Aerodynamic fastening of turbomachine fuel injectors

Patent metadata

Field	Value
Publication number	US-10641493-B2
Application number	US-201715626783-A
Country	US
Kind code	B2
Filing date	Jun 19, 2017
Priority date	Jun 19, 2017
Publication date	May 5, 2020
Grant date	May 5, 2020

Abstract

A premixing fuel nozzle assembly for a turbomachine is disclosed as having at least one fuel injector with an outer jacket having a first end and a second end and a threaded surface disposed therebetween. The first end has a cylindrical sealing surface and the second end has at least one wrenching pocket. An annular hub is disclosed as having an aperture with a first end and a second end and a threaded surface disposed therebetween, wherein the aperture is configured to at least partially house the fuel injector therein and the annular hub further has a conical seat about the first end. The fuel injector cylindrical sealing surface swages inward to form a hermetic seal when contacting the annular hub conical seat as the fuel injector is threaded into the aperture.

First claim

What is claimed is:

1. A premixing fuel nozzle assembly for a turbomachine, comprising:
an inner hub comprising an aperture, the aperture extending from a first end to a second end, the aperture comprising an internal threaded surface disposed between the first end and the second end and a conical seat defined at the first end;
an outer shroud surrounding the inner hub;
a premixing chamber defined between the inner hub and the outer shroud, the premixing chamber in communication with a flow of compressed air via an air inlet of the premixing fuel nozzle assembly and in communication with a flow of gaseous fuel via a fuel injection port, whereby the flow of compressed air and the flow of gaseous fuel mix in the premixing chamber to form a premixed flow downstream of the fuel injection port;
a liquid fuel injector comprising an outer jacket, the outer jacket comprising a first end and a second end with an external threaded surface disposed therebetween, the first end of the outer jacket comprising a cylindrical sealing surface, the second end of the outer jacket comprising a seating surface and a downstream face of the liquid fuel injector, the downstream face of the liquid fuel injector in contact with the premixed flow, and a wrenching pocket extending from the downstream face of the liquid fuel injector, wherein the wrenching pocket is in fluid communication with the premixing chamber and in contact with the premixed flow;
wherein the second end of the aperture comprises a seating surface positioned radially outward of the external threaded surface, the seating surface of the aperture configured to mate with the seating surface of the liquid fuel injector as the liquid fuel injector is threaded into the aperture; and
wherein the cylindrical sealing surface of the liquid fuel injector is swaged inward to form a hermetic seal with the conical seat of the inner hub.

2. The fuel nozzle assembly of claim 1 , wherein the wrenching pocket comprises a recessed cylindrical bore, a recessed oval bore, a recessed square bore, or combinations thereof.

3. The fuel nozzle assembly of claim 1 , wherein the liquid fuel injector comprises an atomizing liquid fuel injector, a plain jet liquid fuel injector, a simple orifice liquid fuel injector, or combinations thereof.

4. The fuel nozzle assembly of claim 1 , wherein the aperture is in communication with a liquid fuel passage.

5. The fuel nozzle assembly of claim 4 , wherein the liquid fuel passage comprises a fuel plenum therein.

6. The fuel nozzle assembly of claim 5 , wherein a thermal break is disposed between the liquid fuel passage and the liquid fuel injector.

7. The fuel nozzle assembly of claim 1 , wherein the outer jacket comprises:
an internal passageway between the first end and the second end thereof; and
an orifice disposed about the second end thereof, wherein the orifice is narrower than the internal passageway.

8. The fuel nozzle assembly of claim 7 , further comprising a swirler disposed within the internal passageway.

9. A turbomachine, comprising:
a compressor;
a combustor in communication with the compressor, the combustor comprising a premixing fuel nozzle assembly, the premixing fuel nozzle assembly comprising:
an inner hub comprising an aperture, the aperture extending from a first end to a second end, the aperture comprising an internal threaded surface disposed between the first end and the second end and a conical seat defined at the first end;
an outer shroud surrounding the inner hub;
a premixing chamber defined between the inner hub and the outer shroud, the premixing chamber in communication with a flow of compressed air via an air inlet of the premixing fuel nozzle assembly and in communication with a flow of gaseous fuel via a fuel injection port, whereby the flow of compressed air and the flow of gaseous fuel mix in the premixing chamber to form a premixed flow downstream of the fuel injection port;
a liquid fuel injector comprising an outer jacket, the outer jacket comprising a first end and a second end with an external threaded surface disposed therebetween, the first end of the outer jacket comprising a cylindrical sealing surface, the second end of the outer jacket comprising a seating surface and a downstream face of the liquid fuel injector, the downstream face of the liquid fuel injector in contact with the premixed flow, and a wrenching pocket extending from the downstream face of the liquid fuel injector, wherein the wrenching pocket is in fluid communication with the premixing chamber and in contact with the premixed flow;
wherein the second end of the aperture comprises a seating surface positioned radially outward of the external threaded surface, the seating surface of the aperture configured to mate with the seating surface of the liquid fuel injector as the liquid fuel injector is threaded into the aperture; and
wherein the cylindrical sealing surface of the liquid fuel injector is swaged inward to form a hermetic seal with the conical seat of the inner hub.

10. The turbomachine of claim 9 , wherein the wrenching pocket comprises a recessed cylindrical bore, a recessed oval bore, a recessed square bore, or combinations thereof.

11. The turbomachine of claim 9 , wherein the liquid fuel injector comprises an atomizing liquid fuel injector, a plain jet liquid fuel injector, a simple orifice liquid fuel injector, or combinations thereof.

12. The turbomachine of claim 9 , wherein the aperture is in communication with a liquid fuel passage.

13. The turbomachine of claim 12 , wherein the liquid fuel passage comprises a fuel plenum therein.

14. The turbomachine of claim 13 , wherein a thermal break is disposed between the liquid fuel passage and the liquid fuel injector.

15. The turbomachine of claim 9 , wherein the outer jacket comprises:
an internal passageway between the first end and the second end thereof; and
an orifice disposed about the second end thereof, wherein the orifice is narrower than the internal passageway.

16. The turbomachine of claim 15 , further comprising a swirler disposed within the internal passageway.

Assignees

• Gen Electric

Inventors

• Johnson Thomas Edward
• Graham Kaitlin Marie
• Myers Geoffrey David

Classifications

• F23R3/286 Primary

  having fuel-air premixing devices (F23R3/30 takes precedence) · CPC title

• F23R2900/00012

  Details of sealing devices · CPC title

• F23R3/36

  Supply of different fuels · CPC title

• F23R3/38 Primary

  comprising rotary fuel injection means · CPC title

• F23R3/283

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