|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 137/152|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 0|
An air intake control for an air utilizing jet aircraft engine. The control is provided with fixed and movable air intake control ramps and the positioning of such movable ramps for air control purposes is determined by the static pressure above one thereof modified by the static pressure of the external air flow, the total pressure and the angle of attack of the aircraft. One control parameter is produced by a device responsive to the relationship between the static pressure above the one movable ramp and the total pressure of the external air flow. Par...
An air intake control for an air intake in an air utilizing engine in a high-powered aircraft having supersonic flight capability, said air intake control comprising: means defining an air intake duct, said air intake duct being free of bypass passageway means for controlling the position of the shock waves ahead of said air intake duct means, movable ramp means mounted in said air intake duct means and being movable across said air intake duct means for controlling the amount of air passing therethrough, a movement of said ramp means toward a closing of...