Pressure tolerant fuel tank panels

• US 5,674,586 A
• Filed: 06/07/1995
• Issued: 10/07/1997
• Est. Priority Date: 01/21/1993
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Kay, Bruce Fredric, Dobyns, Alan Lee, Barr, Bruce Henry, Terceno, Joaquin, Furnes, Kenneth Morgan, Fabian, Edward Joseph, Toni, Darryl Mark
• Primary Examiner(s): Epstein, Henry F.
• Application Number:
  US08/499,642
• Time in Patent Office: 853 Days
• Field of Search: 428/116, 428/118, 428/36.3, 428/408
• US Class Current: 428/116
• CPC Class Codes: B32B 1/00 Layered products having a non-planar shape
• CPC Class Codes: B32B 2262/0261 Polyamide fibres
• CPC Class Codes: B32B 2262/101 Glass fibres
• CPC Class Codes: B32B 2262/106 Carbon fibres, e.g. graphite fibres
• CPC Class Codes: B32B 2605/18 Aircraft blades, propellers B32B2603/00
• CPC Class Codes: B32B 27/08 of synthetic resin
• CPC Class Codes: B32B 5/14 characterised by a layer differing constitutionally or physically in different parts, e.g. denser near its faces
• CPC Class Codes: B32B 5/24 one layer being a fibrous or filamentary layer
• CPC Class Codes: B60K 15/03177 made of non-metallic material, e.g. plastics, or of a combination of non-metallic and metallic material B60K15/03006 takes precedence
• CPC Class Codes: B60K 2015/03046 made from more than one layer
• CPC Class Codes: B60K 2015/03407 to protect tanks against projectiles
• CPC Class Codes: B64D 2037/325 Fuel tanks with provisions for reduction hydraulic ram shocks due to projectile impacts
• CPC Class Codes: B64D 37/32 Safety measures not otherwise provided for, e.g. preventing explosive conditions extinguishing or preventing fires in aircraft A62C
• CPC Class Codes: Y10T 428/1369 Fiber or fibers wound around each other or into a self-sustaining shape [e.g., yarn, braid, fibers shaped around a core, etc.]
• CPC Class Codes: Y10T 428/24149 Honeycomb-like
• CPC Class Codes: Y10T 428/30 Self-sustaining carbon mass or layer with impregnant or other layer

Abstract

A pressure tolerant composite panel has an inner fiber reinforced layer, an outer fiber reinforced layer and an core disposed therebetween. In one embodiment of the invention, the inner layer has weakening structures incorporated at the peripheral edges thereof, and has an outer layer of a different and lower modulus of elasticity than the inner layer to provide some degree of elongation. When high internal forces are encountered, the weakening structures allow the inner layer to separate, with the outer layers stretching to absorb the forces without failure. Optionally, strengthening straps are position about the panel such that it is compartmentalized into discrete sections to contain damage in localized areas. In an alternative embodiment of the invention, the inner core is produced of a crushable material which has a yield strength sufficient to provide structural support under normal operating conditions. When a high pressure is encountered which exceeds the yield limit, the core is crushed to prevent force transmission to the outer layer. Such a composite panel assures survivability of the panel when subject to impact damage.

Claims

1. A fuel tank having containment walls for containing a fuel, at least one containment wall comprising:

a pressure tolerant composite panel having an inner fiber reinforced layer, an outer fiber reinforced layer, and a strengthening honeycomb core disposed therebetween produced of a material which is crushable in response to high pressure to prevent a stress buildup, and thereby limit impact damage, in the outer layer of the composite panel, and, a plurality of spaced and crossed strapping means disposed over the outer layer for compartmentalizing the outer layer into discrete sections.

2. The fuel tank of claim 1 wherein the strapping means are composed of one or more plies of a glass fiber or polyaramid fiber reinforced epoxy.

3. The fuel tank of claim 1 wherein the honeycomb core is an aluminum honeycomb core.

4. The fuel tank of claim 3 wherein the honeycomb core has a weight of at least about 4.5 lbs. per cubic foot.

5. The fuel tank of claim 3 wherein the honeycomb core has a weight of from about 4.5 to 8 lbs. per cubic foot.

6. The fuel tank of claim 1 wherein the inner layer is composed of one or more plies of a graphite fiber reinforce epoxy material.

7. The fuel tank of claim 1 wherein the outer layer is composed of one or more plies of a graphite fiber reinforced epoxy material.

8. The fuel tank of claim 1 further comprising means for partially releasing the inner fiber layer at the periphery thereof, said means being weakening structures disposed along the edges of the panel.

9. The fuel tank of claim 1 wherein the plurality of strapping means are disposed over the outer layer surface in a crossing pattern.

10. A fuel tank having containment walls for containing a fuel, at least one containment wall comprising:

a pressure tolerant composite panel having a fiber reinforced inner layer, a fiber reinforced outer layer, and a strengthening honeycomb core disposed therebetween, the inner layer having means for partially releasing the inner layer at the periphery thereof to absorb forces, the outer layer having a lower modulus of elasticity than the inner layer, such that the outer layer flexes in a membrane like manner to absorb forces, and, a plurality of strapping means disposed over the outer layer in a crossing pattern which compartmentalizes the outer layer into discrete sections.

11. The fuel tank of claim 10 wherein the inner layer is composed of one or more plies of a fiber reinforced material of relatively high modulus.

12. The fuel tank of claim 10 wherein the inner layer is composed of one or more plies of a graphite fiber reinforced epoxy material.

13. The fuel tank of claim 10 wherein the outer layer is composed of one or more plies of a glass fiber or polyaramid fiber reinforced epoxy material.

14. The fuel tank of claim 10 wherein the means for partially releasing the inner fiber layer at the periphery thereof comprise weakening structures disposed along the edges of the panel.

15. The fuel tank of claim 10 wherein the strapping means are composed of a high elongation material.

16. The fuel tank of claim 10 wherein the strapping means are composed of a glass fiber or polyaramid fiber reinforced epoxy.

17. The fuel tank of claim 10 wherein the composite panel further comprises an insulating facing layer located between the core and the inner and outer layers.