|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 18|
An aircraft designed with three wings located on either side of the fuselage. The forward wing has a downward angle with a curved top and bottom surface. The upper wing is located towards the rear of the aircraft and above the forward wing. The lower wing is located below the upper wing and slightly forward. It is also located to the rear and below of the forward wing. The outer ends of all three wings come into contact at one point. The forward wing uses the Coanda effect to increase the airflow across the top surface of the bottom wing. The aircraft ca...
What is claimed is: 1. An aircraft comprising: a fuselage with a forward end, an aft end and two lateral sides; a pair of coanda each with an inner and outer end; a pair of upper wings each with a leading edge, a top surface, a bottom surface, a Kruger flap, an inner end and an outer end, wherein the Kruger flap is located on the bottom surface aft of the leading edge; and a pair of lower wings each with an inner and outer end; one of the coanda is disposed on either side of the fuselage with the inner ends attached to the lateral sides of the fuselage;...