|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/91 ; 244/36 ; 244/87|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 30 인용 특허 : 0|
A high efficiency vertical tail unit is combined with a variable wing geometry for large angles of attack, primarily for all-wing aircraft such as delta-type craft. The vertical tail unit is hinged for adjustment about an axis substantially parallel to the longitudinal axis of the fuselage. The outer wing portions are connected, at an angle, with a vertical tail unit which is directed vertically downward in its normal position. The assembly comprising an outer wing portion and a vertical tail unit is rotatable about the parallel axis whereby three differ...
A high efficiency vertical tail assembly for an all-wing craft having a longitudinal axis and comprising a fuselage and two wings, said wings defining a common plane extending laterally away from said fuselage, each wing having a respective wing tip, said vertical tail assembly consisting of two identical vertical tail units, one vertical tail unit being provided for each of said wing tips, each vertical tail unit consisting of its wing tip (2) and of a vertical tail surface (1) rigidly connected to the wing tip so as to include a given angle (t