COMPOSITE FORWARD PRESSURE BULKHEAD
A forward pressure bulkhead for aircraft includes an energy dissipating material layer, a metallic or nonmetallic inboard skin with a porous filler material positioned within said layers. The energy and load distribution layer redistributes and disperses energy of impacts and penetrations. The porous filler material is a material having ligaments that collapse resulting in a densification of the porous filler material in response to impact loading or a compression force sufficient to cause failure of the combined assembly.
1 . A composite forward pressure bulkhead for an aircraft comprising:
an energy and load distribution layer;
an inboard skin layer; and
a porous filler material positioned between said energy and load distribution layer and said inboard skin layer.
2 . The composite forward pressure bulkhead according to claim 1 wherein said energy and load distribution layer is composed of highly deformable fiber-reinforced composite material that redistributes impact energy without puncture or penetration.
3 . The composite forward pressure bulkhead according to claim 2 wherein said energy and load distribution layer is composed of aromatic polyamide fibers.
4 . The composite forward pressure bulkhead according to claim 1 wherein said porous filler material contains open cells and ligaments.
5 . The composite forward pressure bulkhead according to claim 4 wherein said ligaments collapse in response to a force created by an impact to said energy and load distribution layer or inboard skin layer of said composite forward pressure bulkhead.
6 . The composite forward pressure bulkhead according to claim 4 wherein said ligaments collapse in response when said composite forward pressure bulkhead experiences high compression stresses.
7 . The composite forward pressure bulkhead according to claim 5 wherein said collapse of said ligaments results in a densification of said porous filler material.
8 . The composite forward pressure bulkhead according to claim 6 wherein said collapse of said ligaments results in a densification of said porous filler material.
9 . The composite forward pressure bulkhead according to claim 1 wherein said porous filler material is formed of a metallic material.
10 . The composite forward pressure bulkhead according to claim 9 wherein said metallic material is one of the group consisting of aluminum, steel, nickel, copper, zinc, lead cobalt, cadmium and alloys thereof.
11 . The structural composite element according to claim 1 wherein said inboard skin comprises a metal selected from on of the group of aluminum, steel, nickel, copper, zinc, and alloys thereof.
12 . The structural, energy absorbing composite element according to claim 1 wherein said inboard skin comprises a composite material comprised of the group of carbon/epoxy, thermal set materials, thermoplastic materials and metal matrix composite materials.
13 . A composite forward pressure bulkhead for an aircraft comprising:
an energy and load distribution layer having high tensile strength and high modulus fiber;
an inboard skin layer; and
a porous filler material having open cells and ligaments positioned within said energy absorbing layer and said inboard skin layer, wherein said ligaments collapse in response to a force created by an impact to said energy absorbing layer or inboard skin layer or when said composite forward pressure bulkhead experiences high compression stresses.
14 . The composite forward pressure bulkhead according to claim 13 wherein said energy and load distribution layer absorbs and dissipate energy of a puncture or penetration.
15 . The composite forward pressure bulkhead according to claim 13 wherein said collapse of said ligaments results in a densification of said porous filler material.
16 . The composite forward pressure bulkhead according to claim 13 wherein said porous filler material is formed of a metallic material.
17 . The composite forward pressure bulkhead according to claim 16 wherein said metallic material is one of the group consisting of aluminum, steel, nickel, copper, zinc, lead cobalt, cadmium and alloys thereof.
18 . The forward pressure bulkhead according to claim 13 wherein said inboard skin layer comprises a metal selected from on of the group of aluminum, steel, nickel, copper, zinc, and alloys thereof.
18 . The composite forward pressure bulkhead according to claim 13 wherein said inboard skin layer comprises a composite material comprised of the group of carbon/epoxy, thermal set materials, thermoplastic materials and metal matrix composite materials.
20 . A composite forward pressure bulkhead for an aircraft comprising:
an energy and load distribution layer having high tensile strength and high modulus fiber that absorbs and dissipates energy of a puncture or penetration;
an inboard skin layer; and
a porous filler material insert having open cells and ligaments positioned within said energy absorbing layer and said inboard skin layer, wherein said ligaments collapse resulting in a densification of said porous filler material in response to a force created by an impact to said energy and load distribution layer or said inboard skin or when the composite forward pressure bulkhead experiences high compression stresses.
21 . The composite forward pressure bulkhead according to claim 20 wherein said porous filler material is one of the group consisting of aluminum, steel, nickel, copper, zinc, lead cobalt, cadmium and alloys thereof.
22 . The composite forward pressure bulkhead according to claim 20 wherein said energy and load distribution layer is composed of aromatic polyamide fibers.
23 . The composite forward pressure bulkhead according to claim 20 wherein said inboard skin layer comprises a metal selected from on of the group of aluminum, steel, nickel, copper, zinc, and alloys thereof.
24 . The composite forward pressure bulkhead according to claim 20 wherein said inboard skin layer comprises a composite material comprised of the group of carbon/epoxy, thermal set materials, thermoplastic materials and metal matrix composite materials.