Fuel tank assembly

• US 7,861,884 B2
• Filed: 10/08/2007
• Issued: 01/04/2011
• Est. Priority Date: 10/08/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Childress, James J., Davis, Warren A. II
• Primary Examiner(s): Grosso; Harry A
• Application Number:
  US11/868,712
• Publication Number:
  US 20090090724A1
• Time in Patent Office: 1,184 Days
• Field of Search: 220/4.14, 220/4.15, 220/88.3, 220/560.01, 220/562, 220/723, 220/900, 244/135.B, 244/135.R
• US Class Current: 220/560.01
• CPC Class Codes: B60K 15/03 Fuel tanks chassis frame comprising fluid storage compartment B62D21/16 ; Details of the fuel feeding system related to the fuel tank F02M37/0076
• 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 37/06 Constructional adaptations thereof
• 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 137/0318 Processes
• CPC Class Codes: Y10T 137/0402 Cleaning, repairing, or assembling

Abstract

A fuel tank assembly are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The fuel tank assembly may include a bladder defined between exterior and interior bladder walls, with the interior bladder wall defining a volume for storing fuel. The exterior bladder wall is at least as or more rigid than the interior bladder wall. The fuel tank assembly can also include connectors between the exterior and interior bladder walls to at least partially limit expansion of the bladder. The fuel tank assembly can also include an inlet opening into the bladder to permit a pressurized gas to be introduced into the bladder. The fuel tank assembly may also include a valve through the interior bladder wall into the volume for storing fuel to permit at least some of the pressurized gas to be introduced therein.

Claims

1. A fuel tank assembly comprising:

a bladder defined between an exterior bladder wall and an interior bladder wall, wherein the interior bladder wall defines a volume for storing fuel, and wherein the exterior bladder wall is comprised of a different material than the interior bladder wall so as to be at least more rigid than the interior bladder wall;

an inlet opening into the bladder defined between the exterior and interior bladder walls in order to permit a pressurized gas to be introduced within the bladder such that the exterior and interior bladder walls are in contact with the pressurized gas; and

a plurality of connectors extending between the exterior and interior bladder walls in order to at least partially limit expansion of the bladder while permitting the pressurized gas to flow past the connectors in order to be housed within the bladder on opposite sides of the connectors.

2. A fuel tank assembly according to claim 1 wherein the interior bladder wall is comprised of an elastomeric or a composite material.

3. A fuel tank assembly according to claim 1 wherein the exterior bladder wall is comprised of a composite or metallic material.

4. A fuel tank assembly according to claim 1 wherein the interior bladder wall is comprised of rubber and the exterior bladder wall is comprised of a composite material configured to generate fuzz if the exterior bladder wall is punctured.

5. A fuel tank assembly according to claim 1 further comprising a valve through the interior bladder wall into the volume for storing fuel to permit at least some pressurized gas to enter the volume.

6. A fuel tank assembly according to claim 1 wherein the bladder extends continuously about a majority of a fuel tank.

7. A fuel tank assembly comprising:

a rigid fuel tank;

an expandable bladder wall disposed within and connected to the fuel tank to thereby define a bladder bounded by the fuel tank and the bladder wall, the bladder wall formed of a different material than the fuel tank and configured to transition from a deflated configuration in which the bladder wall is proximate the fuel tank to an expanded configuration in which the bladder wall is spaced from the fuel tank;

an inlet opening into the bladder in order to permit a pressurized gas to be introduced within the bladder such that the fuel tank and the bladder wall are in contact with the pressurized gas; and

a plurality of connectors extending between the fuel tank and the bladder wall in order to at least partially limit expansion of the bladder wall while permitting the pressurized gas to flow past the connectors in order to be housed within the bladder on opposite sides of the connectors.

8. A fuel tank assembly according to claim 7 wherein the interior bladder wall is comprised of an elastomeric or a composite material.

9. A fuel tank assembly according to claim 8 wherein the interior bladder wall is comprised of rubber and the fuel tank is comprised of a composite material configured to generate fuzz if the fuel tank is punctured.

10. A fuel tank assembly according to claim 7 wherein the fuel tank comprises a portion of an aircraft fuselage.

11. A fuel tank assembly according to claim 7 wherein the fuel tank comprises an upper portion that is separable from other portions of the fuel tank to permit the expandable bladder wall to be inserted into the fuel tank.

12. A fuel tank assembly according to claim 11 wherein the upper portion is comprised of a different material than the other portions of the fuel tank.

13. A fuel tank assembly according to claim 7 further comprising a valve through the bladder wall to permit at least some pressurized gas to enter the fuel.

14. A fuel tank assembly according to claim 7 wherein the bladder extends continuously about a majority of the fuel tank.