Device for attaching an air inlet onto a fan casing of an aircraft turbojet nacelle
A device for fastening a downstream end of an air inlet on a fan casing of an aircraft turbojet engine nacelle is provided. The device includes an acoustic shroud, a first flange coupled to the fan casing, a second L-shaped flange having a base coupled to the acoustic shroud, and a collar linked to the first flange. The acoustic shroud extends from an upstream segment to a downstream segment which defines an inner skin and an outer skin that encloses an acoustic panel. The collar further includes a protrusion that extends from the outer skin to the downstream segment.
1. A device for fastening a downstream end of an air inlet on a fan casing of an aircraft turbojet engine nacelle wherein the downstream end comprises an acoustic shroud having an annular shape, the acoustic shroud extending axially from an upstream point to a downstream point along a longitudinal axis and delimited radially by an inner skin and an outer skin enclosing an acoustic panel, the device comprising:
a first flange coupled to the fan casing;
a second L-shaped flange having a base coupled to the acoustic shroud and a collar linked to the first flange; and
a protrusion, wherein the protrusion extends longitudinally from an upstream segment to a downstream segment, wherein the upstream segment is fixed to the acoustic shroud and the downstream segment delimits a radial space with the acoustic shroud, and
wherein the protrusion is adapted to be fastened on the base of the second L-shaped flange by fastening means.
2. The device according to claim 1 , wherein the protrusion is in a shape of an annular ring.
3. The device according to claim 1 , wherein the acoustic panel of the acoustic shroud extends continuously from the upstream segment to the downstream segment of the protrusion.
4. The device according to claim 1 , wherein the second L-shaped flange comprises a metallic material.
5. The device according to claim 1 , wherein the second L-shaped flange includes a plurality of independent portions arranged annularly along the longitudinal axis of the acoustic shroud.
6. The device according to claim 1 , wherein the protrusion comprises a composite material.
7. The device according to claim 1 , wherein the protrusion comprises a wave shape that draws an alternation of hollows and bumps distributed about the longitudinal axis of the acoustic shroud, said bumps each forming a radial overthickness designed to promote fastening of the second L-shaped flange on the protrusion.
8. The device according to claim 1 , wherein the acoustic panel extends longitudinally downstream beyond the plane of the second L-shaped flange.
9. The device according to claim 1 , wherein the device further comprises a corner disposed radially between the outer skin and the downstream segment of the protrusion.
10. The device according to claim 1 , wherein the fastening means includes a plurality of metal links configured to connect the downstream segment of the protrusion to the base of the second L-shaped flange.
11. The device according to claim 1 , wherein the protrusion is integral with the outer skin of the acoustic shroud.