Method for determining circumferential sensor positioning

Patent metadata

Field	Value
Publication number	US-9933313-B2
Application number	US-201414478018-A
Country	US
Kind code	B2
Filing date	Sep 5, 2014
Priority date	Sep 6, 2013
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

A method for positioning sensors about a sensor ring includes the steps of assigning each sensor in a plurality of sensors a sensor number selected from a set of sensor numbers, where the set of sensor numbers is a whole number in the range of 0 to N, and where N is the total number of sensors in said plurality of sensors minus one, disposing a first sensor at a circumferential angular position zero on the sensor ring, and disposing each sensor in the plurality of sensors at a circumferential angular position about the sensor ring, wherein the circumferential angular position is defined by an offset from a circumferential angular position zero and the offset is equal to a base arc length between sensors multiplied by the sensor number of the sensor plus a base offset arc length multiplied by the sensor number of the sensor.

First claim

The invention claimed is:

1. A gas turbine engine comprising:
a compressor section;
a combustor fluidly connected to the compressor section via a core flow path, the combustor including a plurality of fuel nozzles having a total number of fuel nozzles, the plurality of fuel nozzles are disposed evenly circumferentially about the combustor;
a turbine section fluidly connected to the combustor via the core flow path;
a plurality of sensors having a total number of sensors, the plurality of sensors disposed circumferentially about the core flow path, the total number of sensors is not equal to the total number of fuel nozzles;
each sensor in said plurality of sensors has a respective sensor number selected from a set of sensor numbers, where each respective sensor number in the set of sensor numbers is a unique whole number in a range of 0 to N, where N is equal to the total number of sensors minus one; and
each sensor of said plurality of sensors is positioned at a respective circumferential offset relative to a circumferential angular position zero, wherein the respective circumferential offset is equal to a base arc length multiplied by the respective sensor number of the sensor plus a base offset arc length multiplied by the respective sensor number of the sensor, the base arc length is 360 degrees divided by the total number of sensors, the base offset arc length is a nozzle arc length divided by the total number of sensors, and the nozzle arc length is 360 degrees divided by the total number of fuel nozzles, wherein the circumferential angular position zero is a circumferential angular position of one of the plurality of fuel nozzles.

2. The gas turbine engine of claim 1 , wherein the total number of fuel nozzles is 16.

3. The gas turbine engine of claim 1 , wherein the total number of sensors is 7.

4. The gas turbine engine of claim 1 , wherein the base offset arc length is approximately 3.21 degrees.

5. The gas turbine engine of claim 1 , wherein the nozzle arc length is an arc length from each fuel nozzle to each adjacent fuel nozzle in the plurality of fuel nozzles.

6. A sensor ring for determining an average sensed value about the sensor ring comprising:
a plurality of sensors disposed circumferentially about said sensor ring for measuring a parameter, the plurality of sensors having a total number of sensors;
wherein the sensor ring has a plurality of expected peaks disposed circumferentially about said sensor ring, wherein each of the plurality of expected peaks corresponds to an expected local peak value of the parameter, the plurality of expected peaks having a total number of expected peaks;
wherein each sensor in said plurality of sensors has a respective sensor number selected from a set of sensor numbers, where each respective sensor number in the set of sensor numbers is a unique whole number in the range of 0 to N, where N is equal to the total number of sensors minus one; and
each sensor of said plurality of sensors is positioned at a respective circumferential offset relative to a circumferential angular position zero, wherein the respective circumferential offset is equal to a base arc length multiplied by the respective sensor number of the sensor plus a base offset arc length multiplied by the respective sensor number of the sensor, the base arc length is equal to 360 degrees divided by the total number of sensors, the base offset arc length is equal to a peak to peak arc length divided by the total number of sensors, and the peak to peak arc length is equal to 360 degrees divided by the total number of expected peaks; and
the total number of sensors is not equal to the total number of expected peaks, wherein the circumferential angular position zero is a circumferential angular position of one of the plurality of expected peaks.

7. A method for positioning a plurality of sensors about a sensor ring for measuring a parameter, the sensor ring having a plurality of expected peaks disposed circumferentially about said sensor ring, wherein each of the plurality of expected peaks corresponds to an expected local peak value of the parameter, the plurality of sensors having a total number of sensors and the plurality of expected peaks having a total number of expected peaks, the method comprising the steps of:
assigning each sensor in the plurality of sensors a respective sensor number selected from a set of sensor numbers, where each respective sensor number in the set of sensor numbers is a unique whole number in the range of 0 to N, where N is the total number of sensors minus one;
disposing each sensor in said plurality of sensors at a respective circumferential angular position about said sensor ring, wherein the respective circumferential angular position is defined by a respective circumferential offset relative to a circumferential angular position zero, the respective circumferential offset is equal to a base arc length multiplied by the respective sensor number of the sensor plus a base offset arc length multiplied by the respective sensor number of the sensor, the base arc length is equal to 360 degrees divided by the total number of sensors, the base offset arc length is equal to a peak to peak arc length divided by the total number of sensors, and the peak to peak arc length is equal to 360 degrees divided by the total number of expected peaks; and
the total number of sensors is not equal to the total number of expected peaks, wherein the circumferential angular position zero is a circumferential angular position of one of the plurality of expected peaks.

Assignees

• United Technologies Corp

Inventors

• Agrawal Rajendra K

Classifications

• G01K2013/024

  Physics · mapped topic

• F05D2220/32

  in gas turbines · CPC title

• G01K2205/00

  Application of thermometers in motors, e.g. of a vehicle · CPC title

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• Y10T29/49826

  Assembling or joining · CPC title