On-line parameters measurement of combustion flame in engineusing radiation spectroscopy

Bin Yang; Xin Yang Gui; Wu Zhou; Yong Jun Jiang; Fei Qin; Xiao Shu Cai; Guo Qiang He

doi:10.13224/j.cnki.jasp.2015.12.013

On-line parameters measurement of combustion flame in engineusing radiation spectroscopy

Bin Yang, Xin Yang Gui, Wu Zhou, Yong Jun Jiang, Fei Qin, Xiao Shu Cai, Guo Qiang He

School of Astronautics

University of Shanghai for Science and Technology

Research output: Contribution to journal › Article › peer-review

8 Scopus citations

Abstract

For the non-intrusive, on-line and in-situ measurement of high-temperature combustion flame in engine, the method based on radiation spectroscopy (RS) was presented. The system using optical fiber spectrometer was designed for on-line parameters measurements of flame in engine. The wavelength response of charge-coupled device (CCD) was calibrated by the blackbody furnace. Then, the radiation spectroscopy range of 200-1100 nm wavelength of high temperature flame in rocket based combined cycle (RBCC) engine ground testing was obtained by using this system, and the temperature and radiance of flame were determined with Planck radiation law and the least square method. It can provide important reference for combustion diagnostics and optimization of engine.

Original language	English
Pages (from-to)	2904-2909
Number of pages	6
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	30
Issue number	12
DOIs	https://doi.org/10.13224/j.cnki.jasp.2015.12.013
State	Published - 1 Dec 2015

Keywords

Combustion diagnostics of engine
Combustion flam parameters
On-line measurement
Radiation spectroscopy
Thermometry

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10.13224/j.cnki.jasp.2015.12.013

Cite this

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title = "On-line parameters measurement of combustion flame in engineusing radiation spectroscopy",

abstract = "For the non-intrusive, on-line and in-situ measurement of high-temperature combustion flame in engine, the method based on radiation spectroscopy (RS) was presented. The system using optical fiber spectrometer was designed for on-line parameters measurements of flame in engine. The wavelength response of charge-coupled device (CCD) was calibrated by the blackbody furnace. Then, the radiation spectroscopy range of 200-1100 nm wavelength of high temperature flame in rocket based combined cycle (RBCC) engine ground testing was obtained by using this system, and the temperature and radiance of flame were determined with Planck radiation law and the least square method. It can provide important reference for combustion diagnostics and optimization of engine.",

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author = "Bin Yang and Gui, {Xin Yang} and Wu Zhou and Jiang, {Yong Jun} and Fei Qin and Cai, {Xiao Shu} and He, {Guo Qiang}",

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T1 - On-line parameters measurement of combustion flame in engineusing radiation spectroscopy

AU - Yang, Bin

AU - Gui, Xin Yang

AU - Zhou, Wu

AU - Jiang, Yong Jun

AU - Qin, Fei

AU - Cai, Xiao Shu

AU - He, Guo Qiang

PY - 2015/12/1

Y1 - 2015/12/1

N2 - For the non-intrusive, on-line and in-situ measurement of high-temperature combustion flame in engine, the method based on radiation spectroscopy (RS) was presented. The system using optical fiber spectrometer was designed for on-line parameters measurements of flame in engine. The wavelength response of charge-coupled device (CCD) was calibrated by the blackbody furnace. Then, the radiation spectroscopy range of 200-1100 nm wavelength of high temperature flame in rocket based combined cycle (RBCC) engine ground testing was obtained by using this system, and the temperature and radiance of flame were determined with Planck radiation law and the least square method. It can provide important reference for combustion diagnostics and optimization of engine.

AB - For the non-intrusive, on-line and in-situ measurement of high-temperature combustion flame in engine, the method based on radiation spectroscopy (RS) was presented. The system using optical fiber spectrometer was designed for on-line parameters measurements of flame in engine. The wavelength response of charge-coupled device (CCD) was calibrated by the blackbody furnace. Then, the radiation spectroscopy range of 200-1100 nm wavelength of high temperature flame in rocket based combined cycle (RBCC) engine ground testing was obtained by using this system, and the temperature and radiance of flame were determined with Planck radiation law and the least square method. It can provide important reference for combustion diagnostics and optimization of engine.

KW - Combustion diagnostics of engine

KW - Combustion flam parameters

KW - On-line measurement

KW - Radiation spectroscopy

KW - Thermometry

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DO - 10.13224/j.cnki.jasp.2015.12.013

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

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ER -

On-line parameters measurement of combustion flame in engineusing radiation spectroscopy

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Keywords

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