Temperature field reconstruction method for aero engine exhaust using the colored background oriented Schlieren technology

doi:https://doi.org/10.1007/s11801-022-1139-1

Home > Archive>Volume 18, Issue 4, 2022 >243-250. DOI:https://doi.org/10.1007/s11801-022-1139-1

Temperature field reconstruction method for aero engine exhaust using the colored background oriented Schlieren technology
DOI:
                        https://doi.org/10.1007/s11801-022-1139-1
                    
CSTR:
                        [cstr]
                    
Author:
                        SONG FengchengSONG Fengcheng
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site
WU JunWU Jun
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site
ZHU YuhengZHU Yuheng
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site
XU HaitaoXU Haitao
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site
LI YanlingLI Yanling
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site
YU ZhijingYU Zhijing
1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Find this author on All Journals
Find this author on BaiDu
Search for this author on this site

                    
Affiliation:1. College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China ;2. State Key Laboratory of Precision Measuring Technology and Instruments, Tianjin University, Tianjin 300072, China;3. Xinjin Flight Training College, Civil Aviation Flight University of China, Guanghan 618300, China;4. College of Electronic Information and Automation, Civil Aviation University of China, Tianjin 300300, China
Clc Number:
Fund Project:

Article

Figures

Metrics

Reference

Cited by

Materials

Comments

Abstract:

The detection of the jet temperature field in an aircraft engine tail is an effective way to reflect the running state of an engine. To solve the complicated detection process of current laser diagnostic methods, the colored background oriented Schlieren (CBOS) method was proposed to obtain a tail jet temperature field. First, the background Schlieren image with three-color points was collected for the exhaust gas temperature (EGT) field of the engine. Then the refractive index field of the engine exhaust was obtained according to the proposed CBOS method. Finally, the three-dimensional EGT field was reconstructed through the refractive index field. The simulation and the experimental results show the feasibi-lity and effectiveness of the proposed method.

Get Citation

SONG Fengcheng, WU Jun, ZHU Yuheng, XU Haitao, LI Yanling, YU Zhijing. Temperature field reconstruction method for aero engine exhaust using the colored background oriented Schlieren technology[J]. Optoelectronics Letters,2022,18(4):243-250

Copy

Article Metrics

Abstract:
PDF:
HTML:
Cited by:

History

Received:
Revised:
Adopted:
Online: April 27,2022
Published:

Home

About us

Authors

Editors

News

Contents

Contact us

Get Citation

Share

Article Metrics

History

Article QR Code