|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 244/73 ; R ; 137/151 ; 137/152|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 13 인용 특허 : 8|
The air intake includes two main flaps (1, 2) facing each other and each pivoting about a pin (4, 5) adjacent to a wall (6, 7) extending the flap in question (1, 2) rearwards, and in which a first boundary layer bleed (8a, 8b) is arranged, the pins (4, 5) being substantially parallel to the plane of the wings or of the fuselage so that the flaps (1, 2) move perpendicularly to this plane, and a ramp (11) pivoting about a pin (12) adjacent to its leading edge (11a) by which it is adjacent to the wings and to the fuselage and substantially parallel to the p...
A two-dimensional variable-geometry supersonic and hypersonic air intake, for the combustion air of an aircraft engine, placed under the wings or the fuselage of the aircraft and comprising two main flaps arranged face to face and each movable about a pivot axis situated in the vicinity of one wall of the air intake which extends the main flap in question rearwards, in which wall is arranged a first boundary layer bleed, the pivot axes of the two main flaps being substantially parallel to the plane of the wings or of the fuselage, so that the abovementio...