Photoacoustic gas sensor and method for operating a photoacoustic gas sensor
US-2019360975-A1 · Nov 28, 2019 · US
US2022074897A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2022074897-A1 |
| Application number | US-202117446507-A |
| Country | US |
| Kind code | A1 |
| Filing date | Aug 31, 2021 |
| Priority date | Sep 10, 2020 |
| Publication date | Mar 10, 2022 |
| Grant date | — |
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A gas sensor having a heater, a receiver, and a space arranged between the heater and the receiver, is described, the heater being configured to generate a thermoacoustic sound wave propagating through the space by using a stimulation signal. The receiver is in this case configured to receive the thermoacoustic sound wave that has propagated through the space and to convert it into a reception signal that has a time-of-flight-dependent shift with respect to the stimulation signal and therefore information relating to the gas concentration in the space.
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1 . A gas sensor comprising: a heater, a receiver, and a space arranged between the heater and the receiver, the heater being configured to generate a thermoacoustic sound wave propagating through the space by using a stimulation signal, and the receiver being configured to receive the thermoacoustic sound wave that has propagated through the space and to convert the thermoacoustic sound wave into a reception signal that has a time-of-flight-dependent shift with respect to the stimulation signal and therefore information relating to the gas concentration in the space. 2 . The gas sensor as claimed in claim 1 , wherein the receiver comprises a microphone. 3 . The gas sensor as claimed in claim 1 , wherein the receiver comprises a temperature sensor. 4 . The gas sensor as claimed in claim 1 further comprising: a gas concentration determination circuit that is configured to determine: a phase shift between the reception signal and a heater signal, or based on the reception signal, a time of flight of the thermoacoustic wave through the space, which are respectively a measure of the gas concentration in the space. 5 . The gas sensor as claimed in claim 4 , wherein the heater signal is the stimulation signal or a temperature signal that indicates a temperature of the heater. 6 . The gas sensor as claimed in claim 5 , wherein the electrical resistance of the heater is temperature-dependent, the gas sensor being configured to generate the temperature signal as a function of the electrical resistance of the heater. 7 . The gas sensor as claimed in claim 1 , which furthermore comprises a thermal conductivity determination circuit that is configured to determine the thermal conductivity of the space based on the heater signal. 8 . The gas sensor as claimed in claim 1 further comprising a driver circuit that is configured to apply the stimulation signal to the heater. 9 . The gas sensor as claimed in claim 1 , wherein at least the heater, the receiver, and the space arranged between the heater and the receiver, are integrated into a microsystem or a MEMS system. 10 . The gas sensor as claimed in claim 9 , wherein the microsystem or the MEMS system comprises a first terminal for application of the stimulation signal to the heater and a second terminal for output of the reception signal. 11 . The gas sensor as claimed in claim 9 , wherein the heater is arranged on a first side of a cavity in the microsystem or the MEMS system, and the receiver comprises a membrane that is arranged at a distance from the heater on a second side of the cavity in the microsystem or the MEMS system. 12 . A method for determining a gas concentration, comprising: applying a stimulation signal to a heater to generate a thermoacoustic sound wave that propagates through a space arranged between the heater and a receiver, receiving the thermoacoustic sound wave at the receiver to generate a reception signal, determining a time-of-flight-dependent shift between a heater signal and the reception signal, and determining the gas concentration in the space based on the time-of-flight-dependent shift. 13 . The method as claimed in claim 12 , wherein the heater signal is a periodic signal and the determination of the time-of-flight-dependent shift comprises determining a phase shift between the reception signal and the heater signal. 14 . The method as claimed in claim 12 , wherein the determination of the time-of-flight-dependent shift comprises determining a time of flight of the thermoacoustic sound wave through the space. 15 . The method as claimed in claim 12 , wherein the heater signal is the stimulation signal that indicates a temperature of the heater or a temperature signal that indicates the temperature of the heater. 16 . The method as claimed in claim 15 , wherein the electrical resistance of the heater is temperature-dependent, and the temperature signal is generated as a function of the electrical resistance of the heater. 17 . The method as claimed in claim 12 , which furthermore comprises determining the thermal conductivity of the space based on the heater signal.
using other means for acoustic excitation, e.g. heat, microwaves, electron beams (sound producing devices not otherwise provided for G10K15/04) · CPC title
by measuring propagation velocity or propagation time of acoustic waves · CPC title
Concentration of a compound, e.g. measured by a surface mass change · CPC title
Attenuation, scattering · CPC title
with stored values, e.g. threshold values · CPC title
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