Liquid fuel cartridge unit for gas turbine combustor and method of assembly

Patent metadata

Field	Value
Publication number	US-2018363907-A1
Application number	US-201715625044-A
Country	US
Kind code	A1
Filing date	Jun 16, 2017
Priority date	Jun 16, 2017
Publication date	Dec 20, 2018
Grant date	—

Abstract

A liquid fuel cartridge unit for a gas turbine combustor includes a cartridge tip having an aft plate and a side wall circumscribing the aft plate. First injection ports are defined through the side wall, and second injection ports are defined through the side wall upstream of the first injection ports, relative to fuel flow through the cartridge tip. Nested conduits extend into the cartridge tip with the concentric conduits defining therebetween respective flow passages. The first injection ports are in fluid communication with a first flow passage, and the second injection ports are in fluid communication with a second flow passage. A method of assembling the liquid fuel cartridge unit is also provided.

First claim

What is claimed is:

1 . A liquid fuel cartridge unit for a gas turbine combustor, the cartridge unit comprising:
a cartridge tip having an aft plate and a side wall circumscribing the aft plate; a first plurality of injection ports defined through the side wall; a second plurality of injection ports defined through the side wall in a different axial plane from the first plurality of injection ports; and a plurality of nested conduits extending into the cartridge tip, the plurality of nested conduits defining therebetween respective flow passages, the first plurality of injection ports in fluid communication with a first flow passage and the second plurality of injection ports in flow communication with a second flow passage.

2 . The cartridge unit of claim 1 , wherein the first plurality of injection ports comprises fewer injection ports than the second plurality of injection ports.

3 . The cartridge unit of claim 1 , wherein each injection port of the first plurality of injection ports has a first size; wherein each injection port of the second plurality of injection ports has a second size; and wherein the first size is different from the second size.

4 . The cartridge unit of claim 1 , wherein the plurality of nested conduits comprises a first conduit defining the first flow passage and a second conduit surrounding the first conduit, the second flow passage being defined between the first conduit and the second conduit.

5 . The cartridge unit of claim 4 , wherein the first conduit and the second conduit are joined, respectively, to a first supply tube and a second supply tube; and wherein the first supply tube and the second supply tube are nested and extend upstream from the cartridge tip.

6 . The cartridge unit of claim 5 , wherein the first flow passage is in flow communication with a source of pilot fuel via the first supply tube, and the second flow passage and is in flow communication with a source of liquid fuel via the second supply tube.

7 . The cartridge unit of claim 1 , wherein the plurality of nested conduits includes a third conduit surrounding the second conduit, such that a third flow passage is defined between the second conduit and the third conduit; and wherein a third plurality of injection ports is defined through the side wall in a different axial plane from the first plurality of injection ports and the second plurality of injection ports, the third plurality of injection ports being in flow communication with the third flow passage.

8 . The cartridge unit of claim 7 , wherein the second plurality of injection ports and the third plurality of injection ports are equal in number.

9 . The cartridge unit of claim 7 , wherein each injection port of the third plurality of injection ports has a third size; and wherein the third size is different from at least one of the first size and the second size.

10 . The cartridge unit of claim 7 , wherein the third conduit is joined to a third supply tube, the third supply tube surrounding the second supply tube and being in flow communication with a liquid fuel supply.

11 . The cartridge unit of claim 1 , wherein the plurality of nested conduits includes an air flow conduit surrounding the second conduit, such that an air flow passage is defined between the second conduit and the air flow conduit; and wherein the air flow conduit is joined to an air flow supply tube in flow communication with a supply of compressed air.

12 . The cartridge unit of claim 11 , wherein the aft plate defines therethrough a plurality of apertures in flow communication with the air flow passage defined by the air flow conduit.

13 . The cartridge unit of claim 11 , wherein at least one injection port of the first plurality of injection ports and the second plurality of injection ports is surrounded by an air vent, the air vent being in flow communication with the air flow passage defined by the air flow conduit.

14 . A method of assembling a liquid fuel cartridge unit for a combustor, the method comprising:
providing a liquid fuel cartridge tip having a plurality of nested conduits extending axially upstream therefrom; joining a downstream end of a first supply tube to a first conduit of the plurality of conduits; joining a downstream end of a second supply tube to a second conduit of the plurality of conduits, such that the second supply tube circumscribes the first supply tube; joining a downstream end of a third supply tube to a third conduit of the plurality of conduits, such that the third supply tube circumscribes the second supply tube and thereby forming a concentric tube assembly; bending the concentric tube assembly around a die at a bend location upstream of the cartridge tip; joining an upstream end of each of the first supply tube, the second supply tube, and the third supply tube to a fluid manifold hub; wherein the first supply tube, the second supply tube, and the third supply tube are supported solely by the cartridge tip and the fluid manifold hub.

15 . The method of claim 14 , wherein the joining of the downstream ends of the supply tubes to respective conduits is accomplished by welding or brazing; and wherein the joining of the upstream ends of the supply tubes to the fluid manifold hub is accomplished by welding or brazing.

16 . The method of claim 14 , wherein the bend location is proximate the upstream ends of the supply tubes.

17 . The method of claim 14 , further comprising filling the first supply tube, the second supply tube, and the third supply tube with a removable material prior to bending the concentric tube assembly.

18 . The method of claim 18 , further comprising removing the removable material after bending the concentric tube assembly.

19 . The method of claim 14 , further comprising providing the fluid manifold hub with a first fluid inlet in flow communication with the first supply tube, a second fluid inlet in flow communication with the second supply tube, and a third fluid inlet in flow communication with the third supply tube; and wherein the first fluid inlet is upstream of the second fluid inlet, and wherein the second fluid inlet is upstream of the third fluid inlet.

20 . The method of claim 14 , further comprising joining a downstream end of a fourth supply tube to a fourth conduit, the fourth supply tube surrounding the third supply tube; and wherein the fourth supply tube is in flow communication with a fourth fluid inlet provided in a mounting flange disposed downstream of the bend location.

Assignees

• Gen Electric

Inventors

• Purcell Timothy James
• Chila Ronald James
• Stoia Lucas John

Classifications

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F23R3/343

  Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion (ignition in gas-turbine plants F02C7/264; pilot flame igniters F23Q9/00) · CPC title

• F23R3/36

  Supply of different fuels · CPC title

• F23D11/38

  Nozzles; Cleaning devices therefor · CPC title

• F02C7/22

  Fuel supply systems · CPC title