Fuel injector device

Patent metadata

Field	Value
Publication number	US-10544940-B2
Application number	US-201615084012-A
Country	US
Kind code	B2
Filing date	Mar 29, 2016
Priority date	Mar 30, 2015
Publication date	Jan 28, 2020
Grant date	Jan 28, 2020

Abstract

A fuel injector device includes a body having a leading edge and a trailing edge and defining a streamwise direction from the leading edge to the trailing edge. The fuel injector device body includes a first surface and a second surface opposite the first surface, each surface extending between and including the leading edge and the trailing edge, and the surfaces conjoining each other at the leading edge and the trailing edge. The trailing edge, when seen in the streamwise direction, undulates along a trailing edge mean line and, along its extent, deviates in opposite directions from the mean line and includes at least one inflection point along its extent.

First claim

The invention claimed is:

1. A fuel injector device comprising:
a body, said body having a leading edge and a trailing edge and defining a streamwise direction from the leading edge to the trailing edge, the fuel injector device body including a first surface and a second surface opposite the first surface, each of said surfaces extending between and including the leading edge and the trailing edge and said surfaces conjoining each other at the leading edge and the trailing edge, wherein the trailing edge, when seen in the streamwise direction, undulates along a trailing edge mean line and, along its extent, deviates in opposite directions from said mean line and includes at least two inflection points and at least one apex along its extent, wherein the at least two inflection points are located on the mean line, and
at least one first internal fuel supply and at least one first fuel discharge duct fluidly connecting the at least one first internal fuel supply with at least one first fuel discharger opening out to an exterior of the injector device, wherein the at least one first fuel discharge duct terminates at the at least one first fuel discharger arranged at the trailing edge,
wherein at least two first fuel dischargers of the at least one first fuel discharger are arranged at the trailing edge, an entirety of each of the at least two first fuel dischargers being arranged between a first inflection point of the at least two inflection points and a first apex of the at least one apex, wherein the first apex is the apex nearest to the first inflection point.

2. The fuel injector device according to claim 1 , wherein the at least two first fuel dischargers are slot-shaped and have a slot longitudinal extent extending along the trailing edge.

3. The fuel injector device according to claim 1 , comprising: at least one second internal fuel supply and at least one second fuel discharge duct fluidly connecting the at least one second internal fuel supply with at least one second fuel discharger provided on the trailing edge and opening out to the exterior of the fuel injector device.

4. The fuel injector device according to claim 3 wherein the number of the at least two first fuel dischargers is larger than the number of the at least one second fuel discharger.

5. The fuel injector device according to claim 3 , wherein the at least one second fuel discharger or a multitude of the at least one second fuel discharger are arranged on the at least two inflection points of the trailing edge.

6. The fuel injector device according to claim 3 , wherein the at least one second fuel discharger is arranged and configured for the discharge of a liquid fuel and are liquid fuel nozzles.

7. The fuel injector device according to claim 1 , wherein the at least two first fuel dischargers are arranged and configured for the discharge of a gaseous fuel.

8. The fuel injector device according to claim 1 , comprising: at least one internal carrier fluid supply and at least one carrier fluid discharge duct fluidly connecting the at least one carrier fluid supply with at least one carrier fluid discharger opening out to the exterior of the injector device, wherein a respective carrier fluid discharger of the at least one carrier fluid discharger is provided adjacent each of the at least two first fuel dischargers and encircling each of the at least two first fuel dischargers.

9. The fuel injector device according to claim 1 , wherein at least two carrier fluid dischargers are arranged adjacent each of the at least two first fuel dischargers and on opposite sides of each of said at least two first fuel dischargers.

10. The fuel discharge means according to claim 1 , further comprising at least one carrier fluid discharger, wherein the at least one carrier fluid discharger is slot-shaped.

11. The fuel injector device according to claim 1 , wherein the fuel injector device is seamless.

12. The fuel injector device according to claim 1 , manufactured by additive manufacturing using a selective laser melting process and/or a selective electron beam melting process.

13. A combustor, comprising:
a fuel injector device according to claim 1 .

14. A gas turbine comprising:
a combustor according to claim 13 , wherein the gas turbine is a sequential combustion gas turbine engine and the combustor is a subsequent combustor arranged to be supplied with partly expanded flue gas from a turbine.

Assignees

• Ansaldo Energia Switzerland AG

Inventors

• Loeffel Kaspar
• Yang Yang
• Eroglu Adnan
• Maurer Michael Thomas
• Biagioli Nico
• Stytsenko Alexey
• Mylnikov Sergey
• Baibuzenko Igor

Classifications

• F23C2900/07001

  Air swirling vanes incorporating fuel injectors · CPC title

• F23R3/14 Primary

  by using swirl vanes · CPC title

• F23R3/20

  incorporating fuel injection means · CPC title

• F23R3/26 Primary

  Controlling the air flow · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title