Panel with impact protection membrane
View Patent ↗An aircraft leading edge panel having an outer aerodynamic surface; and an inner surface carrying the elastomeric impact protection membrane. The membrane comprises a woven or knitted fabric which is impregnated with an elastomeric material. The membrane and the panel may be bonded by an adhesive or co-cured to bond the membrane to the panel. The membrane provides impact protection to the panel by de-bonding from the face of the panel and absorbing at least part of the energy of an object impacting the panel.
1. An aircraft leading edge panel assembly comprising a panel having an outer aerodynamic face and an inner face; and an elastomeric impact protection membrane bonded to the inner face of the panel, wherein the membrane is configured to de-bond from the face of the panel to absorb at least part of the energy of an object impacting the panel.
2. The panel assembly of claim 1 wherein the membrane comprises a woven or knitted fabric which is impregnated with an elastomeric material.
3. The panel assembly of claim 1 wherein the membrane and the panel are co-cured to bond the membrane to the panel.
4. The panel assembly of claim 3 wherein the panel comprises a resin which is co-cured with the membrane.
5. The panel assembly of claim 3 wherein the membrane and the panel are co-cured by heating them together.
6. The panel assembly of claim 1 wherein the membrane comprises an elastomeric material with a molecular weight greater than 5,000.
7. The panel assembly of claim 1 wherein the membrane comprises an elastomeric material with a density lower than 1.6 Mgm −3 .
8. The panel assembly of claim 1 further comprising one or more fasteners which pass through the membrane and the panel.
9. An aircraft comprising a panel assembly according to claim 1 .
10. An aircraft leading edge panel assembly comprising a panel having an outer aerodynamic face and an inner face; and an elastomeric impact protection membrane bonded to the inner face of the panel, wherein the membrane is configured to de-bond from the face of the panel by cohesive failure to absorb at least part of the energy of an object impacting the panel.
11. A method of providing impact protection, the method comprising bonding an elastomeric membrane to a face of a panel; and de-bonding the elastomeric membrane from the face of the panel to absorb at least part of the energy of an object impacting the panel, wherein the panel comprises an aircraft leading edge panel.
12. The method of claim 11 wherein the membrane de-bonds from the face of the panel by cohesive failure.
13. The method of claim 11 wherein the membrane de-bonds from the face of the panel by cohesive adhesive failure.
14. The method of claim 11 wherein the panel comprises an aircraft panel.