Non-symmetric arrangement of fuel nozzles in a combustor

Patent metadata

Field	Value
Publication number	US-9310072-B2
Application number	US-201213542808-A
Country	US
Kind code	B2
Filing date	Jul 6, 2012
Priority date	Jul 6, 2012
Publication date	Apr 12, 2016
Grant date	Apr 12, 2016

Abstract

A fuel nozzle arrangement includes an annular combustor having four quadrants. Fuel injectors are located in the four quadrants and each fuel injector has either a first or second type nozzle attached to it. The first and second type fuel nozzles are located in an array so that at least two of one nozzle type are located together to allow for non-uniform injector spacing with uniform downstream temperatures.

First claim

The invention claimed is:

1. A fuel nozzle arrangement comprising:
an annular combustor having four quadrants;
a plurality of fuel injectors disposed in the four quadrants; and
a plurality of fuel nozzles of a first type and second type disposed onto the plurality of fuel injectors so that each fuel injector of the plurality of fuel injectors has either one first type fuel nozzle or one second type fuel nozzle attached to it, wherein the first type fuel nozzles are configured to provide a higher fuel flow than the second type fuel nozzles;
wherein the plurality of fuel injectors with attached first type and second type fuel nozzles are disposed with varying circumferential spacing which defines a circumferential array of the first type fuel nozzles and second type fuel nozzles in which at least two fuel nozzles of the same type are adjacent to each other, wherein the plurality of fuel nozzles of the circumferential array are spaced non-uniformly so that circumferential spacing between any two adjacent second type fuel nozzles is less than circumferential spacing between a second type fuel nozzle and an adjacent first type fuel nozzle, and the circumferential spacing between the second type fuel nozzle and the adjacent first type fuel nozzle is less than circumferential spacing between any two adjacent first type fuel nozzles, wherein adjacent fuel nozzles do not have any other fuel nozzle between them.

2. The arrangement of claim 1 , wherein the four quadrants divide the annular combustor into four 90° segments.

3. A fuel nozzle arrangement comprising:
an annular combustor;
a plurality of fuel injectors circumferentially disposed in the combustor; and
a plurality of first type fuel nozzles configured to provide a first fuel flow and a plurality of second type fuel nozzles configured to provide a second, lower fuel flow, the plurality of first type fuel nozzles and the plurality of second type fuel nozzles disposed onto the plurality of fuel injectors so that each fuel injector of the plurality of fuel injectors has either one first type fuel nozzle or one second type fuel nozzle attached to it;
wherein the plurality of fuel injectors with attached first type and second type fuel nozzles are disposed with varying circumferential spacing which defines a circumferential array of the first and second type fuel nozzles wherein the plurality of fuel nozzles are arranged in a non-alternating pattern of first type fuel nozzles and second type fuel nozzles, so that at least one of one type of fuel nozzle is located adjacent to an identical type of fuel nozzle, and so that circumferential spacing between any two adjacent second type fuel nozzles is less than circumferential spacing between a second type fuel nozzle and an adjacent first type fuel nozzle, and the circumferential spacing between the second type fuel nozzle and the adjacent first type fuel nozzle is less than circumferential spacing between any two adjacent first type fuel nozzles, wherein adjacent fuel nozzles do not have any other fuel nozzle between them.

4. The arrangement of claim 3 , wherein:
the annular combustor has four quadrants; and
at least two quadrants contain an unequal number of first type fuel nozzles and second type fuel nozzles.

5. A fuel nozzle arrangement comprising:
an annular combustor;
a plurality of fuel injectors disposed in the combustor; and
a plurality of fuel nozzles of a first type and second type disposed onto the plurality of fuel injectors so that each fuel injector of the plurality of fuel injectors has either one first type fuel nozzle or one second type fuel nozzle attached to it;
wherein the plurality of fuel injectors with attached first type and second type fuel nozzles are disposed with varying circumferential spacing that defines an array of the first type fuel nozzles and second type fuel nozzles, wherein the first type fuel nozzles and second type fuel nozzles are arranged in a non-uniformly spaced circumferential array with at least one pair of first type fuel nozzles or least one pair of second type fuel nozzles being adjacent one another, so that circumferential spacing between any two adjacent second type fuel nozzles is less than circumferential spacing between a second type fuel nozzle and an adjacent first type fuel nozzle, and the circumferential spacing between the second type fuel nozzle and the adjacent first type fuel nozzle is less than circumferential spacing between any two adjacent first type fuel nozzles, wherein adjacent fuel nozzles do not have any other fuel nozzle between them.

6. The arrangement of claim 5 , wherein the annular combustor has four quadrants; and wherein at least two quadrants contain an unequal number of first type fuel nozzles and second type fuel nozzles.

7. The arrangement of claim 6 , wherein at least one quadrant is bounded by a first type fuel nozzle and contains at least one first type fuel nozzle and one second type fuel nozzle.

Assignees

• Ainslie Walter Ernest
• Hamilton Sundstrand Corp

Inventors

• Ainslie Walter Ernest

Classifications

• F23R2900/00014

  Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators · CPC title

• F23R2900/00013

  Reducing thermo-acoustic vibrations by active means · CPC title

• F23C5/08 Primary

  Disposition of burners · CPC title

• F23R3/28

  characterised by the fuel supply (burners F23D) · CPC title