The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines

In order to solve the problem of combustion cycle variation in two-stroke aviation kerosene piston engines under idle conditions, experiments were conducted to investigate the influence of intake air temperature on combustion cycle variation and output work. The coefficient of variation of the indic...

Full description

Saved in:
Bibliographic Details
Main Authors: Jian Wang, Zhiqiang Han, Yusheng Liang, Zinong Zuo, Zhongxin Fang, Wei Tian, Jia Fang, Xueshun Wu
Format: Article
Language:English
Published: MDPI AG 2025-01-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/18/2/331
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1832588583593050112
author Jian Wang
Zhiqiang Han
Yusheng Liang
Zinong Zuo
Zhongxin Fang
Wei Tian
Jia Fang
Xueshun Wu
author_facet Jian Wang
Zhiqiang Han
Yusheng Liang
Zinong Zuo
Zhongxin Fang
Wei Tian
Jia Fang
Xueshun Wu
author_sort Jian Wang
collection DOAJ
description In order to solve the problem of combustion cycle variation in two-stroke aviation kerosene piston engines under idle conditions, experiments were conducted to investigate the influence of intake air temperature on combustion cycle variation and output work. The coefficient of variation of the indicated mean effective pressure was used to characterize combustion cycle variation. The results showed that there is a negative correlation between the engine combustion work and the combustion cycle variation. In the lower range, increasing the intake air temperature has a greater effect on reducing the combustion cycle variation, while in the higher range, the combustion cycle variation has a greater impact on the output work. At the same time, the influence of intake air temperature on the fuel evaporation rate is related to engine speed, and this relationship weakens as the engine speed increases. In the range of 0~40 °C, the higher the intake air temperature, the larger the stable combustion range.
format Article
id doaj-art-d3e7caec7b1a41938762b31c580df33e
institution Kabale University
issn 1996-1073
language English
publishDate 2025-01-01
publisher MDPI AG
record_format Article
series Energies
spelling doaj-art-d3e7caec7b1a41938762b31c580df33e2025-01-24T13:31:04ZengMDPI AGEnergies1996-10732025-01-0118233110.3390/en18020331The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston EnginesJian Wang0Zhiqiang Han1Yusheng Liang2Zinong Zuo3Zhongxin Fang4Wei Tian5Jia Fang6Xueshun Wu7School of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaSchool of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaSchool of Aeronautics and Astronautice, Xihua University, Chengdu 610039, ChinaSchool of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaSchool of Automobile and Transportation, Xihua University, Chengdu 610039, ChinaSchool of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaSchool of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaSchool of Energy and Power Engineering, Xihua University, Chengdu 610039, ChinaIn order to solve the problem of combustion cycle variation in two-stroke aviation kerosene piston engines under idle conditions, experiments were conducted to investigate the influence of intake air temperature on combustion cycle variation and output work. The coefficient of variation of the indicated mean effective pressure was used to characterize combustion cycle variation. The results showed that there is a negative correlation between the engine combustion work and the combustion cycle variation. In the lower range, increasing the intake air temperature has a greater effect on reducing the combustion cycle variation, while in the higher range, the combustion cycle variation has a greater impact on the output work. At the same time, the influence of intake air temperature on the fuel evaporation rate is related to engine speed, and this relationship weakens as the engine speed increases. In the range of 0~40 °C, the higher the intake air temperature, the larger the stable combustion range.https://www.mdpi.com/1996-1073/18/2/331aviation keroseneidle speedintake temperaturetwo-stroke enginecombustion cyclic variations
spellingShingle Jian Wang
Zhiqiang Han
Yusheng Liang
Zinong Zuo
Zhongxin Fang
Wei Tian
Jia Fang
Xueshun Wu
The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
Energies
aviation kerosene
idle speed
intake temperature
two-stroke engine
combustion cyclic variations
title The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
title_full The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
title_fullStr The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
title_full_unstemmed The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
title_short The Effect of Intake Temperature on the Idle Combustion Cycle Variation of Two-Stroke Aviation Kerosene Piston Engines
title_sort effect of intake temperature on the idle combustion cycle variation of two stroke aviation kerosene piston engines
topic aviation kerosene
idle speed
intake temperature
two-stroke engine
combustion cyclic variations
url https://www.mdpi.com/1996-1073/18/2/331
work_keys_str_mv AT jianwang theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zhiqianghan theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT yushengliang theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zinongzuo theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zhongxinfang theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT weitian theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT jiafang theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT xueshunwu theeffectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT jianwang effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zhiqianghan effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT yushengliang effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zinongzuo effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT zhongxinfang effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT weitian effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT jiafang effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines
AT xueshunwu effectofintaketemperatureontheidlecombustioncyclevariationoftwostrokeaviationkerosenepistonengines