Abstract

The need for advanced combustion technologies for use in future highly efficient powertrains in the automotive sector is well understood. Pre-chamber combustors, a technology with numerous historic examples, are fast becoming a major area of research once again. Pre-chambers are proportionally small partially enclosed chambers where combustion of a small quantity of fuel and air initiates before transferring to the main cylinder and, in spark ignition applications, subsequently igniting the bulk of the fuel and air. Pre-chambers effectively cascade two combustion events in order to increase the ignition energy present in the main combustion event, thereby enabling stable combustion of difficult-to-ignite main chamber mixtures, such as those with high levels of dilution. A traditional weakness of the subset of pre-chamber concepts known as jet igniters is poor low load engine performance. Combustion stability challenges and insufficient spark retard authority under heavily throttled conditions have limited the prospects of commercial implementation of jet ignition in modern engines. This study seeks to evaluate the root cause of these limitations and propose practical solutions that leverage the inherent flexibility of auxiliary fueled (active) jet ignition. Results of these experiments demonstrate the ability of a jet ignition engine to achieve idle and catalyst heating performance consistent with that of modern SI engines, thereby reducing the barriers to commercial implementation.

Highlights

  • The need for advanced combustion technologies for use in future highly efficient powertrains in the automotive sector is well understood

  • As the engine is enleaned beyond λ = 1.3, the pulsewidth of the pre-chamber Direct injection (DI) is increased to maintain the coefficient of variation (COV) of gross indicated mean effective pressure (IMEPg) less than 3%

  • A traditional weakness of pre-chamber concepts, jet igniters, is load engine performance. This is manifested as poor combustion stability under heavily throttled conditions and lack of adequate spark retard

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Summary

MAHLE JET IGNITION COMBUSTION SYSTEM

MAHLE Powertrain has been developing a pre-chamber combustor concept known as MAHLE Jet Ignition® (MJI) since 2009 through the research of Attard, et al [11,13,16] and this author [1,2,17,18]. MJI incorporates the characteristics of many jet ignition concepts researched since the early 1990s, namely a small volume pre-chamber (42% [1], representing an increase of approximately 15% above the highest reported comparable production SI engine at the time, and 10% above the highest reported production-intent SI engine at the time of this writing

APPLICABILITY ACROSS ENGINE MAP
EXPERIMENTAL APPARATUS
METHODOLOGY
CSSR Operation
CONCLUSION
Findings
AUTHOR INFORMATION
Full Text
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