|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/1181 ; 244/1371 ; 244/130 ; ; 89/154|
|발명자 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 5|
A fighter aircraft achieves low aerodynamic drag and radar signature without sacrificing flight performance through a unique arrangement of the air inlets, the weapons bays, and the main landing gear. Separate main and auxiliary weapons bays permit a narrower fuselage than could be be obtained with a single common bay. Also, the auxiliary weapons bays and the landing gear can be aligned outboard of the main weapons bay without needing to increase the length or width of the aircraft. The air intake ducts extend aft from each intake and curve upwardly and ...
A fighter aircraft having minimized aerodynamic drag and radar signature without sacrificing flight performance, comprising a fuselage having a substantially constant width fore to aft; at least one jet engine; a wing connected to the fuselage; at least one air intake for each jet engine; an air intake duct extending from each air intake to the engine; a radar dome mounted on the forward portion of the fuselage, a transparent pilot canopy mounted behind the radar dome, ahead of the wing, above and between the air intakes; a pair of retractable main landi...