|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/1181 ; 244/1371 ; 244/130 ; 244/53 ; B|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 6 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 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 inw...
A fighter aircraft having minimized aerodynamic drag and radar signature without sacrificing flight performance and having a center of gravity, comprising: a fuselage defining a volume of substantially constant cross-section fore to aft for low aerodynamic drag and radar signature penalties and containing the aircraft\s center of gravity; at least one jet engine mounted in the fuselage; 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 th...