Split nozzle tip for pulverized coal burner

• US 4,634,054 A
• Filed: 03/14/1985
• Issued: 01/06/1987
• Est. Priority Date: 04/22/1983
• Status: Expired due to Term

• Current Assignee: ALSTOM Power Inc. (General Electric Company)
• Original Assignee: Combustion Engineering Incorporated (ABB Limited)
• Inventors: Grusha, John
• Primary Examiner(s): Peters, Jr., Joseph F.
• Assistant Examiner(s): WELDON, KEVIN P
• Application Number:
  US06/712,454
• Time in Patent Office: 663 Days
• Field of Search: 239/552, 239/498, 239/502, 239/512, 239/522, 239/524, 239/589, 239/590.5, 239/549, 239/418, 239/423, 239/424, 239/502, 239/512, 239/522, 239/521, 110/263
• US Class Current: 239/423
• CPC Class Codes: F23C 5/06 Provision for adjustment of burner position during operation
• CPC Class Codes: F23C 7/02 Disposition of air supply not passing through burner to obtain a cyclonic tapering flame when burning pulverulent fuel F23C5/32
• CPC Class Codes: F23D 1/00 Burners for combustion of pulverulent fuel disposition of burners F23C
• CPC Class Codes: F23D 2201/101 tiltable

Abstract

An improved nozzle tip (30) which provides enhanced ignition and stabilization of pulverized fuel flames in furnaces operating at low load. The nozzle tip (30) comprises open-ended inner and outer shells (32,34) mounted to the fuel delivery pipe (12) and defining a flow passageway within the inner shell through which the pulverized fuel is directed into the furnace and an annular flow passageway (50) between the inner and outer shells through which additional air is directed into the furnace. A pair of diverging splitter plates (41,42) are disposed within the inner shell (32) so as to divide the flow passageway therethrough into two separate, diverging subpassages (52,54) so that the pulverized fuel stream discharging from the fuel delivery pipe is split into first and second streams (60,70) which pass from the nozzle tip (30) into the furnace in a diverging manner thereby establishing an ignition stabilizing pocket in the low pressure zone (80) created between the diverging fuel streams.

Claims

1. A nozzle tip for a burner on a pulverized fuel fired furnace comprising:

a. an open-ended inner shell having an inlet end and an outlet end and defining therebetween a flow passageway through which a mixture of pulverized fuel and transport air passes from the burner into the furnace;

b. an open-ended outer shell spaced from and surrounding said inner shell thereby defining an annular flow passageway therebetween through which additional air passes from the burner into the furnace; and

c. first and second splitter plates disposed within said inner shell, each having a leading edge portion disposed transversely across the flow passageway of said inner shell at the inlet end thereof and a trailing edge portion extending transversely across the flow passageway of said inner shell at the outlet end thereof, said first and second splitter plates converging at the inlet end of said inner shell and extending outwardly therefrom in a diverging manner toward the outlet end of said inner shell, said first and second splitter plates thereby dividing the flow passageway through said inner shell into a first flow passage bounded by the first splitter plate and said inner shell and a second flow passage bounded by the second splitter plate and said inner shell, said first and second flow passages diverging in the direction of flow through the nozzle tip and being spaced apart at the outlet end of the nozzle tip so as to establish a void region therebetween through which flow directly from the nozzle tip is precluded, the trailing edge portion of each of said first and second splitter plates being formed of a plurality of longitudinally elongated strips extending longitudinally outward from the leading edge portion of each of said first and second splitter plates in a side-by-side relationship transversely across the flow passageway of said inner shell, a first portion of said trailing edge strips disposed alternately between a second portion of said trailing edge strips and bent radially away from the leading edge portion of each of said first and second splitter plates thereby forming a scalloped tailing edge portion of each of said first and second splitter plates.

2. A nozzle tip as recited in claim 1 wherein the second portion of said trailing edge strips is bent radially away from the leading edge portion of each of said first and second splitter plates in the direction opposite to that in which the first portion of said trailing edge strips are bent radially away from the leading edge portion of each of said first and second splitter plates.

3. A nozzle tip as recited in claim 1 further comprising a plurality of filler plates disposed transversely between adjacent first and second portions of said trailing edge strips along the interface therebetween thereby precluding the flow of pulverized fuel and transport air across the interface formed between adjacent diverging first and second portions of said trailing edge strips.

4. A nozzle tip as recited in claim 1 wherein the leading edge portions of said first and second splitter plates diverge at an included angle of approximately twenty degrees.