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Open Access

Development of 2C-Scheimpflug planar laser-induced incandescence system for soot concentration measurement at exhaust of aero-engine model combustor

Sijie YANaPengji DINGa( )Linsen WANGb,cJie LIdChaozong WANGb,cQuan ZHOUb,cJinhe MUb,cWenyan SONGdZhenyu XUeBo YANb,cShuang CHENb,c( )
School of Nuclear Science and Technology, Lanzhou University, Lanzhou 730000, China
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China
Facility Design and Instrumentation Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
School of Power Energy, Northwestern Polytechnical University, Xi’an 710129, China
Anhui Institute of Optics and Fine Mechanics, Chinese Academy of Sciences, Hefei 230031, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Precise and quantitative measurement of soot particle emission plays an essential role in accurately assessing the combustion performance of aero-engine combustors and infrared signature levels in aircraft exhausts. Among various intrusive or non-intrusive approaches for soot diagnostics, Laser-Induced Incandescence (LII) technique has been increasingly applied for soot concentration measurement in various combustion environments such as laminar flames and internal combustion engines due to its high spatial resolution and sensitivity. As for LII measurement in aero-engine combustors, however, it normally suffers from very limited optical accesses and often faces mandatory requirements of oblique imaging from a small backward angle. In this work, we demonstrate a Two-Color (2C) LII system that simultaneously captures LII signal images at two distinct wavelengths using a Scheimpflug imaging configuration. A projective transformation algorithm and image overlapping procedures were employed to spatially correct the raw Scheimpflug LII images. Performance validation of the developed 2C-Scheimpflug LII system was first conducted under specified conditions in a laminar C2H4/air McKenna flame. The obtained Soot Volume Fraction (SVF) level and its spatial distribution are in consistent with previous studies under identical flame conditions reported by other research groups. Finally, as a demonstration of engineering benchmark application, we applied the developed 2C-Scheimpflug LII system to measure SVF distribution in the cross-section plane perpendicular to the direction of flame propagation at the exhaust of a single-sector dual-swirl aero-engine model combustor. Transient soot production events were observed and characteristics of the SVF distribution were investigated. These experimental results suggest the feasibility of the 2C-Scheimpflug LII technique developed in this work for precise and quantitative measurements of soot concentration in practical environments.

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Chinese Journal of Aeronautics

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Cite this article:
YAN S, DING P, WANG L, et al. Development of 2C-Scheimpflug planar laser-induced incandescence system for soot concentration measurement at exhaust of aero-engine model combustor. Chinese Journal of Aeronautics, 2025, 38(12). https://doi.org/10.1016/j.cja.2025.103622

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Received: 15 October 2024
Revised: 05 November 2024
Accepted: 25 November 2024
Published: 10 June 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).