Gas turbine engine combustor with integral fuel conduit(s)

1. An assembly for a gas turbine engine, comprising:

a combustor comprising a combustor wall that forms a peripheral boundary of a combustion chamber within the combustor;

a fuel conduit extending along and formed integral with the combustor wall, the fuel conduit disposed outside of the combustion chamber;

a turbine engine case with a plenum formed by and disposed between the turbine engine case and the combustor wall; and

a fuel manifold extending along and formed integral with the turbine engine case, the fuel manifold fluidly coupled with the fuel conduit.

2. The assembly of claim 1 , further comprising:

a fuel injector arranged with the combustor;

the fuel injector configured to receive fuel from the fuel conduit and inject the fuel into the combustion chamber.

3. The assembly of claim 2 , wherein the fuel injector is formed integral with the combustor and the fuel conduit.

4. The assembly of claim 1 , further comprising:

a second fuel conduit extending along and formed integral with the combustor wall;

the second fuel conduit disposed outside of the combustion chamber; and

the fuel manifold fluidly coupled with the second fuel conduit.

5. The assembly of claim 1 , wherein a segment of the fuel conduit projects out from the combustor, through the plenum, to the turbine engine case.

6. The assembly of claim 1 , wherein

the combustor includes an inner sidewall, an outer sidewall and a bulkhead extending radially between and connected to the inner sidewall and the outer sidewall; and

the bulkhead comprises the combustor wall.

7. The assembly of claim 6 , wherein the fuel conduit further extends along and is formed integral with the outer sidewall.

8. The assembly of claim 1 , further comprising:

a fuel injector arranged with the combustor and fluidly coupled with the fuel conduit; and

a segment of the fuel conduit laterally offset from the fuel injector.

9. The assembly of claim 1 , further comprising:

a fuel injector arranged with the combustor and fluidly coupled with the fuel conduit; and

a segment of the fuel conduit laterally aligned with the fuel injector.

10. The assembly of claim 1 , wherein at least a segment of the fuel conduit follows a straight trajectory as the fuel conduit extends along the combustor wall.

11. The assembly of claim 1 , wherein at least a segment of the fuel conduit follows a non-straight trajectory as the fuel conduit extends along the combustor wall.

12. The assembly of claim 1 , wherein a segment of the fuel conduit extends along and is spaced from the combustor wall.

13. The assembly of claim 1 , further comprising:

a nozzle; and

the combustor meeting the nozzle at a slip joint between the combustor and the nozzle.

14. An assembly for a gas turbine engine, comprising:

a combustor comprising a combustor wall that forms a peripheral boundary of a combustion chamber within the combustor; and

a fuel conduit extending along and formed integral with the combustor wall, the fuel conduit disposed outside of the combustion chamber;

wherein the combustor includes an inner sidewall, an outer sidewall and a bulkhead extending radially between and connected to the inner sidewall and the outer sidewall; and

wherein the outer sidewall comprises the combustor wall.

15. An assembly for a gas turbine engine, comprising:

a combustor comprising a combustor wall that forms a peripheral boundary of a combustion chamber within the combustor;

a fuel conduit extending along and formed integral with the combustor wall, the fuel conduit disposed outside of the combustion chamber; and

a fuel injector arranged with the combustor and fluidly coupled with the fuel conduit;

a segment of the fuel conduit laterally offset from the fuel injector, and the segment of the fuel conduit is circumferentially clocked from the fuel injector about a centerline of the gas turbine engine between five degrees and twenty-five degrees.

16. An assembly for a gas turbine engine, comprising:

a combustor including an outer sidewall, an inner sidewall, a bulkhead and a combustion chamber, the combustion chamber extending radially within the combustor between the outer sidewall and the inner sidewall, and the combustion chamber extending axially within the combustor to the bulkhead; and

a fuel conduit extending along and connected to the bulkhead, at least the fuel conduit and the bulkhead formed together in a monolithic body.

17. The assembly of claim 16 , wherein the fuel conduit also extend along and is connected to the outer sidewall.

18. The assembly of claim 16 , wherein the fuel conduit is disposed outside of the combustor.