Fuel system and method for supplying a combustion chamber in an aircraft turboshaft engine with fuel
US-2024318601-A1 · Sep 26, 2024 · US
US9791154B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9791154-B2 |
| Application number | US-201414646729-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 30, 2014 |
| Priority date | Jun 18, 2013 |
| Publication date | Oct 17, 2017 |
| Grant date | Oct 17, 2017 |
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A power generation system includes: a combustor operative to combust a fuel; a power generator operative to utilize energy obtained from the combustor when generating electric power; a fuel supplier operative to supply the fuel to the combustor; an air supplier operative to supply combustion air to the combustor; a discharged gas passage through which a discharged gas from the combustor flows; a CO detector operative to detect CO in the discharged gas; a temperature detector operative to detect a temperature of the discharged gas; and control circuitry operative to, when the discharged gas is flowing through the discharged gas passage, perform at least one of an operation of detecting a structural abnormality of the discharged gas passage based on a difference between detected temperatures of the temperature detector relative to a difference between heated amounts of the discharged gas heated by a heater and an operation of detecting the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to a difference between outputs of at least one of the fuel supplier and the air supplier.
Opening claim text (preview).
The invention claimed is: 1. A power generation system comprising: a combustor operative to combusts a fuel; a power generator operative to utilize energy obtained from the combustor when generating electric power; a fuel supplier operative to supply the fuel to the combustor; an air supplier operative to supply combustion air to the combustor; a discharged gas passage through which a discharged gas from the combustor flows; a CO detector operative to detect CO in the discharged gas; a temperature detector operative to detect a temperature of the discharged gas; and control circuitry operative to, when the discharged gas is flowing through the discharged gas passage, perform at least one of: an operation of detecting a structural abnormality of the discharged gas passage based on a difference between detected temperatures of the temperature detector relative to a difference between heated amounts of the discharged gas heated by a heater, and an operation of detecting the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to a difference between outputs of at least one of the fuel supplier and the air supplier. 2. The power generation system according to claim 1 , wherein the heater is disposed on the discharged gas passage and located at an upstream side of a flow of the discharged gas, and the temperature detector is disposed on the discharged gas passage and located at a downstream side of the flow of the discharged gas. 3. The power generation system according to claim 1 , wherein the heater is disposed on the discharged gas passage and located at a downstream side of a flow of the discharged gas, and the temperature detector is disposed on the discharged gas passage and located at an upstream side of the flow of the discharged gas. 4. The power generation system according to claim 2 , wherein the CO detector is disposed on the discharged gas passage and located between the heater and the temperature detector. 5. The power generation system according to claim 1 , wherein when the air supplier is supplying the air in a state where the combustor is not performing combustion, the control circuitry executes at least one of: an operation of detecting the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to a difference between the heated amounts of the air discharged from the combustor and heated by the heater; and an operation of, while the heater is heating the air discharged from the combustor, detecting the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to a difference between the outputs of the air supplier. 6. The power generation system according to claim 1 , wherein while the heater is heating the discharged gas when the discharged gas is flowing through the discharged gas passage, the control circuitry detects the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to the difference between the outputs of at least one of the fuel supplier and the air supplier. 7. The power generation system according to claim 1 , wherein the power generator includes: a reformer operative to generate a hydrogen-containing gas by using a raw material; and a fuel cell operative to generate the electric power by using the hydrogen-containing gas. 8. The power generation system according to claim 1 , wherein the power generator includes an electric generator operative to generate electric power by using power obtained from an engine serving as the combustor. 9. The power generation system according to claim 7 , further comprising: a branch passage branching from the discharged gas passage; and a blocker which is disposed on the branch passage and operative to block a flow of the discharged gas, wherein: the CO detector is disposed on the branch passage; the combustor combusts the hydrogen-containing gas as the fuel; the temperature detector detects the temperature of the discharged gas flowing through the branch passage; and when the discharged gas is flowing through the discharged gas passage, the control circuitry cancels blocking of the blocker and detects sticking of the blocker based on the detected temperatures detected by the temperature detector after the blocking of the blocker is canceled. 10. The power generation system according to claim 9 , wherein when canceling at least the blocking of the blocker, the control circuitry activates the heater disposed on the branch passage and located upstream of the temperature detector. 11. The power generation system according to claim 1 , wherein when the structural abnormality of the discharged gas passage is detected, the control circuitry causes an informer to inform of the structural abnormality of the discharged gas passage. 12. A method of operating a power generation system, the method comprising: combusting a fuel by a combustor; utilizing energy obtained by the combustor to generate electric power by a power generator; and when a discharged gas is flowing from the combustor through a discharged gas passage, performing at least one of: an operation of detecting a structural abnormality of the discharged gas passage based on a difference between detected temperatures of a temperature detector relative to a difference between heated amounts of the discharged gas heated by a heater, and an operation of detecting the structural abnormality of the discharged gas passage based on the difference between the detected temperatures of the temperature detector relative to a difference between outputs of at least one of a fuel supplier and an air supplier. 13. The power generation system according to claim 1 , wherein the structural abnormality of the discharged gas passage includes break of the discharged gas passage. 14. The power generation system according to claim 1 , wherein the structural abnormality of the discharged gas passage includes come-off of the discharged gas passage. 15. The power generation system according to claim 1 , wherein the structural abnormality of the discharged gas passage includes clogging of the discharged gas passage. 16. The power generation system according to claim 1 , wherein the discharged gas passage is a flow passage in which combustion of the fuel is not performed and the temperature detector is provided on the discharged gas passage or a branch passage of the discharged gas passage.
stack temperature · CPC title
the fuel containing hydrogen · CPC title
of auxiliary devices, e.g. batteries, capacitors · CPC title
Concentration; Density (H01M8/04492 takes precedence) · CPC title
the reforming step being a steam reforming step · CPC title
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