Experimental research has been carried out on a single cylinder naturally aspirated spark ignition engine which was modified to operate with coal-bed gas fuel to investigate the method of improving operation stability and lean burn limit. Varied fuel composition with methane concentration 30–100% and CO2 volumetric fraction 0–0.7 was employed to simulate coal-bed methane (CBM) and coal mined methane (CMM), respectively. Hydrogen was then employed to improve operational stability and lean burn limit. The results show that a stable operation range of the engine was obtained under most of the fuel compositions even if up to CO2 volumetric fraction = 0.6 was employed. Besides lean burn limit, the unstable operation with COVIMEP > 10% only appears at lean burn limit as well as CO2 volumetric fraction = 0.7 at each equivalence ratio. The lean burn limit of coal-bed gas has been significantly enlarged from the equivalence ratio equals to 0.6–0.4 by hydrogen addition. Stable operation with COVIMEP < 5% at the equivalence ratio equals to 0.4 has also been obtained at some high hydrogen concentration conditions. Hydrogen addition induced the reduction of both carbon monoxide (CO) and total hydrocarbon (THC) emissions at all equivalence ratio conditions, especially at the equivalence ratio equals to 0.4 and 0.6. CO2 addition improves NOx emission significantly; however, high CO2 volumetric fraction will lead to unstable operation, which results in deteriorated CO and THC emissions. Hydrogen addition has benefits of improving operation stability and enlarging lean burn limit of coal-bed gas engine, which has practical significance to improve the application of coal-bed gas engine technology.
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July 2017
Technical Briefs
Experimental Study of Operation Stability of a Spark Ignition Engine Fueled With Coal Bed Gas
Lei Chen,
Lei Chen
Liaoning Key Laboratory of Advanced Measurement
and Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China;
and Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China;
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Search for other works by this author on:
Peng Song,
Peng Song
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China;
Dalian University of Technology,
Dalian 116023, China;
College of Mechanical and Electronic Engineering,
Dalian Nationalities University,
Dalian 116600, China
e-mail: 20143625@qq.com
Dalian Nationalities University,
Dalian 116600, China
e-mail: 20143625@qq.com
Search for other works by this author on:
Wuqiang Long,
Wuqiang Long
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Search for other works by this author on:
Liyan Feng,
Liyan Feng
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
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Jing Zhang,
Jing Zhang
Liaoning Key Laboratory of Advanced Measurement and
Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China
Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China
Search for other works by this author on:
Yang Wang
Yang Wang
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Search for other works by this author on:
Lei Chen
Liaoning Key Laboratory of Advanced Measurement
and Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China;
and Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China;
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Peng Song
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China;
Dalian University of Technology,
Dalian 116023, China;
College of Mechanical and Electronic Engineering,
Dalian Nationalities University,
Dalian 116600, China
e-mail: 20143625@qq.com
Dalian Nationalities University,
Dalian 116600, China
e-mail: 20143625@qq.com
Wuqiang Long
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Liyan Feng
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
Jing Zhang
Liaoning Key Laboratory of Advanced Measurement and
Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China
Test Technology for Aviation Propulsion System,
Shenyang Aerospace University,
Shenyang 110136, China
Yang Wang
School of Energy and Power Engineering,
Dalian University of Technology,
Dalian 116023, China
Dalian University of Technology,
Dalian 116023, China
1Corresponding author.
Contributed by the Internal Combustion Engine Division of ASME for publication in the JOURNAL OF ENERGY RESOURCES TECHNOLOGY. Manuscript received May 6, 2016; final manuscript received August 26, 2016; published online April 17, 2017. Assoc. Editor: Avinash Kumar Agarwal.
J. Energy Resour. Technol. Jul 2017, 139(4): 044501 (5 pages)
Published Online: April 17, 2017
Article history
Received:
May 6, 2016
Revised:
August 26, 2016
Citation
Chen, L., Song, P., Long, W., Feng, L., Zhang, J., and Wang, Y. (April 17, 2017). "Experimental Study of Operation Stability of a Spark Ignition Engine Fueled With Coal Bed Gas." ASME. J. Energy Resour. Technol. July 2017; 139(4): 044501. https://doi.org/10.1115/1.4035427
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