|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-001/00 B64C-003/10 B64C-003/36|
|미국특허분류(USC)||244/36 ; 244/35A ; 244/204 ; 244/45R|
|발명자 / 주소|
|인용정보||피인용 횟수 : 14 인용 특허 : 0|
A supersonic flight aircraft having a longitudinally forwardly extending axis in the direction of flight, and a wing, comprising a wing extending generally laterally relative to the axis, and having a leading edge angled forward or rearwardly relative to a normal to the axis at an angle ll
A wing for use on an airplane designed for efficient supersonic flight, said wing having leading and trailing edges, a longitudinal axis extending directionally between said edges, wing tip ends and upper and lower surfaces, said wing having a main portion and a tip portion, a) said main portion of the wing having leading edge sweep angularity l30°at all spanwise locations, wherein said leading edge sweep angularity at any spanwise location is defined as the angle between the tangent to the leading edge of said wing at said location, and the plane normal...