Details
Original language | English |
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Title of host publication | Proceedings of Global Power & Propulsion Society |
Number of pages | 12 |
Publication status | Published - 19 Oct 2023 |
Abstract
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Proceedings of Global Power & Propulsion Society. 2023.
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Axial Compressor as eBooster for charging an Ultra-Lean-Burn Hydrogen Combustion Engine
AU - Schulz, Yannik
AU - Seume, Joerg R.
AU - Sagan, Lukas
AU - Eilts, Peter
PY - 2023/10/19
Y1 - 2023/10/19
N2 - Hydrogen as a fuel in spark-ignition combustion engines provides an opportunity for using an ultra-lean-burn combustion strategy. This combustion concept has the advantage of ensuring a high thermal efficiency as well as ultra-low NOx emissions at the same time. This makes it an interesting concept, especially in the field of commercial vehicles. Providing these high pressure ratios while guaranteeing an acceptable boost pressure is challenging for charging systems. In order to face these requirements, an axial compressor eBooster stage is developed. The eBooster concept extends the operating range of a single-stage turbocharger. Otherwise, a complex and cost intensive two-stage configuration would be needed. The compressor is designed to operate for mass flow rates of 0.4 to 0.8 kg/s and total pressure ratios of up to 1.72. When operating the eBooster stage, the centrifugal compressor performance map is shifted towards higher mass flow rates by means of pre-compression. The compressor developed shows a peak isentropic efficiency of 82.8 % with high efficiencies (>78 %) for the whole operating range.
AB - Hydrogen as a fuel in spark-ignition combustion engines provides an opportunity for using an ultra-lean-burn combustion strategy. This combustion concept has the advantage of ensuring a high thermal efficiency as well as ultra-low NOx emissions at the same time. This makes it an interesting concept, especially in the field of commercial vehicles. Providing these high pressure ratios while guaranteeing an acceptable boost pressure is challenging for charging systems. In order to face these requirements, an axial compressor eBooster stage is developed. The eBooster concept extends the operating range of a single-stage turbocharger. Otherwise, a complex and cost intensive two-stage configuration would be needed. The compressor is designed to operate for mass flow rates of 0.4 to 0.8 kg/s and total pressure ratios of up to 1.72. When operating the eBooster stage, the centrifugal compressor performance map is shifted towards higher mass flow rates by means of pre-compression. The compressor developed shows a peak isentropic efficiency of 82.8 % with high efficiencies (>78 %) for the whole operating range.
U2 - 10.33737/gpps23-tc-056
DO - 10.33737/gpps23-tc-056
M3 - Conference contribution
BT - Proceedings of Global Power & Propulsion Society
ER -