Description of an air temperature sensor based on O
A-band
Cavity ring down
Flowing air
Optical cavity
Oxygen
Temperature sensor
Journal
Spectrochimica acta. Part A, Molecular and biomolecular spectroscopy
ISSN: 1873-3557
Titre abrégé: Spectrochim Acta A Mol Biomol Spectrosc
Pays: England
ID NLM: 9602533
Informations de publication
Date de publication:
05 Mar 2019
05 Mar 2019
Historique:
received:
28
06
2018
revised:
04
10
2018
accepted:
13
11
2018
pubmed:
21
11
2018
medline:
21
11
2018
entrez:
21
11
2018
Statut:
ppublish
Résumé
In this paper, we describe in detail an assembled open-path optical cavity to act as a temperature sensor of air. A metal absorption cell in a temperature-regulated tube furnace is placed at the center of an optical cavity. The optical cavity consists of two mirrors, two nitrogen buffer sleeves, and the open cell. The air is injected through a fitting in one extreme of the metal tube and travels half the tube length through a channel in the wall of the tube. The channel directs the air towards the center of the cell. The air flowing is heated at the temperature of the metal tube in contact with the furnace. The heated air injected at the center of the tube, flows towards the open extremes of the tube. The nitrogen buffer sleeves protect the mirrors from the heated air. The temperature of the air flowing through the tube is determined by measuring the absorption of the A band of oxygen as a function of the wavenumber in the 769-755 nm wavelength range. The absorption technique is phase-shift cavity ring down spectroscopy. To obtain the temperature, the energy of the lower rotational state for eleven selected rotational transitions is linearly fitted to a logarithmic function that contains the relative intensity of the rotational transition, the initial and final rotational quantum numbers and the energy of the transition. Accuracy of the measurement is determined by comparing the calculated temperature from the spectra with the analog reading of the temperature-regulated tube furnace. This technique is proposed for exhaust air temperature measurements of combustion chambers and cooling air after passing through the blades of a turbine.
Identifiants
pubmed: 30458392
pii: S1386-1425(18)31030-8
doi: 10.1016/j.saa.2018.11.034
pii:
doi:
Types de publication
Journal Article
Langues
eng
Pagination
245-250Informations de copyright
Copyright © 2018 Elsevier B.V. All rights reserved.