|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/46 ; 244/45R|
|발명자 / 주소|
|인용정보||피인용 횟수 : 34 인용 특허 : 0|
A staggered channel aircraft having a forward pair of wings and a rearward pair of wings. The forward pair of wings are substantially horizontal and are swept backward from the fuselage to join at their tips the pair of rearward wings. The rearward wings are sloping and are swept backward from their tips to join the fuselage in a substantially triangular-like configuration.
A staggered channel wing-type aircraft comprising: a fuselage with a nose, a passenger section, and an aft section; a propulsion means coupled to said fuselage; a pair of substantially horizontal forward wings having leading and trailing edges, said forward wings and said leading and trailing edges, thereof being swept backward from said fuselage; a pair of sloping rearward wings having leading and trailing edges, each of said rearward wings being attached to its tip to a corresponding tip of said forward wings, said rearward wings and said leading and t...