Combustor apparatus in a gas turbine engine
View Patent ↗A combustor apparatus defines a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus includes an outer wall, coupling structure on the outer wall adjacent to a fuel inlet opening thereof, a fuel injection system, a fuel feed assembly, and a fitting member. The fuel injection system provides fuel to be burned in the combustion zone. The fuel supply structure includes a threaded inner surface formed from a first material. The fuel feed assembly includes a fuel feed pipe that extends through the fuel inlet opening in the outer wall and has an outlet portion formed from the first material and that is threadedly engaged with the fuel supply structure, and an inlet portion affixed to the outlet portion and formed from a second material. The fitting member secures the fuel feed assembly relative to the outer wall.
1. A combustor apparatus in a gas turbine engine, the combustor apparatus defining a combustion zone where air and fuel are burned to create high temperature combustion products, the combustor apparatus comprising:
an outer wall defining an interior volume and comprising a fuel inlet opening;
coupling structure on the outer wall adjacent to the fuel inlet opening, the coupling structure comprising a threaded inner coupling portion;
a fuel injection system at least partially located in the interior volume of the outer wall and comprising fuel supply structure for providing fuel to at least one fuel injector that delivers fuel to be burned in the combustion zone, the fuel supply structure including a threaded inner surface formed from a first material having a first hardness and a first coefficient of thermal expansion;
a fuel feed assembly for delivering fuel to the fuel injection system, the fuel feed assembly including a fuel feed pipe that extends through the fuel inlet opening in the outer wall and comprises:
an outlet portion formed from the first material and including a threaded outer surface that is threadedly engaged with the threaded inner surface of the fuel supply structure to create a first sealed coupling with the fuel supply structure; and
an inlet portion affixed to the outlet portion and formed from a second material having a second hardness softer than the first hardness and a second coefficient of thermal expansion; and
a fitting member disposed about and engaged with the inlet portion of the fuel feed pipe and comprising a threaded outer coupling portion, the threaded outer coupling portion being threadedly engaged with the inner coupling portion of the coupling structure to:
create a second sealed coupling with the coupling structure; and
secure the fuel feed assembly relative to the outer wall.
2. The combustor apparatus of claim 1 , wherein the coupling structure comprises a coupling member that is affixed to the outer wall adjacent to the fuel inlet opening.
3. The combustor apparatus of claim 2 , wherein the fitting member creates a compression fitting with the coupling member to clamp the fuel feed pipe in place at a clamping location, wherein a third sealed coupling is formed between the fitting member and the inlet portion of the fuel feed pipe at the clamping location.
4. The combustor apparatus of claim 3 , wherein the fitting member is formed from the second material.
5. The combustor apparatus of claim 3 , wherein the fitting member structurally deforms the inlet portion of the fuel feed pipe at the clamping location.
6. The combustor apparatus of claim 1 , wherein the inlet portion of the fuel feed pipe is welded to the outlet portion thereof at a weld joint.
7. The combustor apparatus of claim 6 , wherein the weld joint is located inside the fuel inlet opening in the outer wall.
8. The combustor apparatus of claim 1 , wherein the first material comprises a metal alloy including at least 45% nickel by mass.
9. The combustor apparatus of claim 8 , wherein the second material comprises stainless steel.
10. The combustor apparatus of claim 1 , wherein the fuel supply system delivers fuel upstream from a main burn zone in the combustion zone.
11. The combustor apparatus of claim 1 , wherein the outlet portion of fuel feed pipe is connected to the fuel supply structure inside of the interior volume of the outer wall.
12. The combustor apparatus of claim 1 , wherein the interior volume of the outer wall defines a passageway for air on its way to the combustion zone.
13. A combustor apparatus in a gas turbine engine, the combustor apparatus defining a combustion zone where air and fuel are burned to create high temperature combustion products, the combustor apparatus comprising:
an outer wall defining an interior volume and comprising a fuel inlet opening;
a coupling member affixed to the outer wall adjacent to the fuel inlet opening, the coupling member comprising a threaded inner coupling portion;
a fuel injection system at least partially located in the interior volume of the outer wall and comprising fuel supply structure for providing fuel to at least one fuel injector that delivers fuel to be burned upstream from a main burn zone in the combustion zone, the fuel supply structure including a threaded inner surface formed from a first material having a first hardness and a first coefficient of thermal expansion;
a fuel feed assembly for delivering fuel to the fuel injection system, the fuel feed assembly including a fuel feed pipe that extends through the fuel inlet opening in the outer wall and comprises:
an outlet portion formed from the first material and being threadedly engaged with the threaded inner surface of the fuel supply structure inside of the interior volume of the outer wall to create a first sealed coupling with the fuel supply structure; and
an inlet portion affixed to the outlet portion and formed from a second material having a second hardness softer than the first hardness; and
a fitting member disposed about and engaged with the inlet portion of the fuel feed pipe and comprising a threaded outer coupling portion, the threaded outer coupling portion being threadedly engaged with the inner coupling portion of the coupling member to secure the fuel feed assembly relative to the outer wall, wherein the fitting member creates a compression fitting with the coupling member to clamp the fuel feed pipe in place at a clamping location.
14. The combustor apparatus of claim 13 , wherein the fitting member is formed from the second material.
15. The combustor apparatus of claim 13 , wherein, due to the compression fitting with the coupling member, the fitting member structurally deforms the inlet portion of the fuel feed pipe at the clamping location.
16. The combustor apparatus of claim 14 , wherein a second sealed coupling is formed between the fitting member the coupling member and a third sealed coupling is formed between the fitting member and the inlet portion of the fuel feed pipe at the clamping location.
17. The combustor apparatus of claim 13 , wherein the inlet portion of the fuel feed pipe is welded to the outlet portion thereof at a weld joint that is located inside the fuel inlet opening in the outer wall.
18. The combustor apparatus of claim 13 , wherein the first material comprises a metal alloy including at least 45% nickel by mass.
19. The combustor apparatus of claim 18 , wherein the second material comprises stainless steel.
20. The combustor apparatus of claim 13 , wherein the interior volume of the outer wall defines a passageway for air on its way to the combustion zone.