Fuel nozzles

Patent metadata

Field	Value
Publication number	US-10385809-B2
Application number	US-201514674709-A
Country	US
Kind code	B2
Filing date	Mar 31, 2015
Priority date	Mar 31, 2015
Publication date	Aug 20, 2019
Grant date	Aug 20, 2019

Abstract

A nozzle includes a nozzle body defining a longitudinal axis. The nozzle body has an air passage, a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, and a cooling circuit. The fuel circuit extends from a fuel circuit inlet to a fuel circuit annular outlet. The fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall. At least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis. A cooling circuit is defined within at least one of the fuel circuit inner wall or the fuel circuit outer wall. The cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet.

First claim

What is claimed is:

1. A nozzle, comprising:
a nozzle body defining a longitudinal axis including:
an air passage;
a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, the fuel circuit extending from a fuel circuit inlet to a fuel circuit annular outlet, wherein the fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall, wherein at least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis;
a cooling circuit defined within at least one of the fuel circuit inner wall and the fuel circuit outer wall, wherein the cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet, wherein the cooling circuit includes a pair of helical threads; and
a stem operatively connected to a fuel manifold of the nozzle body, wherein the stem includes:
a coolant-in channel in fluid communication with a distribution channel of the cooling circuit, wherein the coolant-in channel is configured and adapted to provide coolant to the distribution channel, and
a coolant-out channel in fluid communication with a collection channel of the cooling circuit, wherein the coolant-out channel is configured and adapted to receive coolant from the collection channel, wherein a first one of the helical threads begins at the distribution channel and extends to an axial position proximate the fuel circuit outlet to provide cooling flow to a tip of the nozzle, and wherein a first end of a second one of the helical threads is connected to the first helical thread proximate to the fuel circuit outlet and extends to the collection channel to provide a cooling flow exit to the coolant-out channel.

2. A nozzle as recited in claim 1 , wherein the stem includes a fuel channel in fluid communication with the fuel manifold to provide fuel to the fuel circuit inlet.

3. A nozzle as recited in claim 1 , wherein the distribution channel and the collection channel are at least one of: circumferentially spaced apart from one another, or co-planar.

4. A nozzle as recited in claim 1 , wherein the first end of the second one of the helical threads is connected to the first helical thread through a short circuit segment.

5. A nozzle as recited in claim 1 , wherein the nozzle body includes a pair of tubes defined through the air passage and though the fuel manifold, wherein one of the tubes fluidly connects the distribution channel to the coolant-in channel and the other one of the tubes fluidly connects the collection channel to the coolant-out channel.

6. A nozzle as recited in claim 5 , wherein the air passage includes an annular inlet having radial swirl vanes circumferentially spaced apart from one another, wherein the tubes are defined within the radial swirl vanes.

7. A nozzle as recited in claim 1 , wherein the air passage is defined between a backing plate and the fuel circuit inner wall downstream from the backing plate, wherein at least a portion of the fuel circuit inner wall is a conical shape that converges toward the longitudinal axis in a downstream direction.

8. A nozzle as recited in claim 1 , wherein the air passage includes a radial swirler, a converging conical cross-section, and an annular inlet, wherein the radial swirler includes radial swirl vanes circumferentially spaced apart from one another about the annular inlet to induce swirl into air entering the annular inlet of the air passage.

9. A nozzle as recited in claim 1 , wherein the nozzle body includes an outer air passage defined radially outboard of the fuel circuit with respect to the longitudinal axis.

10. A nozzle as recited in claim 9 , wherein the outer air passage is defined between the fuel circuit outer wall and an outer air passage wall, and wherein the outer air passage is a converging non-swirling outer air passage.

11. A nozzle, comprising:
a nozzle body defining a longitudinal axis including:
an air passage;
a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, the fuel circuit extending from a fuel circuit inlet to a fuel circuit annular outlet, wherein the fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall, wherein at least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis;
a cooling circuit defined within at least one of the fuel circuit inner wall and the fuel circuit outer wall, wherein the cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet;
a stem operatively connected to a fuel manifold of the nozzle body, wherein the stem includes:
a coolant-in channel in fluid communication with a distribution channel of the cooling circuit, wherein the coolant-in channel is configured and adapted to provide coolant to the distribution channel, and
a coolant-out channel in fluid communication with a collection channel of the cooling circuit, wherein the coolant-out channel is configured and adapted to receive coolant from the collection channel; and

a pair of tubes defined through the air passage and though the fuel manifold, wherein one of the tubes fluidly connects the distribution channel to the coolant-in channel and the other one of the tubes fluidly connects the collection channel to the coolant-out channel.

12. A nozzle as recited in claim 11 , wherein the stem includes a fuel channel in fluid communication with the fuel manifold to provide fuel to the fuel circuit inlet.

13. A nozzle as recited in claim 11 , wherein the distribution channel and the collection channel are at least one of: circumferentially spaced apart from one another, or co-planar.

14. A nozzle as recited in claim 11 , wherein the cooling circuit includes a pair of helical threads, wherein a first one of the helical threads begins at the distribution channel and extends to an axial position proximate the fuel circuit outlet to provide cooling flow to a tip of the nozzle, and wherein a first end of a second one of the helical threads is connected to the first helical thread proximate to the fuel circuit outlet and extends to the collection channel to provide a cooling flow exit to the coolant-out channel.

15. A nozzle as recited in claim 14 , wherein the first end of the second one of the helical threads is connected to the first helical thread through a short circuit segment.

16. A nozzle as recited in claim 11 , wherein the air passage includes an annular inlet having radial swirl vanes circumferentially spaced apart from one another, wherein the tubes are defined within the radial swirl vanes.

17. A nozzle as recited in claim 11 , wherein the air passage is defined between a backing plate and the fuel circuit inner wall downstream from the backing plate, wherein at least a portion of the fuel circuit inner wall is a conical shape that converges toward the longitudinal axis in a downstream direction.

18. A nozzle as recited in claim 11 , wherein the air passage includes a radial swirler, a converging conical cross-section, and an annular inlet, wherein the radial swirler includes radial swirl vanes circumferentially spaced apart from one another about the annular inlet to induce swirl into air entering the annular inlet of the air passage.

19. A nozzle as recited in claim 11 , wherein the nozzle body includes an outer air passage defined radially outboard of the fuel c

Assignees

• Delavan Inc

Inventors

• Prociw Lev A

Classifications

• F23R3/283

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

• F23R3/14 Primary

  by using swirl vanes · CPC title

• F23D11/36

  Details · CPC title

• F02M31/20 Primary

  for cooling ({F02M31/005 takes precedence; use of cold F02M17/52;} cooling of charging-air or of scavenging-air F02B29/04) · CPC title

• F02C7/22

  Fuel supply systems · CPC title