|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 137/151 ; 244/55 ; 244/15|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 34 인용 특허 : 0|
An air intake system of an aircraft is improved so that a performance of the air intake system will not be degraded even during flight at a large angle of attack and at high mobility of the aircraft while at the same time secretiveness or security of the aircraft against radar beam irradiation from below will be maintained. The air intake system includes a main air intake port provided on an upper surface of the airframe of the aircraft, an auxiliary air intake port provided on a lower surface of the airframe, and a closure member for the auxiliary air i...
In an air intake system for use in an aircraft having an airframe, said air intake system including a main air intake port at an upper surface of the airframe, whereby during normal cruising flight suitable air intake will be through said main air intake port and a lower surface of the airframe will have low reflectiveness of radar beam irradiation from below, but whereby during flight at a large angle of attack and at high maneuverability air turbulence at said main air intake port will prevent suitable air intake therethrough, the improvement comprisin...