Energy absorption device for aircraft structural element
A device for absorbing kinetic energy for an aircraft structural element undergoing a dynamic impact. The device includes an outer enclosure made from a braided composite material configured to preserve its integrity after an impact, and a foam core contained in the outer enclosure and to at least partially fill the outer enclosure. The foam core configured to at least partially absorb the kinetic energy generated by the impact. Reinforcing elements include at least one dry composite fiber preform integrated into the foam core to dissipate, in combination with the foam core, the kinetic energy generated by the impact. A method for integrating the device for absorbing kinetic energy.
1. A kinetic energy absorption device for a structural element of an aircraft subjected to a dynamic impact, the aircraft comprises a leading edge and a trailing edge, the device comprising:
an outer casing made of a braided composite maintaining an integrity after an impact, said braided composite comprising at least two dry fibers;
a foam core contained inside the outer casing and at least partially filling the outer casing, the foam core configured to at least partially absorb kinetic energy generated by the impact;
reinforcing elements comprising at least one preform made of dry composite fibers, the reinforcing elements in association with the foam core dissipate the kinetic energy generated by the impact, said at least one preform is incorporated into the foam core; and
the kinetic energy absorption device is situated in a region of the leading edge.
2. The kinetic energy absorption device as claimed in claim 1 , wherein the dry composite fibers are made of at least one of the following: carbon, aramid or polyphenylene-2,6-benzoisoxazole.
3. The kinetic energy absorption device as claimed in claim 1 , wherein the outer casing comprises a plurality of plies of impregnated rovings braided with at least two dry fibers.
4. The kinetic energy absorption device as claimed in claim 1 , wherein the kinetic energy generated by the impact is dissipated through rubbing of said at least two dry fibers of the braided composite.
5. The kinetic energy absorption device as claimed in claim 1 , wherein said at least one preform made of dry composite fibers forms a fabric surrounding part of the foam core.
6. The kinetic energy absorption device as claimed in claim 5 , wherein the reinforcing elements comprise a plurality of preforms made of dry composite fibers, each preform forming a fabric surrounding a part of the foam core to partition the foam core.
7. The kinetic energy absorption device as claimed in claim 1 , wherein the reinforcing elements comprise filaments inserted into the foam core by stitching.
8. The kinetic energy absorption device as claimed in claim 7 , wherein the filaments are impregnated with a curable resin.
9. A method of integrating a kinetic energy absorption device for a structural element of an aircraft subjected to a dynamic impact, the aircraft comprises a leading edge and a trailing edge, the method comprising the steps of:
manufacturing a block of foam,
placing a preform made of dry composite fibers around the block of foam;
integrating an additional layer of foam around the block of foam and the preform form a foam core of the kinetic energy absorption device, the foam core is configured to at least partially absorb and dissipate kinetic energy generated by an impact;
installing an outer casing of the kinetic energy absorption device around the foam core, the outer casing made of a braided composite maintaining an integrity after the impact, said braided composite comprising at least two dry fibers;
situating the kinetic energy absorption device in a region of the leading edge; and
wherein the kinetic energy generated by the impact is dissipated through rubbing of said at least two dry fibers of the braided composite.
10. The method of integrating the kinetic energy absorption device as claimed in claim 9 , further comprising the step of repeating the steps of placing and integrating to obtain a second preform made of dry composite fibers around the foam core.
11. The method of integrating the kinetic energy absorption device as claimed in claim 9 , further comprising the step of stitching filaments into the foam core before installing the outer casing.