Systems and methods for efficient detection of hazardous fuel gas leakage within a gas turbine compartment

US12169168B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12169168-B2
Application numberUS-202217661461-A
CountryUS
Kind codeB2
Filing dateApr 29, 2022
Priority dateMay 4, 2021
Publication dateDec 17, 2024
Grant dateDec 17, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present application provides a hazardous gas detection system to determine hazardous gas concentrations and/or temperatures within a flow of exhaust air in an exhaust duct of a gas turbine compartment. The hazardous gas detection system may include one or more sensors positioned within or in communication with the exhaust duct and a static mixer positioned upstream of the one or more sensors to promote mixing of the flow of exhaust air.

First claim

Opening claim text (preview).

What we claim is: 1. A hazardous gas detection system to determine hazardous gas concentrations and temperatures within a flow of exhaust air in an exhaust duct of a gas turbine compartment, comprising: one or more sensors positioned within or in communication with the exhaust duct; and a static mixer positioned upstream of the one or more sensors to promote mixing of the flow of exhaust air, wherein the static mixer comprises a plurality of ducts and wherein each of the plurality of ducts comprises one or more walls comprising a plurality of apertures. 2. The hazardous gas detection system of claim 1 , wherein the static mixer is positioned within the gas turbine compartment adjacent to the exhaust duct. 3. The hazardous gas detection system of claim 1 , wherein the static mixer is positioned within the exhaust duct adjacent to the gas turbine compartment. 4. The hazardous gas detection system of claim 1 , wherein the exhaust duct comprises an instrumentation duct comprising the one or more sensors and wherein the static mixer is positioned upstream of the instrumentation duct. 5. The hazardous gas detection system of claim 1 , further comprising one or more sampling tubes positioned within the exhaust duct. 6. The hazardous gas detection system of claim 5 , wherein the one or more sensors comprise hazardous gas sensors in communication with the one or more sampling tubes. 7. The hazardous gas detection system of claim 5 , wherein the one or more sensors comprise thermocouples positioned about the one or more sampling tubes. 8. The hazardous gas detection system of claim 1 , wherein the plurality of ducts comprises a pair of ducts positioned in a crossed configuration. 9. The hazardous gas detection system of claim 1 , wherein the one or more walls comprise an entrance wall and an exit wall. 10. The hazardous gas detection system of claim 9 , wherein each of the entrance wall and the exit wall comprises the plurality of apertures therein. 11. The hazardous gas detection system of claim 1 , wherein the one or more walls comprise a lateral side wall and wherein the lateral sidewall comprises the plurality of apertures. 12. The hazardous gas detection system of claim 1 , wherein each of the plurality of ducts comprises a splitter plate therein. 13. The hazardous gas detection system of claim 1 , wherein the plurality of ducts comprises a plurality of angled ducts positioned in a plurality of rows. 14. A method of determining a concentration or temperature of a hazardous gas in a flow of exhaust air in an exhaust duct of a gas turbine compartment, comprising: pulling the flow of exhaust air into the exhaust duct; positioning a static mixer in the flow of exhaust air, wherein the static mixer comprises a plurality of ducts and wherein each of the plurality of ducts includes one or more walls comprising a plurality of apertures; uniformly mixing the hazardous gas within the flow of exhaust air; and sensing the concentration or temperature of the hazardous gas. 15. A hazardous gas detection system to determine hazardous gas concentrations and temperatures within a flow of exhaust air in an exhaust duct of a gas turbine compartment, comprising: one or more gas sensors and one or more temperature sensors positioned within or in communication with the exhaust duct; and a static mixer positioned upstream of the one or more gas sensors and the one or more temperature sensors to promote mixing of the flow of exhaust air; wherein the static mixer comprises a plurality of ducts and wherein each of the plurality of ducts includes one or more walls comprising a plurality of apertures. 16. The hazardous gas detection system of claim 15 , wherein the static mixer is positioned within the gas turbine compartment adjacent to the exhaust duct. 17. The hazardous gas detection system of claim 15 , wherein the static mixer is positioned within the exhaust duct adjacent to the gas turbine compartment. 18. The hazardous gas detection system of claim 15 , wherein the exhaust duct comprises an instrumentation duct comprising the one or more gas sensors and the one or more temperature sensors and wherein the static mixer is positioned upstream of the instrumentation duct.

Assignees

Inventors

Classifications

  • Details with respect to the testing of engines or engine parts · CPC title

  • for tubes · CPC title

  • by using thermal means · CPC title

  • responsive to temperature · CPC title

  • Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title

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What does patent US12169168B2 cover?
The present application provides a hazardous gas detection system to determine hazardous gas concentrations and/or temperatures within a flow of exhaust air in an exhaust duct of a gas turbine compartment. The hazardous gas detection system may include one or more sensors positioned within or in communication with the exhaust duct and a static mixer positioned upstream of the one or more sensor…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification G01N1/38. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Dec 17 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).