneously, the flight safety and ride quality during takeoff and landing at low speeds would be similar to the existing subsonic passenger aircraft. A low fuel consumption, long range, hig...
We claim: 1. A canarded deltoid main wing aircraft having a symmetry plane and a transversal axis, said transversal axis being perpendicular to said symmetry plane, said symmetry plane including a longitudinal and a vertical axis, said longitudinal axis coinciding with airflow direction, said canarded deltoid main wing aircraft comprising: a. means for aerodynamic lift production, said means for aerodynamic lift production being symmetrical relative to said symmetry plane, the cross-sections of said means for aerodynamic lift production being shaped as ...