|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 0|
The present invention relates to an air inlet for a nacelle of a jet engine with a front fan, comprising an upper part (115S), a lower part (115I), an inner lateral part (115int) and an outer lateral part (ext), defining a leading edge (115) between an external wall (111) of the nacelle and an internal wall (113) forming the air supply channel of the jet engine. According to the invention, the air inlet is characterized in that the leading edge of the outer lateral part (115ext) is to the rear with respect to the leading edge of the inner lateral part (1...
The invention claimed is: 1. An air inlet for a nacelle of a jet engine for an aircraft, said jet engine having a front fan and having a longitudinal axis X-X, said air intake being non-rotatably fixed to and monolithically formed with said nacelle and comprising: an upper part, a lower part, an inner lateral part and an outer lateral part, together defining a leading edge between an external wall of the nacelle and an internal wall forming the air supply channel of the jet engine, wherein an outer portion of the leading edge located at the outer latera...