|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 7 인용 특허 : 4|
The amphibious aircraft has two top mounted wings and an engine having a rear mounted propeller. The aircraft also has a tail having two wings mounted in a V-shaped fashion. Each of the wings has a pivotal tip mounted thereon. The aircraft also has a sponson on each side of the fuselage by way of horizontally mounted struts. The struts and thereby the sponsons are mounted to the aircraft in such a manner so that they are adjustable in their horizontal attitude. The pivotal wing tips at the top mounted wings control the yaw of the aircraft while the adjus...
What is claimed is: 1. An amphibious aircraft having an engine and top wings and a V-tail section, said V-tail consisting of two wings placed in a V configuration, each of the two top wings and the wings in the V-tail section having pivotal wing tips, said airplane further having sponsons having means thereon for adjusting said sponsons in their horizontal attitude. 2. The amphibious aircraft of claim 1, wherein said engine has a rear mounted propeller. 3. The amphibious aircraft of claim 1 including a ventral fence mounted to each end of said wings...