|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/036; 244/117.0R; 244/198|
|발명자 / 주소|
|인용정보||피인용 횟수 : 16 인용 특허 : 15|
“T-tailed Deltoid Main Wing” idea allows for design of high-subsonic passenger aircraft with a capacity between 200 and 650 passengers with outer dimensions fitting within 80 m box on class VI airports while having more than twice lower fuel consumption per unit of payload when compared to the present classical-concept aircraft with fuselage that have the same passenger capacity. T-tailed deltoid main wing aircraft is satisfying all safety requirements for a passenger aircraft while having over 50% longer range than the aircraft of equivale...
We claim: 1. A T-tailed deltoid main wing aircraft having a vertical symmetry plane oriented in airflow direction, said T-tailed deltoid main wing aircraft comprising: a. means for aerodynamic lift production, said means for aerodynamic lift production being symmetrical relative to said symmetry plane, said means for aerodynamic lift production including a main wing, two symmetrical outer wings, and two symmetrical wing transition sections, said main wing being the central section of said means for aerodynamic lift production, the main wing trailing edg...