초록 ▼

The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second half-shells (9, 10) rotatably mounted about an axis (A) such that

The invention relates to a jet engine nacelle intended to equip an aircraft, comprising a forward air inlet section, a mid-section intended to surround a fan of the jet engine, and an aft section formed from at least first and second half-shells (9, 10) rotatably mounted about an axis (A) such that they can each be deployed between a working position in which the half-shells (9, 10) are drawn towards one another and a maintenance position in which the half-shells (9, 10) are spaced apart, the mid- and aft sections being connected to one another by a frame (12) which is fixed with respect to the jet engine, the first and second half-shells (9, 10) being equipped with positioning means (13) which in the working position cooperate with complementary positioning means (14) formed on the fixed frame (12). At least the first half-shell (10) is equipped with the locking means (20) which in the maintenance position cooperate with complementary locking means (16, 17) arranged on the fixed frame (12), so as to prevent the first half-shell (10) from moving translationally along its axis (A).

대표청구항 ▼

1. A turbojet nacelle designed to be fitted to an aircraft, the nacelle comprising: a forward air-intake section;a mid-section designed to surround a fan of the turbojet; andan aft section formed from at least a first half-shell and a second half-shell mounted so as to be able to rotate on an axis s

1. A turbojet nacelle designed to be fitted to an aircraft, the nacelle comprising: a forward air-intake section;a mid-section designed to surround a fan of the turbojet; andan aft section formed from at least a first half-shell and a second half-shell mounted so as to be able to rotate on an axis so that each of the half-shells can deploy between a working position in which the half-shells are brought closer to one another and a maintenance position in which the half-shells are separated from one another, the mid-section and aft section being connected to one another by a frame that is fixed relative to the turbojet, the first and second half-shells being fitted with positioning means interacting in the working position with matching positioning means arranged on the fixed frame,wherein the first half-shell at least is fitted with immobilization means interacting, in the maintenance position, with matching immobilization means placed on the fixed frame, in order to prevent the translation of the first half-shell on its axis and in the working position, the immobilization means on the half-shell is completely disengaged from the matching immobilization means on the fixed frame. 2. The nacelle as claimed in claim 1, wherein the immobilization means comprise a finger placed on the first half-shell, the matching immobilization means comprising a groove placed on the fixed frame, or vice versa. 3. The nacelle as claimed in claim 2, wherein, in the working position of the first half-shell, the immobilization finger is retracted from the groove, and in that, in the maintenance position of the first half-shell, the immobilization finger is inserted into the groove. 4. The nacelle as claimed in claim 1, wherein the immobilization finger is disposed adjacent the axis of articulation of the corresponding half-shell. 5. The nacelle as claimed in claim 2, wherein the groove is delimited by a U-shaped section piece fixed to the fixed frame. 6. The nacelle as claimed in claim 2, wherein the groove comprises sidewalls that are inclined relative to one another so as to form a narrowing of the groove in the direction of engagement of the immobilization finger inside the latter when the half-shells are brought closer to one another. 7. The nacelle as claimed in claim 6, wherein the width of the immobilization finger is substantially equal to the width of the groove in its narrowed zone. 8. The nacelle as claimed in claim 6, wherein the immobilization finger and the corresponding groove are arranged so as to allow, when the half-shells are brought closer to one another, the positioning means to come into contact with the matching positioning means only when the finger reaches the narrowed zone of the groove. 9. An aircraft equipped with at least one nacelle as claimed in claim 1.