초록 ▼

A nacelle for a turban engine includes an air intake structure and a central structure. The central structure has a casing intended to surround a fan and an external structure. The air intake structure has at least one internal panel attached to the central structure via the casing and therewith for

A nacelle for a turban engine includes an air intake structure and a central structure. The central structure has a casing intended to surround a fan and an external structure. The air intake structure has at least one internal panel attached to the central structure via the casing and therewith forming a fixed structure and at least one longitudinal external panel attached removably to the fixed structure and incorporating an air intake lip. The external panel is moveable between an operating position and a maintenance position in which the external panel is separated from the external structure of the central section and the air intake lip is separated from the internal panel of the air intake structure.

대표청구항 ▼

1. A nacelle for a turbojet comprising: an air intake structure capable of channeling an air flow toward a fan of the turbofan,a middle structure surrounding said fan and to which the air intake structure is attached so as to provide an aerodynamic continuity, anda rear section aft of the middle str

1. A nacelle for a turbojet comprising: an air intake structure capable of channeling an air flow toward a fan of the turbofan,a middle structure surrounding said fan and to which the air intake structure is attached so as to provide an aerodynamic continuity, anda rear section aft of the middle structure, said rear section housing a thrust reverser system,the middle structure comprising a casing surrounding the fan and an outer structure,wherein the air intake structure comprises at least one inner panel attached to the middle structure by means of the casing and forming with the casing a fixed structure of the nacelle, and, at least one outer longitudinal panel attached in a removable manner to the fixed structure and incorporating an air intake lip,said at least one outer longitudinal panel being movable between an operating position in which the outer panel provides the aerodynamic continuity with the outer structure of the middle structure and the air intake lip provides the aerodynamic continuity with the inner panel of the air intake structure, and a maintenance position in which the outer panel is separated from the outer structure of the middle structure and the air intake lip is separated from the inner panel of the air intake structure, andwherein the middle structure comprises at least one laterally movable fan cover allowing external access to the nacelle. 2. The nacelle as claimed in claim 1, wherein the middle structure has, with the outer panel, an interface situated downstream of the air intake structure. 3. The nacelle as claimed in claim 1, wherein the lip and the outer panel of the air intake structure have an interface at which said lip and outer panel overlap partially when in the closed position. 4. The nacelle as claimed in claim 3, wherein a portion of an inner wall overlapping the lip incorporates means for deicing the bottom zone of said lip. 5. The nacelle as claimed in claim 1, wherein the outer panel of the air intake structure has a front frame capable of being attached to a matching partition of the air intake structure secured to a fixed portion of the nacelle by means of the inner panel. 6. The nacelle as claimed in claim 1, wherein the air intake structure comprises means for centering and positioning the outer panel. 7. The nacelle as claimed in claim 1, wherein the air intake structure comprises guidance means capable of allowing a substantially rectilinear movement of the outer panel toward the upstream of the nacelle so as to be able to open the outer panel. 8. The nacelle as claimed in claim 7, wherein the air intake structure comprises at least one abutment means of the outer panel capable of allowing a partial opening of the outer panel without requiring complete removal. 9. The nacelle as claimed in claim 7, wherein the guidance means comprise at least one rail system. 10. The nacelle as claimed in claim 9, wherein the at least one rail system comprises at least one rail capable of interacting with a corresponding slide or a runner. 11. The nacelle as claimed in claim 9, wherein the at least one rail system comprises at least one system of skids with rollers capable of interacting with a corresponding rail. 12. The nacelle as claimed in claim 11, wherein the rollers are mounted on flexible axles. 13. The nacelle as claimed in claim 11, wherein the rollers are mounted on at least one plate, said plate being attached in a flexible manner, via a swivel-joint connection or a flexible interface. 14. The nacelle as claimed in claim 9, wherein the at least one rail system comprises at least one channel-like rail capable of interacting with a corresponding slide system. 15. The nacelle as claimed in claim 7, wherein the guidance means comprise at least one longitudinal shaft capable of sliding through a corresponding opening. 16. The nacelle as claimed in claim 7, wherein the air intake structure comprises mechanical or manual means for moving the outer panel along the guidance means. 17. The nacelle as claimed in claim 1, wherein the inner panel of the air intake structure comprises an acoustic shroud. 18. The nacelle as claimed in claim 1, wherein the air intake structure comprises equipment for deicing the air intake structure. 19. The nacelle as claimed in claim 1, wherein the inner panel is, at the junction of the air intake lip, extended by a peripheral elastic tongue capable of covering said junction when the outer panel is in the closed position. 20. The nacelle as claimed in claim 1, wherein said at least one outer longitudinal panel is opened only after said laterally movable fan cover fitted to the middle structure is opened.