Bleed valve assembly

1. A gas turbine engine, comprising:

a fan including a plurality of fan blades;

a compressor section;

a combustor section in fluid communication with said compressor section;

a turbine section driving said fan, the combustor in fluid communication with said turbine section;

a tubing system that circulates a fluid between a fuel tank and said combustor section;

a bleed valve assembly mounted to at least one tube portion of said tubing system; and

said bleed valve assembly including a tube boss mounted to said at least one tube portion of said tubing system and a bleed adaptor connected to said tube boss, said tube boss defining a bore and a first passage, said bleed adaptor received in said bore, said first passage interconnecting said at least one tube portion and said bore, said bleed adaptor movable between a first position and a second position relative to said bore of said tube boss to expose a bleed opening of said bleed adaptor to the fluid inside said at least one tube portion, wherein the fluid includes fuel.

2. The gas turbine engine as recited in claim 1 , wherein an inlet portion of said bleed adaptor is received against a seat of said tube boss in said first position and is spaced from said seat in said second position.

3. The gas turbine engine as recited in claim 2 , wherein said bleed adaptor is threadably connected to said tube boss.

4. The gas turbine engine as recited in claim 3 , wherein said bleed opening is disposed on said inlet portion of said bleed adaptor, said bleed opening in communication with a fluid passage extending longitudinally through said bleed adaptor, and said inlet portion slopes inwardly toward an end of said bleed adaptor.

5. The gas turbine engine as recited in claim 1 , wherein said bleed opening is disposed on an inlet portion of said bleed adaptor.

6. The gas turbine engine as recited in claim 1 , comprising a hose connected to said bleed adaptor on an opposite side from said tube boss.

7. A method of bleeding fluid from a tubing system, comprising:

selectively exposing a bleed opening of a bleed adaptor that is connected to a tube portion of the tubing system, said tubing system in communication with a combustor section of a gas turbine engine and with a fuel tank;

communicating fluid from inside of the tube portion into the bleed opening to remove the fluid from the tube portion, wherein the fluid includes fuel; and

communicating the fluid through the bleed adaptor and then through a hose connected to the bleed adaptor.

8. The method as recited in claim 7 , wherein the step of selectively exposing includes:

moving the bleed adaptor from a first position in which the bleed adaptor is received against a seat of a tube boss mounted to the tube portion and a second position in which the bleed adaptor is spaced from the seat.

9. The method as recited in claim 7 , wherein the step of communicating includes:

directing the fluid from the tube portion, through the bleed opening, and into a passage of the bleed adaptor.

10. A fuel bleed system for a gas turbine engine, comprising:

at least one tube portion that circulates fluid between a fuel tank and a combustor section of a gas turbine engine; and

a bleed valve assembly comprising:

a tube boss mounted to said at least one tube portion, said tube boss defining a bore and a first passage that interconnects said at least one tube portion and said bore; and

a bleed adaptor received in said bore, said bleed adaptor movable between a first position and a second position relative to said bore, said first position blocking flow of the fluid from inside said at least one tube portion into a bleed opening of said bleed adaptor, and said second position exposing said bleed opening to the fluid inside said at least one tube portion, wherein the fluid includes fuel.

11. The fuel bleed system as recited in claim 10 , wherein said bleed adaptor includes an inlet portion, a fitting opposite said inlet portion, and an adaptor body that extends between said inlet portion and said fitting, said bleed opening disposed on said adaptor body, and wherein said bleed opening is exposed in said second position such that the fluid is directed from said at least one tube portion, through said first passage, into said bore and then into said bleed adaptor.

12. The bleed valve assembly as recited in claim 11 , wherein said inlet portion of said bleed adaptor is moveable away from a seat of said tube boss to expose said bleed opening.

13. The fuel bleed system as recited in claim 11 , comprising a hose connected to said fitting.

14. The fuel bleed system as recited in claim 11 , comprising a nut and a threaded portion between said inlet portion and said fitting.

15. The fuel bleed system as recited in claim 14 , comprising a seal between said nut and said threaded portion.

16. The fuel bleed system as recited in claim 11 , wherein said inlet portion of said bleed adaptor is received against a seat of said tube boss to prevent said fluid from entering said bleed adaptor.

17. The fuel bleed system as recited in claim 16 , wherein said bleed opening is disposed on said inlet portion.

18. The fuel bleed system as recited in claim 16 , wherein said inlet portion of said bleed adaptor is spaced from said seat when said bleed adaptor is located in said second position such that fluid is directed from said at least one tube portion into said bleed opening, and said seat has a conical shaped geometry.

19. The bleed valve assembly as recited in claim 10 , wherein said bleed adaptor is threadably received by said tube boss.