Connection apparatus for improving the crashworthiness of aircraft fluid systems
A fluid connection system for fluidly connecting a pair of fluid reservoirs, such as fuel cells, includes a bellowed portion surrounding a connection portion through which fluid can flow between the two reservoirs. The bellowed portion allows for relative movement between the two reservoirs without breaking the fluid-tight connection between the two reservoirs. Also, a guard member surrounds at least some of the outer periphery of the bellowed portion. The guard member serves as a shield around the fluid-tight connection and bellowed portion, and thereby helps prevent damage to the fluid-tight connection in the event of a crash or hard landing.
1. A fluid connection system comprising:
a first bladder configured to store a fluid, the first bladder comprising a tubular bellowed portion comprising an outer pleat, an inner pleat, and an intermediate portion that forms a portion of each of the outer pleat and the inner pleat, wherein the outer pleat comprises a crest portion disposed at least partially outside the first bladder and wherein the inner pleat comprises a root portion disposed at least partially within the first bladder;
a fitting connected to the inner pleat of the first bladder, the fitting and being connected so as to provide a fluid-tight path through which the fluid can travel to and from the first bladder; and
a guard member extending about an outer periphery of at least a portion of each of the outer pleat, the intermediate portion, and the inner pleat.
2. The system of claim 1 , wherein the guard member extends about the crest portion of the bellowed portion of the first bladder.
3. The system of claim 1 , further comprising a second bladder, wherein the fitting is connected to the second bladder, and wherein the fluid-tight path is between the first and second bladders.
4. The system of claim 3 , wherein the bellowed portion is configured to allow movement of the first and second bladders relative to each other while maintaining the fluid-tight path between the connection portion and the fitting.
5. The system of claim 3 , wherein the guard member includes a portion thereof that extends between the first and second bladders.
6. The system of claim 1 , wherein the guard member is attached to a bulkhead.
7. The system of claim 1 , wherein the guard member is attached to the first bladder.
8. A fluid connection system for fluidly connecting a first fuel cell on a first side of a bulkhead to a second fuel cell on a second side of the bulkhead, the system comprising:
a tubular bellowed portion of a first fuel bladder, the first fuel bladder being configured for retaining fuel within the first fuel cell, the bellowed portion comprising an outer pleat, an inner pleat, and an intermediate portion that forms a portion of each of the outer pleat and the inner pleat, wherein the outer pleat comprises a crest portion disposed at least partially outside the first fuel cell and wherein the inner pleat comprises a root portion disposed at least partially inside the first fuel cell;
a fitting attached between the inner pleat and a second bladder, the second bladder being configured for retaining fuel within the second fuel cell,
wherein the fitting provides a fluid path between the first and second bladders; and
a guard member extending about an outer periphery of at least a portion of each of the outer pleat, the intermediate portion, and the inner pleat.
9. The system of claim 8 , wherein the guard member extends about the crest portion of the bellowed portion of the first bladder.
10. The system of claim 8 , wherein the guard member is attached to the bulkhead.
11. The system of claim 8 , wherein the guard member is attached to the first bladder.
12. An aircraft comprising:
an airframe having a bulkhead;
first and second fuel cells on opposite sides of the bulkhead,
wherein the first fuel cell includes a tubular bellowed portion thereof, the bellowed portion of the fuel cell comprising an outer pleat, an inner pleat, and an intermediate portion that forms a portion of each of the outer pleat and the inner pleat, wherein the outer pleat comprises a crest portion disposed at least partially outside the first fuel cell and wherein the inner pleat comprises a root portion disposed at least partially within the first fuel cell;
a fitting connected between the second fuel cell and the inner pleat of the first fuel cell for providing a fluid connection the first and second fuel cells; and
a guard member extending about an outer periphery of at least a portion of each of the outer pleat, the intermediate portion, and the inner pleat.
13. The aircraft of claim 12 , wherein the guard member extends about the crest portion of the bellowed portion of the first bladder.
14. The aircraft of claim 12 , wherein the guard member is attached to the bulkhead.
15. The aircraft of claim 12 , wherein the guard member is attached to a first bladder, the first bladder being configured for retaining fuel within the first fuel cell.
16. The aircraft of claim 12 , wherein the guard member includes a portion thereof that extends between the first and second fuel cells.