|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||137/015.2 ; 244/053B|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 15 인용 특허 : 6|
An internal compression engine inlet (39) including a flexible external cowl with leading edge cowl lips (72); a duct comprising a supersonic diffuser (44) defined by upper and lower forward ramps (50), (52), a subsonic diffuser (46) defined by upper and lower aft ramps (54), (56), and a throat region (48); a first slot (58) formed between adjacent ends of the upper forward and upper aft ramps; and a second slot (60) formed between adjacent ends of the lower forward and lower aft ramps, is provided. Each slot (58), (60) opens to a plenum (120), (122) hav...
[ The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:] [1.] A supersonic internal compression engine inlet for an aircraft engine comprising:(a) a supersonic diffuser including an upper forward ramp and a lower forward ramp positioned between opposed sidewalls, each forward ramp having a forward end and an aft end, at least one of the forward ramp forward ends being movable relative to the longitudinal axis of the inlet to provide a variable inlet aperture area;(b) a subsonic diffuser positioned...