Kinetic energy absorption device and aircraft comprising such a device
A device to absorb kinetic energy caused by an exceptional load includes an outer casing configured to maintain integrity after the exceptional load. A core of the device is made of a compactable material at least partially filling the outer casing. The core material is compacted under an exceptional load and absorbs some of the kinetic energy caused by the load. At least one stiffness element is incorporated into the core. A distribution element includes each stiffness element. An aircraft, a vehicle, an item of equipment and an installation includes such a device.
1. A device to absorb kinetic energy due to an exceptional load, comprising:
an outer shell configured to maintain its integrity after the exceptional load;
a core made of compactable material at least partially filling the outer shell, the compactable material constituting the core compacted under the exceptional load and absorbing a part of the kinetic energy due to the exceptional load;
at least one stiffening member integrated in the core; and
a distribution member comprising each stiffening member,
wherein said at least one stiffening member is an assembly of unidirectional fibers,
wherein the unidirectional fibers of said at least one stiffening member are held by a braided shell.
2. The device as claimed in claim 1 , further comprising a diffusion member to diffuse the exceptional load on the core.
3. The device as claimed in claim 2 , wherein the diffusion member comprises one of the following material: a titanium alloy, an aluminum alloy, a PBO (p-phenylene-2,6-benzobisoxazole) composite, a non-woven composite, a polyethylene composite, an aramid composite or a glass composite.
4. The device as claimed in claim 1 , wherein said at least one stiffening member comprises a bonding material to bond the unidirectional fibers.
5. The device as claimed in claim 1 , wherein at least one unidirectional fiber of said at least one stiffening member is made of a cured polymerized material.
6. The device as claimed in claim 1 , wherein at least a portion of said at least one stiffening member is a truncated cylinder.
7. The device as claimed in claim 1 , wherein at least a portion of said at least one stiffening member is a truncated cone.
8. The device as claimed in claim 1 , wherein said at least one stiffening member is integrated in a concave relief comprised in the core.
9. The device as claimed in claim 1 , wherein each stiffening member is distributed equally by the distribution member.
10. The device as claimed in claim 1 , wherein the distribution member comprises one of the following material: a titanium alloy, an aluminum alloy, a PBO (p-phenylene-2,6-benzobisoxazole) composite, a non-woven composite, a polyethylene composite, an aramid composite or a glass composite.
11. An aircraft comprising the device as claimed in claim 1 .
12. A vehicle comprising the device as claimed in claim 1 .
13. An equipment comprising the device as claimed in claim 1 .
14. An installation comprising the device as claimed in claim 1 .