Please use this identifier to cite or link to this item: https://bura.brunel.ac.uk/handle/2438/33723
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dc.contributor.authorZaman, Zayne-
dc.contributor.authorMohamed, Mohamed-
dc.contributor.authorWang, Xinyan-
dc.contributor.authorZhao, Hua-
dc.contributor.authorHarrington, Anthony-
dc.contributor.authorHall, Jonathan-
dc.date.accessioned2026-08-18T15:39:39Z-
dc.date.available2026-08-18T15:39:39Z-
dc.date.issued2026-08-13-
dc.identifier.citationZaman, Z. et al. (2027) 'Dynamic transient control of hydrogen direct-injection SI engines: effects of ramp duration on engine performance and abnormal combustion', Fuel, 429(Part D (February 2027)), 140829, pp. 1–13. doi: 10.1016/j.fuel.2026.140829.en_US
dc.identifier.issn0016-2361-
dc.identifier.urihttps://bura.brunel.ac.uk/handle/2438/33723-
dc.descriptionData availability: Data will be made available on request.en_US
dc.description.abstractHydrogen internal combustion engines offer a route to near-zero carbon on-road transport while preserving existing engine manufacturing and calibration know-how. Translating that potential into real-world driving, however, depends on transient control; steady-state maps alone cannot guarantee either safe operation or low NOx emissions during load steps. This paper reports a controlled transient sweep on a 0.4 L single-cylinder direct-injection spark-ignition hydrogen research engine. Five ramp durations (1.38, 1.08, 0.84, 0.48 and 0.24 s) were evaluated at a constant engine speed of 2,000 rpm with a target relative air–fuel ratio of 2.75 under closed-loop feedback control. The measurements track injection pulse width, spark timing, boost, lambda, IMEP, peak in-cylinder pressure and the maximum pressure rise rate (𝘙<sub><i>max</i></sub>) through each transient. As ramp duration is shortened, lambda excursions and air-path overshoot grow rapidly: at 0.24 s the in-cylinder pressure overshoot approaches the mechanical safety limit, IMEP overshoots the steady-state target by about 22 %, and 𝘙<sub><i>max</i></sub> exceeds the 600 kPa/°CA calibrated threshold. With a ramp of 0.48 the most hazardous 𝘙<sub><i>max</i></sub> peak at roughly 1,000 kPa/°CA is caused, demonstrating that fastest is not always most damaging. Only the 1.38 s baseline keeps all combustion-severity metrics inside their reliability envelope. A feed-forward fuelling term scaled by the rate of manifold pressure change <i>dP</i>/<i>dt</i> is proposed to close the transient lambda gap; with physical implementation and experimental validation proposed as a future optimisation step. The results identify pressure-gradient management as the binding constraint for transient calibration of lean DI hydrogen engines.en_US
dc.description.sponsorshipUKRI has funded this research, and MAHLE Powertrain provides the experimental power unit. Clean Air Power and Phinia provide the Hydrogen DI and PFI injectors.en_US
dc.format.extentpp. 1–13-
dc.format.mediumPrint-Electronic-
dc.languageEnglish-
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.rightsRe-use licence for this version: CC BY-
dc.rightsLicence for published version: CC BY-
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/-
dc.subject0306 Physical Chemistry (incl. Structural)en_US
dc.subject0904 Chemical Engineeringen_US
dc.subject0913 Mechanical Engineeringen_US
dc.subjectEnergyen_US
dc.titleDynamic transient control of hydrogen direct-injection SI engines: effects of ramp duration on engine performance and abnormal combustionen_US
dc.typeArticleen_US
dc.date.dateAccepted2026-07-28-
dc.identifier.doihttps://doi.org/10.1016/j.fuel.2026.140829-
dc.relation.isPartOfFuel-
pubs.issuePart D (February 2027)-
pubs.publication-statusPublished-
pubs.volume429-
dc.identifier.eissn1873-7153-
dc.rights.licensehttps://creativecommons.org/licenses/by/4.0/legalcode.en-
dcterms.dateAccepted2026-07-28-
dcterms.descriptionHighlights: • First systematic ramp-duration sweep (1.38 → 0.24 s) on a DI-SI hydrogen engine. • Counterintuitive result: 0.48 s ramp peaks at ∼1000 kPa/°CA — worse than 0.24 s. • Every ramp faster than 1.38 s breaches the 600 kPa/°CA structural design limit. • Lambda overshoot to λ≈3.2 then undershoot to λ≈2.1 pinpointed as the Rmax driver. • Novel H₂-specific feed-forward term (K_ff + σ_H₂·dP/dt) proposed to cap Rmax.en_US
dcterms.issued2026-08-13-
dc.date.updated2026-08-18T15:23:56Z-
dc.rights.holderCrown / The Authors-
dc.contributor.orcidZaman, Zayne [0009-0001-4439-8984]-
dc.contributor.orcidMohamed, Mohamed [0000-0003-4534-5099]-
dc.contributor.orcidWang, Xinyan [0000-0002-1988-3742]-
dc.contributor.orcidZhao, Hua [0000-0002-7876-804X]-
dc.identifier.number140829-
Appears in Collections:Department of Mechanical and Aerospace Engineering Research Papers

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