Integral fluid conduit

Patent metadata

Field	Value
Publication number	US-11262003-B2
Application number	US-201716310838-A
Country	US
Kind code	B2
Filing date	Jun 15, 2017
Priority date	Jun 30, 2016
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

A integrated fluid conduit is provided having two or more internal conduits, the size and shape of the internal conduits is designed to optimize the hydraulic diameter of each conduit based on the needs of the system. The integrated fluid conduit is advantageously manufactured according to additive manufacturing techniques which enable formation of off-center and/or non-concentric internal conduits adapted to specific applications requiring turns such as the fuel delivery system or the hydraulic system of/on a gas turbine engine for an airplane.

First claim

We claim:

1. A fuel delivery manifold system comprising:
an annular fluid conduit having a length defining an opening and at least one bend, the annular fluid conduit comprising:
an outer perimeter that defines a central axis of the annular fluid conduit;
a first circular interior fluid conduit having a center that is offset from the central axis of the annular fluid conduit; and
a second interior fluid conduit separate from the first circular interior fluid conduit, and

an annular array of fuel delivery nozzles interconnected by the annular fluid conduit, each of the fuel delivery nozzles extending from different portions of the annular fluid conduit along the length of the annular fluid conduit, each fuel delivery nozzle of the annular array of fuel delivery nozzles extending radially inwardly toward a center of the opening.

2. The fuel delivery manifold system as claimed in claim 1 , wherein the outer perimeter is circular.

3. The fuel delivery manifold system as claimed in claim 2 , further comprising a third interior fluid conduit.

4. The fuel delivery manifold system as claimed in claim 3 , wherein the second and third interior fluid conduits are non-circular and together with the first circular interior fluid conduit occupy at least 90% of the volume of the annular fluid conduit.

5. The fuel delivery manifold system as claimed in claim 1 , wherein the annular fluid conduit has a non-circular outer perimeter.

6. The fuel delivery manifold system as claimed in claim 1 , wherein the annular fluid conduit is an integrated fuel conduit that delivers fuel to fuel nozzles of a gas turbine engine.

7. The fuel delivery manifold system of claim 5 , wherein the first circular interior fluid conduit is a main fuel line.

8. The fuel delivery manifold system as claimed in claim 5 , wherein the second interior fluid conduit is a pilot secondary fuel line.

9. The fuel delivery manifold system as claimed in claim 1 , wherein the annular fluid conduit is an integrated hydraulic fluid conduit.

10. The fuel delivery manifold system as claimed in claim 1 , wherein the integrated hydraulic fluid conduit is part of a hydraulic system of a gas turbine engine for an airplane.

11. A fuel delivery manifold system comprising:
an annular fluid conduit having a length and at least one bend, the annular fluid conduit comprising:
an outer perimeter that defines a central axis of the annular fluid conduit;
a first interior fluid conduit; and
a second interior fluid conduit separate from the first interior fluid conduit, and

an annular array of fuel delivery nozzles interconnected by the annular fluid conduit, each of the fuel delivery nozzles extending from different portions of the annular fluid conduit along the length of the annular fluid conduit, each fuel delivery nozzle of the annular array of fuel delivery nozzles being equidistantly spaced apart from one another along an entire length of the annular fluid conduit,
wherein the first interior fluid conduit and the second interior fluid conduit are non-concentric.

12. The fuel delivery manifold system as claimed in claim 11 , wherein the outer perimeter is circular.

13. The fuel delivery manifold system as claimed in claim 11 , further comprising a third interior fluid conduit.

14. The fuel delivery manifold system as claimed in claim 13 , wherein the second and third interior fluid conduits are non-circular and together with the first interior fluid conduit occupy at least 90% of the volume of the annular fluid conduit.

15. The fuel delivery manifold system as claimed in claim 11 , wherein the annular fluid conduit has a non-circular outer perimeter.

16. The fuel delivery manifold system as claimed in claim 11 , wherein the annular fluid conduit is an integrated fuel conduit that delivers fuel to fuel nozzles of a gas turbine engine.

17. The fuel delivery manifold system as claimed in claim 15 , wherein the first interior fluid conduit is a main fuel line.

18. The fuel delivery manifold system as claimed in claim 15 , wherein the second interior fluid conduit is a pilot secondary fuel line.

19. The fuel delivery manifold system as claimed in claim 11 , wherein the annular fluid conduit is an integrated hydraulic fluid conduit.

20. The fuel delivery manifold system as claimed in claim 11 , wherein the integrated hydraulic fluid conduit is part of a hydraulic system of a gas turbine engine for an airplane.

Assignees

• Gen Electric

Inventors

• Grover Varun
• Wolfe Jared Matthew

Classifications

• F15B21/00

  Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass · CPC title

• F16L9/19 Primary

  Multi-channel pipes or pipe assemblies · CPC title

• F02C7/222 Primary

  Fuel flow conduits, e.g. manifolds · CPC title

• F05D2230/31

  Layer deposition · CPC title