Belt for measuring the temperature of an object
US-2018259395-A1 · Sep 13, 2018 · US
US9287014B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9287014-B2 |
| Application number | US-201414330010-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 14, 2014 |
| Priority date | Apr 24, 2013 |
| Publication date | Mar 15, 2016 |
| Grant date | Mar 15, 2016 |
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A nuclear power distribution measurement assembly that is sized to fit within an instrumentation thimble of a nuclear fuel assembly, that employs a spaced tandem arrangement of thermo-acoustic engines, each of which has a heat source side that is insulated from the reactor coolant traversing the nuclear core in which the fuel assembly is to be placed and a cold side housing a resonator chamber with enhanced thermal conductance to the coolant. The resonator chamber of each of the thermo-acoustic engines is of a different length to generate a different frequency whose amplitude is proportional to the neutron activity at the axial and radial position of the thermo-acoustic engine. The frequency identifies the measurement assembly's position. Acoustic telemetry is employed to monitor the acoustic waves generated by the individual thermo-acoustic engines to provide a remote reading of the axial and radial power distribution of a reactor core.
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What is claimed is: 1. A thermo-acoustic nuclear power distribution measurement assembly comprising: a plurality of thermo-acoustic engines supported in a spaced tandem array and sized to fit within an instrument thimble in a nuclear fuel assembly along an axial length of the fuel assembly; wherein said plurality of thermo-acoustic engines include at least one pair of thermo-acoustic engines; wherein each thermo-acoustic engine of the plurality of thermo-acoustic engines includes an outer cladding, a self-sustaining heat source, a resonant chamber and a heat exchanger stack; wherein the cladding is sized to fit within the instrument thimble to enable coolant to flow around an outside surface of the cladding; wherein the cladding surrounds the heat source, the resonant chamber and the heat exchanger stack; wherein the cladding includes a cladding interior; wherein the cladding interior includes one end and another end; wherein the heat source is supported within the cladding interior at a first side of the heat exchanger stack facing the one end; wherein the resonant chamber is located within the cladding interior at a second side of the heat exchanger stack facing the another end; wherein the heat source is separated from the resonant chamber; wherein the heat exchanger stack is located within the cladding interior; wherein the heat exchanger stack separates the heat source from the resonant chamber; wherein each respective resonant chamber of the plurality of thermo-acoustic engines is configured to generate a sound having a frequency that differs from every other respective resonant chamber of the plurality of thermo-acoustic engines; wherein for each respective resonant chamber, the sound frequency generated by the respective resonant chamber allows that respective resonant chamber to be uniquely identified from the other respective resonant chambers of said plurality of thermo-acoustic engines; wherein for each respective resonant chamber, a difference in temperature between: a first location which is within the respective resonant chamber on the second side of the heat exchanger stack and a second location which is on the first side of the heat exchanger stack that is heated by the heat source, wherein the second side is opposite the first side; and causes the respective resonant chamber to generate a sound with a frequency which comprises an amplitude, wherein the amplitude generated corresponds to the difference in temperature between the first location and the second location, wherein the amplitude generated also corresponds to a nuclear power level at an axial location of the respective resonant chamber; wherein a portion of the cladding that surrounds the resonant chamber is thermally conductive; and a spacer interposed between the thermo-acoustic engines of each pair of thermo-acoustic engines. 2. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein a portion of the cladding that surrounds the self-sustaining heat source is thermally insulated. 3. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein the spacers are configured to thermally insulate the heat source of a first engine of a pair of the thermo-acoustic engines from a second engine of the pair of thermo-acoustic engines. 4. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein the self-sustaining heat source of at least some of the plurality of thermo-acoustic engines is supported within a portion of a lower end of the cladding. 5. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 and further including an acoustic telemetry system, wherein the acoustic telemetry system is configured to have acoustic sensors receive at a location outside of a nuclear reactor vessel, sound generated by substantially each respective engine of the plurality of thermo-acoustic engines, when the thermo-acoustic nuclear power distribution measurement assembly is positioned within the nuclear reactor vessel during operation of a corresponding reactor power generation system. 6. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein the spaced tandem array of the plurality of thermo-acoustic engines is configured to substantially span a height of a nuclear fuel assembly instrument thimble. 7. The thermo-acoustic nuclear power distribution measurement assembly of claim 6 wherein the tandem array of the plurality of thermo-acoustic engines comprises seven thermo-acoustic engines. 8. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein the self-sustaining heat source comprises fissile material. 9. The thermo-acoustic nuclear power distribution measurement assembly of claim 1 wherein the self-sustaining heat source is formed from a material operable to convert fission gamma radiation into a quantity of heat that is able to cause the resonant chamber to generate the different frequency of sound with the amplitude. 10. The thermo-acoustic nuclear power distribution measurement assembly of claim 9 wherein the self-sustaining heat source comprises Tungsten. 11. A nuclear power generation system comprising: a nuclear reactor having a core; a plurality of nuclear fuel assemblies supported within the core, at least some of the fuel assemblies have an instrument thimble having an axial length that spans a height of the corresponding fuel assembly; a thermo-acoustic nuclear power distribution measurement assembly positioned within at least some of the instrument thimbles, the thermo-acoustic nuclear power distribution measurement assembly comprising: a plurality of thermo-acoustic engines supported in a spaced tandem array and sized to fit within an instrument thimble in a nuclear fuel assembly along the axial length; wherein said plurality of thermo-acoustic engines include at least one pair of thermo-acoustic engines; wherein each thermo-acoustic engine of the plurality of thermo-acoustic engines includes an outer cladding, a self-sustaining heat source, a resonant chamber and a heat exchanger stack; wherein the cladding is sized to fit within the instrument thimble to enable coolant to flow around an outside surface of the cladding; wherein the cladding surrounds the heat source, the resonant chamber and the heat exchanger stack; wherein the cladding includes a cladding interior; wherein the cladding interior includes one end and another end; wherein the heat source is supported within the cladding interior at the one end; wherein the resonant chamber is located within the cladding interior at the another end; wherein the heat source is separated from the resonant chamber; wherein the heat exchanger stack is located within the cladding interior; wherein the heat exchanger stack separates the heat source from the resonant chamber; wherein each respective resonant chamber of the plurality of thermo-acoustic engines is configured to generate a sound having a frequency that differs from every other respective resonant chamber of the plurality of thermo-acoustic engines; wherein for each respective resonant chamber, the sound frequency generated by the respective resonant chamber allows that respective resonant chamber to be uniquely identified from the other respective resonant chambers of said plurality of thermo-acoustic engines; wherein for each respective resonant chamber, a difference in temperature between: a first location which is within the respective resonant chamber on the second side of the heat exchanger stack, and a second location which is on the first side of the heat exchanger stack that is heat
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