Multiple segment ceramic fuel nozzle tip

• US 20060249061A1
• Filed: 05/03/2005
• Published: 11/09/2006
• Est. Priority Date: 05/03/2005
• Status: Active Grant

• Current Assignee: General Electric Technology GmbH (GE Aerospace)
• Original Assignee: Alstom Technology Ltd. (Alstom SA)
• Inventors: Nowak, Ronald H., Mann, Jeffrey S.
• Granted Patent: US 7,216,594 B2
• Time in Patent Office: Days
• US Class Current: 110/260
• CPC Class Codes: F23D 1/00 Burners for combustion of pulverulent fuel disposition of burners F23C
• CPC Class Codes: F23D 2201/101 tiltable
• CPC Class Codes: F23D 2211/00 Thermal dilatation prevention or compensation
• CPC Class Codes: F23D 2212/105 Particles

Abstract

A solid fuel nozzle tip (201) having at least first (205) and second (207) ceramic shells is provided by the present invention. An inlet end of the first ceramic shell (205) is interconnected to a pulverized solid fuel nozzle (34), and an outlet end (301) of the first ceramic shell (205) is interconnected to an inlet end (305) of the second ceramic shell (207).

Claims

1. A solid fuel nozzle tip, comprising:

a first ceramic shell having an inlet end adapted to interconnect to a solid fuel nozzle and receive a flow of solid fuel from the interconnected solid fuel nozzle, an outlet end distanced from the inlet end, and a chamber having a peripheral wall defining a first passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the first ceramic shell; and

a second ceramic shell having an inlet end adapted to interconnect to the outlet end of the first ceramic shell and receive the flow of solid fuel from the interconnected outlet end of the first ceramic shell, an outlet end distanced from the inlet end of the second ceramic shell and a chamber having a peripheral wall defining a second passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the second ceramic shell.

2. The solid fuel nozzle tip of claim 1, wherein the outlet end of the first ceramic shell and the inlet end of the second ceramic shell are adapted to be interconnected by a dovetail joint formed by the peripheral walls of the chambers of the first and the second ceramic shells.

3. The solid fuel nozzle tip of claim 2, wherein the dovetail joint restrains movement of the first and second ceramic shell with respect to the first ceramic shell in a first direction, the outlet end of the first ceramic shell is defined by an end surface and the inlet end of the second ceramic shell is defined by an end surface, and further comprising:

a first hole extending from the end surface of the outlet end of the first ceramic shell into the peripheral wall of the chamber of the first ceramic shell; and

a second hole extending from the end surface of the inlet end of the second ceramic shell into the peripheral wall of the chamber of the second ceramic shell;

wherein the outlet end of the first ceramic shell and the inlet end of the second ceramic shell are adapted to be interconnected such that the first and the second holes align;

wherein the first and the second holes are adapted for insertion of a connector to restrain movement of the first and second ceramic shell with respect to the first ceramic shell in a second direction substantially perpendicular to the first direction.

4. The solid fuel nozzle tip of claim 1, wherein the ceramic of the first ceramic shell and the second ceramic shell is one of the group of ceramics including silicon nitride, siliconized silicon carbide having a silicon content of between about thirty percent (30%) to sixty percent (60%) by weight, mullite bonded silicon carbide alumina composite, reaction-bonded silicon carbide, and alumina zirconia composites.

5. The solid fuel nozzle tip of claim 1, further comprising:

a third ceramic shell having an inlet end adapted to interconnect to the outlet end of the second ceramic shell and receive the flow of solid fuel from the interconnected outlet end of the second ceramic shell, an outlet end distanced from the inlet end of the third ceramic shell, and a chamber having a peripheral wall defining a third passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the third ceramic shell.

6. The solid fuel nozzle tip of claim 5, further comprising:

at least one splitter plate adapted for insertion into the second and third passageways and attachment to the peripheral walls of the chambers of the second and the third ceramic shells.

7. The solid fuel nozzle tip of claim 6, wherein each of the at least one splitter plates is ceramic.

8. The solid fuel nozzle tip of claim 6, wherein:

the outlet end of the second ceramic shell and the inlet end of the third ceramic shell are adapted to be interconnected by a dovetail joint that is formed by the peripheral walls of the chambers of the second and the third ceramic shells and that restrains movement of the third ceramic shell with respect to the second ceramic shell in a first direction; and

the at least one splitter plate restrains movement of the third ceramic shell with respect to the second ceramic shell in a second direction substantially perpendicular to the first direction.

17. The solid fuel nozzle tip of claim 1, wherein the first ceramic shell is a first unitary ceramic shell, and the second ceramic shell is a second unitary ceramic shell.

9. A solid fuel nozzle tip for use in cooperative association with a pulverized solid fuel nozzle of a firing system of a pulverized solid fuel-fired furnace, comprising:

a first ceramic shell having an inlet end interconnected to the pulverized solid fuel nozzle so as to receive a flow of solid fuel from the nozzle, an outlet end distanced from the inlet end, and a chamber having a peripheral wall defining a first passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the first ceramic shell;

a second ceramic shell having an inlet end interconnected to the outlet end of the first ceramic shell so as to receive the flow of solid fuel from the first ceramic shell, an outlet end distanced from the inlet end of the second ceramic shell, and a chamber having a peripheral wall defining a second passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the second ceramic shell; and

a third ceramic shell having, an inlet end interconnected to the outlet end of the second ceramic shell so as to receive the flow of solid fuel from the second ceramic shell, an outlet end distanced from the inlet end of the third ceramic shell and a chamber having a peripheral wall defining a third passageway for directing the received flow of solid fuel from the inlet end to the outlet end of the third ceramic shell.

10. The solid fuel nozzle tip of claim 9, further comprising:

a first dovetail joint formed by the peripheral walls of the chambers of the first and the second ceramic shells for interconnecting the inlet end of the second ceramic shell to the outlet end of the first ceramic shell; and

a second dovetail joint formed by the peripheral walls of the chambers of the second and the third ceramic shells for interconnecting the inlet end of the third ceramic shell to the outlet end of the second ceramic shell.

11. The solid fuel nozzle tip of claim 10, further comprising:

at least one splitter plate disposed within the first, the second, and the third passageways and attached to the peripheral walls of the chambers of the second and the third ceramic shells.

12. The solid fuel nozzle tip of claim 11, wherein the outlet end of the first ceramic shell is defined by an end surface and the inlet end of the second ceramic shell is defined by an end surface, and further comprising:

a first hole in the end surface of the outlet end of the first ceramic shell and extending into the peripheral wall of the chamber of the first ceramic shell, and a second hole, aligned with the first hole, in the end surface of the inlet end of the second ceramic shell and extending into the peripheral wall of the chamber of the second ceramic shell; and

a connecting member disposed within the first and the second holes.

13. The solid fuel nozzle tip of claim 12, wherein:

the first dovetail joint restrains movement of the second ceramic shell with respect to the first ceramic shell in a first direction;

the second dovetail joint restrains movement of the third ceramic shell with respect to the second ceramic shell in the first direction;

the connecting member restrains movement of the second ceramic shell with respect to the first ceramic shell in a second direction substantially perpendicular to the first direction; and

the at least one splitter plate restrains movement of the third ceramic shell with respect to the second ceramic shell in the second direction.

14. The solid fuel nozzle tip of claim 13, wherein the splitter plate is ceramic.

15. The solid fuel nozzle tip of claim 14, wherein:

the ceramic of the first, the second and the third ceramic shells and the splitter plate is one of the group of ceramics including silicon nitride, siliconized silicon carbide having a silicon content of between about thirty percent (30%) to sixty percent (60%) by weight, mullite bonded silicon carbide alumina composite, reaction-bonded silicon carbide, and alumina zirconia composites.

16. The solid fuel nozzle tip of claim 9, wherein the first ceramic shell is a first unitary ceramic shell, the second ceramic shell is a second unitary ceramic shell, and the third ceramic shell is a third unitary ceramic shell.