|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/053.B; 137/015.1; 244/015|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 2|
A smooth surfaced, submerged air inlet for use generally forwardly of an engine in an aircraft (missile or other air vehicle). The inlet has an opening having wall surfaces adapted to be flush with or inwardly of an aircraft body surface. The wall surfaces of the opening have a leading and outer end in a plane and the surfaces extend inwardly to form an uncovered shallow channel-shaped portion to the inlet, the channel portion deepening inwardly in the trailing direction and continuing into a partial ellipse portion of the opening. The ellipse portion de...
1. An inwardly extending, submerged, smooth surfaced air inlet, comprising: an inlet opening having wall surfaces adapted to be flush with or inwardly of a body surface; said wall surfaces having a leading and outer end in a plane, said wall surfaces extending inwardly and forming an uncovered shallow channel-shaped portion of the inlet; said channel portion deepening inwardly in the trailing direction continuing into an outwardly opening, partial ellipse portion; said partial ellipse portion deepening inwardly as it extends in a trailing direction...