|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/035.R; 244/199.4; 244/214; 244/216; 244/123.1|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 21 인용 특허 : 23|
A wing for use on a supersonic aircraft that includes an inboard section a central section of the wing outboard of the inboard portion, and an outboard section. The outboard section can be a winglet oriented anhedrally relative to a lateral axis of the supersonic aircraft. Leading edge segments on the inboard section, central section and outboard winglet may have mounted thereon leading-edge flaps. These flaps are adjusted by a control system operable to reposition the leading-edge flaps in order to improve the aerodynamic performance of the supersonic ...
What is claimed is: 1. A supersonic aircraft comprising: a wing, wherein the wing further comprises: an inboard section of the wing adjacent to a fuselage; a central section of the wing outboard of the inboard section; an outboard winglet oriented anhedrally relative to a lateral axis of the supersonic aircraft and outboard of the central section of the wing; a leading edge formed from substantially linear leading edge segments on the central section and outboard winglet, wherein the leading edge segments include a leading edge flap mounted thereon, the...