Performance Characterization and Auto-Ignition Performance of a Rapid Compression Machine
TL;DR: In this article, a new type of hydraulic piston was used to address the problem in which the hydraulic buffer adversely affects the rapid compression process of a rapid compression machine (RCM) test bench.
read more
Abstract: A rapid compression machine (RCM) test bench is developed in this study. The performance characterization and auto-ignition performance tests are conducted at an initial temperature of 293 K, a compression ratio of 9.5 to 16.5, a compressed temperature of 650 K to 850 K, a driving gas pressure range of 0.25 MPa to 0.7 MPa, an initial pressure of 0.04 MPa to 0.09 MPa, and a nitrogen dilution ratio of 35% to 65%. A new type of hydraulic piston is used to address the problem in which the hydraulic buffer adversely affects the rapid compression process. Auto-ignition performance tests of the RCM are then performed using a DME–O2–N2 mixture. The two-stage ignition delay and negative temperature coefficient (NTC) behavior of the mixture are observed. The effects of driving gas pressure, compression ratio, initial pressure, and nitrogen dilution ratio on the two-stage ignition delay are investigated. Results show that both the first-stage and overall ignition delays tend to increase with increasing driving gas pressure. The driving gas pressure within a certain range does not significantly influence the compressed pressure. With increasing compression ratio, the first-stage ignition delay is shortened, whereas the second-stage ignition delay is extended. With increasing initial pressure, both the first-stage and second-stage ignition delays are shortened. The second-stage ignition delay is shortened to a greater extent than that of the first-stage. With increasing nitrogen dilution ratio, the first-stage ignition delay is shortened, whereas the second-stage is extended. Thus, overall ignition delay presents different trends under various compression ratios and compressed pressure conditions.
read more
Chat with Paper
AI Agents for this Paper
Find similar papers on Google Scholar, PubMed and Arxiv
Write a critical review of this paper
Analyze citations of this paper to find unaddressed research gaps
Citations
Advances in rapid compression machine studies of low- and intermediate-temperature autoignition phenomena
S. Scott Goldsborough,Simone Hochgreb,Guillaume Vanhove,Margaret S. Wooldridge,Henry J. Curran,Chih-Jen Sung +5 more
TL;DR: The U.S. Department of Energy will provide public access to these results of federally sponsored research in accordance with the DOE Public Access Plan as mentioned in this paper, which can be found at http://energy.gov/downloads/doe-public-access-plan.
227
Autoignition of DME/H2 mixtures in a rapid compression machine under low-to-medium temperature ranges
TL;DR: In this paper, the first-stage ignition delay of DME/H 2 mixtures is measured in a rapid compression machine at compressed temperatures ranging from 655 to 810 K and compressed pressures from 16.9 to 24.5 bar with an equivalence ratio range of 0.8-1.6.
21
Ignition properties of lean DME/H2 mixtures at low temperatures and elevated pressures
TL;DR: In this paper, the authors measured the ignition delay of lean dimethyl ether (DME)/hydrogen mixtures with hydrogen mole fraction ranging from 0 to 85% using a rapid compression machine with equivalence ratios from 0.3 to 0.5.
20
Study of the Ignition Characteristics of Light Fractions of Crude Oil and Their Surrogate Fuels under a Range of Low-to-Medium Temperatures
TL;DR: In this article, a gas chromatography-mass spectrometry instrument (GC-MS) was used to analyze the reaction kinetics of light fractions of crude oil in a rapid compression machine at compressed pressures of 20 bar and a compressed temperature range of 660-900 K.
13
Effects of Buffer Gas Composition on Autoignition of Dimethyl Ether
TL;DR: In this article, the effects of buffer gas composition on the first-stage and total ignition delay of DME autoignition were investigated using a rapid compression machine (RCM) at compressed pressure of 10 bar, equivalence ratio (φ) of 1 and compressed temperature from 670 K to 795 K.
10
References
Using rapid compression machines for chemical kinetics studies
Chih-Jen Sung,Henry J. Curran +1 more
TL;DR: In this article, the authors present a review of compression machine research with the support of the Combustion Energy Frontier Research Center (CEFRC) funded by the U.S. Department of Energy under Award Number E-SC0001198.
297
Aerodynamics inside a rapid compression machine
Gaurav Mittal,Chih-Jen Sung +1 more
TL;DR: In this article, the effect of reaction chamber configuration on the resulting aerodynamics and temperature field was investigated using a creviced piston and a flat piston under varying conditions, and it was shown that the flat piston design leads to significant mixing of the cold vortex with the hot core region, which causes alternate hot and cold regions inside the combustion chamber.
206
Dimethyl Ether Autoignition in a Rapid Compression Machine: Experiments and Chemical Kinetic Modeling
TL;DR: In this paper, the first-stage ignition delay is found to be insensitive to changes in changes in pressure and equivalence ratio, while the second stage ignition delay was not insensitive.
171
An aerosol rapid compression machine for studying energetic-nanoparticle-enhanced combustion of liquid fuels
Casey Allen,Gaurav Mittal,Chih-Jen Sung,Elisa Toulson,Tonghun Lee +4 more
- 01 Jan 2011
TL;DR: In this paper, a novel aerosol rapid compression machine (RCM) was proposed to study the impact of nanoparticles on reducing the ignition delay of liquid fuels, and a proof-of-concept demonstration was presented using ethanol and JP-8.
169
Demonstration of a Free-Piston Rapid Compression Facility for the Study of High Temperature Combustion Phenomena
TL;DR: A free-piston rapid-compression facility (RCF) has been developed at the University of Michigan (UM) for use in studying high-temperature combustion phenomena, including gas-phase combustion synthesis and homogeneous-chargecompression ignition systems as discussed by the authors.
95