Valve for an aircraft

1. A device for connecting an external tank to an aircraft, the aircraft including a seal surface with an opening and a valve with an opening mechanism, the device comprising:

a valve body; and

a seal assembly configured, in use, to resiliently engage the seal surface on the aircraft, the seal assembly including:

a telescopic seal member extending from a proximal end within the valve body to a distal end, the telescopic seal member being constrained within the valve body so as to maintain axial alignment of the telescopic seal member and the valve body; and

a seal carrier provided at the distal end of the telescopic seal member, the seal carrier being pivotable relative to the telescopic seal member for alignment, in use, with the aircraft seal surface;

wherein the seal carrier is generally annular and configured to engage the distal end of the telescopic seal member, and

wherein the seal carrier and telescopic seal member include mutual engagement features configured to retain the seal carrier, the mutual engagement features including a circumferential recess on an inner surface of the seal carrier and an outwardly extending tab on an outer surface of the distal end of the telescopic seal member, and wherein the outwardly extending tab is configured to engage the recess.

2. The device of claim 1 , wherein the distal end of the telescopic seal member includes a generally convex bearing surface, and

wherein the seal carrier includes a complimentary concave bearing surface.

3. The device of claim 1 , further comprising:

a spherical bearing between the seal carrier and the telescopic seal member.

4. The device of claim 1 ,

wherein the valve body further includes an external surface, and

wherein the external surface includes a hole through which the telescopic seal member protrudes,

wherein the hole is dimensioned and sized to closely match the external profile of the telescopic seal member.

5. The device of claim 1 ,

wherein the valve body is a generally cylindrical body, and

wherein the telescopic seal member is a generally cylindrical body having an external diameter which is less that the internal diameter of the valve body, such that the telescopic seal member is configured to be received within the valve body.

6. The device of claim 5 , further comprising:

a seal,

wherein the seal is provided between an internal surface of the valve body and an external surface of the telescopic seal member.

7. The device of claim 1 , further comprising:

a biasing unit,

wherein the biasing unit is disposed between the valve body and the telescopic seal member, and

wherein the biasing unit is configured to bias the telescopic seal member toward an extended position.

8. The device of claim 1 ,

wherein the seal carrier further includes an abutment surface configured to engage, in use, the seal surface on the aircraft, and

wherein the abutment surface includes a seal seat.

9. The device of claim 1 , wherein the mutual engagement features are further configured to provide a stop to limit a range of motion of the seal carrier.

10. The device of claim 1 , further comprising:

a valve engagement member extending through a central bore defined by the valve body and seal assembly,

the valve engagement member being shaped and configured to engage the opening mechanism.

11. The device of claim 1 , wherein the seal carrier is configured to resiliently engage the distal end of the telescopic seal member.