Gas turbine vane body with instrumentation
US-2024287912-A1 · Aug 29, 2024 · US
US9528880B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9528880-B2 |
| Application number | US-201313969186-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 16, 2013 |
| Priority date | Aug 16, 2013 |
| Publication date | Dec 27, 2016 |
| Grant date | Dec 27, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A temperature measurement system includes a plurality of filaments. The plurality of filaments are configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band at least partially representative of a temperature of the plurality of filaments. A first and second portion of the filaments has a differing first and a second diameter and/or emissivity, respectively. The system also includes a detector array configured to generate electrical signals at least partially representative of the thermal radiation received from the filaments. The system further includes a controller communicatively coupled to the detector array configured to transform the first electrical signals to a first temperature indication at least partially as a function of the first diameter and/or first emissivity and transform the second electrical signals to a second temperature indication at least partially as a function of the second diameter and/or emissivity.
Opening claim text (preview).
What is claimed is: 1. A temperature measurement system comprising: a plurality of filaments configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band at least partially representative of a temperature of said plurality of filaments, wherein: at least a first portion of said plurality of filaments has at least one of a first diameter and a first emissivity; and at least a second portion of said plurality of filaments has at least one of a second diameter that is different from the first diameter and a second emissivity; an optical system configured to receive at least a portion of the thermal radiation emitted from said plurality of filaments, said optical system comprising a detector array configured to: generate first electrical signals at least partially representative of the thermal radiation received from said first portion of said plurality of filaments; generate second electrical signals at least partially representative of the thermal radiation received from said second portion of said plurality of filaments; and a controller communicatively coupled to said detector array, said controller configured to: transform the first electrical signals to a first temperature indication at least partially as a function of at least one of the first diameter and the first emissivity; and transform the second electrical signals to a second temperature indication at least partially as a function of at least one of the second diameter and the second emissivity. 2. The system in accordance with claim 1 , wherein said controller is further configured to calculate a third temperature indication from the first temperature indication and the second temperature indication, wherein the third temperature indication is at least partially a function of a third diameter having a value of zero. 3. The system in accordance with claim 2 , wherein the first, second, and third temperature indications are representative of a portion of at least one of a two-dimensional and a three-dimensional temperature map across a predetermined volume. 4. The system in accordance with claim 2 , wherein the first temperature indication, the second temperature indication, and the third temperature indication have one of a linear relationship and a nonlinear relationship with each other. 5. The system in accordance with claim 1 , wherein said controller is further configured to calculate a third temperature indication from the first temperature indication and the second temperature indication, wherein the third temperature indication is at least partially a function of a third emissivity having a value of zero. 6. The system in accordance with claim 5 , wherein the third temperature indication is representative of a portion of at least one of a two-dimensional and a three-dimensional temperature map across a predetermined volume. 7. The system in accordance with claim 5 , wherein the first temperature indication, the second temperature indication, and the third temperature indication have one of a linear relationship and a nonlinear relationship with each other. 8. The system in accordance with claim 1 , wherein said first portion and said second portion of said plurality of filaments are proximate each other within a predetermined volume. 9. The system in accordance with claim 1 , wherein the first diameter and the second diameter have values within a range between approximately 10 microns and approximately 5.0 millimeters. 10. The system in accordance with claim 1 , wherein the first emissivity and the second emissivity have values within a range between approximately 0.3 and approximately 1.0. 11. The system in accordance with claim 1 , wherein said plurality of filaments comprises at least one of silicon carbide, sapphire, fused silica, tungsten, graphite, and stainless steel. 12. The system in accordance with claim 1 , further comprising a wavelength splitting device configured to split the thermal radiation emitted from said plurality of filaments into at least one relatively narrow wavelength band of thermal radiation, said detector array configured to receive the at least one relatively narrow wavelength band of thermal radiation, wherein said controller is further configured to determine a temperature of one or more of said plurality of filaments without correcting for absorption and emission of thermal radiation from water (H2O) and carbon dioxide (CO2). 13. The system in accordance with claim 12 , wherein the at least one relatively narrow wavelength band of thermal radiation is a plurality of relatively narrow wavelength bands of thermal radiation, wherein said controller is further configured to determine a temperature of one or more of said plurality of filaments using multi-color pyrometry (MCP). 14. The system in accordance with claim 1 , wherein the second emissivity is equal to the first emissivity. 15. The system in accordance with claim 1 , wherein the second emissivity is different from the first emissivity. 16. A method of temperature measurement comprising: positioning a plurality of filaments in a flow path of a fluid, at least a first portion of the plurality of filaments has at least one of a first diameter and a first emissivity and at least a second portion of the plurality of filaments has a second diameter that is different from the first diameter and a second emissivity; positioning an optical system proximate the plurality of filaments; transmitting thermal radiation from the plurality of filaments to the optical system, the thermal radiation at least partially representative of a temperature of the plurality of filaments; generating first electrical signals at least partially representative of the thermal radiation received from the first portion of the plurality of filaments; generating second electrical signals at least partially representative of the thermal radiation received from the second portion of the plurality of filaments; transforming the first electrical signals to a first temperature indication at least partially as a function of at least one of the first diameter and the first emissivity; transforming the second electrical signals to a second temperature indication at least partially as a function of at least one of the second diameter and the second emissivity; and transmitting the first and second temperature indications to a processor. 17. The method in accordance with claim 16 further comprising calculating a third temperature indication from the first temperature indication and the second temperature indication, wherein the third temperature indication is at least partially a function of a third diameter having a value of zero. 18. The method in accordance with claim 17 , wherein calculating a third temperature indication from the first temperature indication and the second temperature indication comprises generating at least one of a two-dimensional and a three-dimensional temperature map across a predetermined volume. 19. The method in accordance with claim 16 further comprising calculating a third temperature indication from the first temperature indication and the second temperature indication, wherein the third temperature indication is at least partially a function of a third emissivity having a value of zero. 20. The method in accordance with claim 19 , wherein calculating a third temperature indication from the first temperature indication and the second temperature indication comprises generating at least one of a two-dimensional and a thre
for sensing the radiation from gases, flames · CPC title
Testing gas-turbine engines or jet-propulsion engines · CPC title
using determination of colour temperature · CPC title
using electric radiation detectors · CPC title
Integrating cavities mimicking black bodies, wherein the heat propagation between the black body and the measuring element does not occur within a solid; Use of bodies placed inside the fluid stream for measurement of the temperature of gases; Use of the reemission from a surface, e.g. reflective surface; Emissivity enhancement by multiple reflections · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.