Study on Operating Temperature Prediction Model of Aero High-speed Gears

With the continuous improvement of the operating temperature of aero transmission under the high-speed and high load, gear scuffing failure has become a key factor restricting the performance of aircrafts. To efficiently predict the operating temperature of aero gears, a sequential coupling numerica...

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Main Authors: Chen Yuling, Zhu Jiazan, Chen Taimin, Zhu Caichao, Wei Peitang, Xu Yongqiang
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Transmission 2024-02-01
Series:Jixie chuandong
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Online Access:http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.02.001
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author Chen Yuling
Zhu Jiazan
Chen Taimin
Zhu Caichao
Wei Peitang
Xu Yongqiang
author_facet Chen Yuling
Zhu Jiazan
Chen Taimin
Zhu Caichao
Wei Peitang
Xu Yongqiang
author_sort Chen Yuling
collection DOAJ
description With the continuous improvement of the operating temperature of aero transmission under the high-speed and high load, gear scuffing failure has become a key factor restricting the performance of aircrafts. To efficiently predict the operating temperature of aero gears, a sequential coupling numerical analysis method of the gear temperature is proposed for an aero engine gear, which simulates the bulk temperature and flash temperature under different working conditions, considering factors such as solid-liquid-gas multi-state flow heat exchange and heat dissipation coefficients of different tooth surfaces. The simulated gear contact temperature is compared with calculation results of ISO/TS 6336-20 and shows consistency, the largest deviation between which under different working conditions is controlled within 10%. When the input speed is 22 400 r/min and the torque is 119.4 N<inline-formula><alternatives><math xmlns:mml="http://www.w3.org/1998/Math/MathML" id="M1"><mo>∙</mo></math><graphic specific-use="big" xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="alternativeImage/EF92CD4E-DA0D-4193-9CEA-33176076FCE8-M001.jpg"><?fx-imagestate width="1.86266661" height="2.62466669"?></graphic><graphic specific-use="small" xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="alternativeImage/EF92CD4E-DA0D-4193-9CEA-33176076FCE8-M001c.jpg"><?fx-imagestate width="1.86266661" height="2.62466669"?></graphic></alternatives></inline-formula>m, the split large gear contact temperature reaches 242.6 ℃, the scuffing safety factor is 1.22, and there is a risk of scuffing failure. The proposed simulation analysis method can effectively predict the operating temperature of aero high-speed gears, and provide an efficient and reliable method for assessing the risk of aero gear scuffing failure.
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institution Kabale University
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language zho
publishDate 2024-02-01
publisher Editorial Office of Journal of Mechanical Transmission
record_format Article
series Jixie chuandong
spelling doaj-art-d3c1afddede847ccb8e29b13d998b10d2025-01-10T14:59:54ZzhoEditorial Office of Journal of Mechanical TransmissionJixie chuandong1004-25392024-02-01481949593849Study on Operating Temperature Prediction Model of Aero High-speed GearsChen YulingZhu JiazanChen TaiminZhu CaichaoWei PeitangXu YongqiangWith the continuous improvement of the operating temperature of aero transmission under the high-speed and high load, gear scuffing failure has become a key factor restricting the performance of aircrafts. To efficiently predict the operating temperature of aero gears, a sequential coupling numerical analysis method of the gear temperature is proposed for an aero engine gear, which simulates the bulk temperature and flash temperature under different working conditions, considering factors such as solid-liquid-gas multi-state flow heat exchange and heat dissipation coefficients of different tooth surfaces. The simulated gear contact temperature is compared with calculation results of ISO/TS 6336-20 and shows consistency, the largest deviation between which under different working conditions is controlled within 10%. When the input speed is 22 400 r/min and the torque is 119.4 N<inline-formula><alternatives><math xmlns:mml="http://www.w3.org/1998/Math/MathML" id="M1"><mo>∙</mo></math><graphic specific-use="big" xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="alternativeImage/EF92CD4E-DA0D-4193-9CEA-33176076FCE8-M001.jpg"><?fx-imagestate width="1.86266661" height="2.62466669"?></graphic><graphic specific-use="small" xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="alternativeImage/EF92CD4E-DA0D-4193-9CEA-33176076FCE8-M001c.jpg"><?fx-imagestate width="1.86266661" height="2.62466669"?></graphic></alternatives></inline-formula>m, the split large gear contact temperature reaches 242.6 ℃, the scuffing safety factor is 1.22, and there is a risk of scuffing failure. The proposed simulation analysis method can effectively predict the operating temperature of aero high-speed gears, and provide an efficient and reliable method for assessing the risk of aero gear scuffing failure.http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.02.001Aero gearGear scuffingTemperature simulationBulk temperatureContact temperature
spellingShingle Chen Yuling
Zhu Jiazan
Chen Taimin
Zhu Caichao
Wei Peitang
Xu Yongqiang
Study on Operating Temperature Prediction Model of Aero High-speed Gears
Jixie chuandong
Aero gear
Gear scuffing
Temperature simulation
Bulk temperature
Contact temperature
title Study on Operating Temperature Prediction Model of Aero High-speed Gears
title_full Study on Operating Temperature Prediction Model of Aero High-speed Gears
title_fullStr Study on Operating Temperature Prediction Model of Aero High-speed Gears
title_full_unstemmed Study on Operating Temperature Prediction Model of Aero High-speed Gears
title_short Study on Operating Temperature Prediction Model of Aero High-speed Gears
title_sort study on operating temperature prediction model of aero high speed gears
topic Aero gear
Gear scuffing
Temperature simulation
Bulk temperature
Contact temperature
url http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2024.02.001
work_keys_str_mv AT chenyuling studyonoperatingtemperaturepredictionmodelofaerohighspeedgears
AT zhujiazan studyonoperatingtemperaturepredictionmodelofaerohighspeedgears
AT chentaimin studyonoperatingtemperaturepredictionmodelofaerohighspeedgears
AT zhucaichao studyonoperatingtemperaturepredictionmodelofaerohighspeedgears
AT weipeitang studyonoperatingtemperaturepredictionmodelofaerohighspeedgears
AT xuyongqiang studyonoperatingtemperaturepredictionmodelofaerohighspeedgears