|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||24/404.5R ; 24/401.3 ; 24/403.5R|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 34 인용 특허 : 15|
An aircraft structure has an arrangement of aircraft components that provide inherent directional stability for a flight vehicle throughout an angle-of-attack range, even at very high angles-of-attack where conventional means of stabilization are ineffective. Components attached to an aircraft fuselage include a wing, horizontal stabilizers and vertical stabilizers. The wing is mounted forward of the horizontal stabilizers and is carried high on the fuselage. The horizontal stabilizer is mounted toward the rear of the aircraft and is attached near the bo...
[ What is claimed is:] [1.] An aircraft structure to improve directional stability comprising:a fuselage;a wing mounted to said fuselage;a horizontal stabilizer mounted to a bottom of said fuselage, rearward of and at a lower level than said wing, said horizontal stabilizer having trailing edges on opposite side of said fuselage, each trailing edge having an outboard junction with a tip of said horizontal stabilizer and an inboard junction with said fuselage, wherein said horizontal stabilizer sweeps backward;a forwardly sweeping right directional stabil...