Optical fiber sensor system for detecting temperature changes in an aircraft
First Claim
1. An optical fibre sensor system arranged to detect a temperature change in a zone in an aircraft having at least one zone, the optical fibre sensor system comprising:
- at least one optical fibre comprising a plurality of Fibre Bragg Gratings for detecting a temperature change, wherein each of the Fibre Bragg Gratings is reflecting radiation within a predetermined wavelength range;
a radiation source unit arranged to emit radiation into the at least one optical fibre;
a radiation detector unit arranged to receive radiation from the at least one optical fibre;
the processing unit configured to identify a spectral response of the received radiation and to determine a temperature change from the spectral response of the received radiation in a predetermined wavelength range;
wherein each of the at least one zone solely has Fibre Bragg Gratings which are reflecting radiation within the same predetermined wavelength range; and
each of at least one Bragg wavelength of the spectral response is determined by identifying a rising or falling edge of the spectral response.
1 Assignment
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Accused Products
Abstract
The present disclosure relates to an optical fiber sensor system (10) arranged to detect a temperature change in a zone (2, 3, 4) in an aircraft (1) having at least one zone (2, 3, 4). The optical fiber sensor system (10) comprises at least one optical fiber (11, 21, 31, 41) comprising a plurality of Fiber Bragg Gratings (20, 30, 40) for detecting a temperature change. Each of the Fiber Bragg Gratings (20, 30, 40) is reflecting radiation within a predetermined wavelength range. A radiation source unit (13) is arranged to emit radiation into the at least one optical fiber (11, 21, 31, 41). A radiation detector unit (14) is arranged to receive radiation from the at least one optical fiber (11, 21, 31, 41). A processing unit (15) is configured to identify a spectral response (22, 32, 42) of the received radiation and to determine a temperature change from the spectral response (22, 32, 42) of the received radiation in a predetermined wavelength range. Each of the at least one zone (2, 3, 4) solely has Fiber Bragg Gratings (20, 30, 40) which are reflecting radiation within the same predetermined wavelength range. The disclosure further relates to method for detecting a temperature change in a zone in an aircraft having at least one zone, by means of the optical fiber sensor system. Yet further the disclosure relates to an aircraft (1) comprising the optical fiber sensor system (10).
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Citations
15 Claims
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1. An optical fibre sensor system arranged to detect a temperature change in a zone in an aircraft having at least one zone, the optical fibre sensor system comprising:
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at least one optical fibre comprising a plurality of Fibre Bragg Gratings for detecting a temperature change, wherein each of the Fibre Bragg Gratings is reflecting radiation within a predetermined wavelength range; a radiation source unit arranged to emit radiation into the at least one optical fibre; a radiation detector unit arranged to receive radiation from the at least one optical fibre; the processing unit configured to identify a spectral response of the received radiation and to determine a temperature change from the spectral response of the received radiation in a predetermined wavelength range; wherein each of the at least one zone solely has Fibre Bragg Gratings which are reflecting radiation within the same predetermined wavelength range; and each of at least one Bragg wavelength of the spectral response is determined by identifying a rising or falling edge of the spectral response. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. A method for detecting a temperature change in a zone in an aircraft having at least one zone, by means of an optical fibre sensor system, the optical fibre sensor system comprising at least one optical fibre comprising a plurality of Fibre Bragg Gratings for detecting a temperature change, wherein each of the Fibre Bragg Gratings is reflecting radiation within a predetermined wavelength range, the method comprising the steps of;
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emitting, from a radiation source unit, radiation into the at least one optical fibre; receiving, by a radiation detector unit, radiation from the at least one optical fibre; identifying, by a processing unit, a spectral response of the received radiation; determining, by a processing unit, a temperature change from the spectral response of the received radiation in a predetermined wavelength range; wherein each of the at least one zone solely has Fibre Bragg Gratings which are reflecting radiation within the same predetermined wavelength range; and determining each of at least one Bragg wavelength of the spectral response by identifying a rising or falling edge of the spectral response. - View Dependent Claims (14, 15)
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Specification