Joseph K. Ausserer, M. Polanka, Paul J. Litke, K. D. Grinstead
{"title":"二冲程火花点火式发动机缸内压力测量方法的研究","authors":"Joseph K. Ausserer, M. Polanka, Paul J. Litke, K. D. Grinstead","doi":"10.4271/01-17-01-0004","DOIUrl":null,"url":null,"abstract":"This work describes an investigation of measurement techniques for the indicated\n mean effective pressure (IMEP) on a 55 cc single-cylinder, 4.4 kW, two-stroke,\n spark ignition (SI) engine intended for use on Group 1 and Group 2 remotely\n piloted aircraft (RPAs). Three different sensors were used: two piezoelectric\n pressure transducers (one flush mount and one measuring spark plug) for\n measuring in-cylinder pressure and one capacitive sensor for determining the top\n dead center (TDC) position of the piston. The effort consisted of three\n objectives: to investigate the merits of a flush mount pressure transducer\n compared to a pressure transducer integrated into the spark plug, to perform a\n parametric analysis to characterize the effect of the variability in the engine\n test bench controls on the IMEP, and to determine the thermodynamic loss angle\n for the engine. The results indicate that as a spark plug, the measuring spark\n plug is not statistically different from the stock spark plug at the 95%\n confidence level. The results indicate a statistically significant, 4%\n difference in the measured IMEP between the pressure transducer in the measuring\n spark plug and the flush mount transducer. The results also suggest a\n statistically significant difference in performance between the modified and\n unmodified engine heads, verifying the suppositions of other researchers who\n suggested that even a small modification to a combustion chamber this size could\n measurably affect the engine performance. While run-to-run variation resulted in\n a 2% to 5% variation in IMEP, a sensitivity analysis determined that 1% to 3% of\n that variation arose from variability in the control variables, while the\n remainder was caused by variation in other engine operating parameters. Between\n 1000 rpm and 2000 rpm, where the engine was typically motored to determine the\n TDC, the thermodynamic loss angle was 0.3 crank angle degrees (CAD) to 0.7 CAD,\n larger than loss angles observed in automotive-sized gasoline engines. The\n results indicate that using tabulated thermodynamic loss angles to set the TDC\n location of the engine using a mono-directional peak pressure method would lead\n to a −1% to −2.5% bias in the IMEP.","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":" ","pages":""},"PeriodicalIF":0.3000,"publicationDate":"2023-05-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Investigation of In-Cylinder Pressure Measurement Methods within a\\n Two-Stroke Spark Ignition Engine\",\"authors\":\"Joseph K. Ausserer, M. Polanka, Paul J. Litke, K. D. Grinstead\",\"doi\":\"10.4271/01-17-01-0004\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This work describes an investigation of measurement techniques for the indicated\\n mean effective pressure (IMEP) on a 55 cc single-cylinder, 4.4 kW, two-stroke,\\n spark ignition (SI) engine intended for use on Group 1 and Group 2 remotely\\n piloted aircraft (RPAs). Three different sensors were used: two piezoelectric\\n pressure transducers (one flush mount and one measuring spark plug) for\\n measuring in-cylinder pressure and one capacitive sensor for determining the top\\n dead center (TDC) position of the piston. The effort consisted of three\\n objectives: to investigate the merits of a flush mount pressure transducer\\n compared to a pressure transducer integrated into the spark plug, to perform a\\n parametric analysis to characterize the effect of the variability in the engine\\n test bench controls on the IMEP, and to determine the thermodynamic loss angle\\n for the engine. The results indicate that as a spark plug, the measuring spark\\n plug is not statistically different from the stock spark plug at the 95%\\n confidence level. The results indicate a statistically significant, 4%\\n difference in the measured IMEP between the pressure transducer in the measuring\\n spark plug and the flush mount transducer. The results also suggest a\\n statistically significant difference in performance between the modified and\\n unmodified engine heads, verifying the suppositions of other researchers who\\n suggested that even a small modification to a combustion chamber this size could\\n measurably affect the engine performance. While run-to-run variation resulted in\\n a 2% to 5% variation in IMEP, a sensitivity analysis determined that 1% to 3% of\\n that variation arose from variability in the control variables, while the\\n remainder was caused by variation in other engine operating parameters. Between\\n 1000 rpm and 2000 rpm, where the engine was typically motored to determine the\\n TDC, the thermodynamic loss angle was 0.3 crank angle degrees (CAD) to 0.7 CAD,\\n larger than loss angles observed in automotive-sized gasoline engines. The\\n results indicate that using tabulated thermodynamic loss angles to set the TDC\\n location of the engine using a mono-directional peak pressure method would lead\\n to a −1% to −2.5% bias in the IMEP.\",\"PeriodicalId\":44558,\"journal\":{\"name\":\"SAE International Journal of Aerospace\",\"volume\":\" \",\"pages\":\"\"},\"PeriodicalIF\":0.3000,\"publicationDate\":\"2023-05-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SAE International Journal of Aerospace\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.4271/01-17-01-0004\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SAE International Journal of Aerospace","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.4271/01-17-01-0004","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Investigation of In-Cylinder Pressure Measurement Methods within a
Two-Stroke Spark Ignition Engine
This work describes an investigation of measurement techniques for the indicated
mean effective pressure (IMEP) on a 55 cc single-cylinder, 4.4 kW, two-stroke,
spark ignition (SI) engine intended for use on Group 1 and Group 2 remotely
piloted aircraft (RPAs). Three different sensors were used: two piezoelectric
pressure transducers (one flush mount and one measuring spark plug) for
measuring in-cylinder pressure and one capacitive sensor for determining the top
dead center (TDC) position of the piston. The effort consisted of three
objectives: to investigate the merits of a flush mount pressure transducer
compared to a pressure transducer integrated into the spark plug, to perform a
parametric analysis to characterize the effect of the variability in the engine
test bench controls on the IMEP, and to determine the thermodynamic loss angle
for the engine. The results indicate that as a spark plug, the measuring spark
plug is not statistically different from the stock spark plug at the 95%
confidence level. The results indicate a statistically significant, 4%
difference in the measured IMEP between the pressure transducer in the measuring
spark plug and the flush mount transducer. The results also suggest a
statistically significant difference in performance between the modified and
unmodified engine heads, verifying the suppositions of other researchers who
suggested that even a small modification to a combustion chamber this size could
measurably affect the engine performance. While run-to-run variation resulted in
a 2% to 5% variation in IMEP, a sensitivity analysis determined that 1% to 3% of
that variation arose from variability in the control variables, while the
remainder was caused by variation in other engine operating parameters. Between
1000 rpm and 2000 rpm, where the engine was typically motored to determine the
TDC, the thermodynamic loss angle was 0.3 crank angle degrees (CAD) to 0.7 CAD,
larger than loss angles observed in automotive-sized gasoline engines. The
results indicate that using tabulated thermodynamic loss angles to set the TDC
location of the engine using a mono-directional peak pressure method would lead
to a −1% to −2.5% bias in the IMEP.