An approach based on mean line assumption for preliminary design of turbochargers' rotors

Bourabia, Lakhdar; Cerdoun, Mahfoudh; Khalfallah, Smail; Chettibi, Taha

doi:10.1504/ijde.2018.100549

Cited by 1 publication

(2 citation statements)

References 0 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Limited works have been found in open literature that treated a complete TC design, 46,47 due to the complex balancing between the TC’s component. Therefore, a 1D aerodynamic in-house code is implemented in the actual work to generate easily and quickly geometries of TC’s rotors, from which further analysis can be proceeded.…”

Section: Methodsmentioning

confidence: 99%

“…Contrarily to traditional methods that balance between the CC and RIT using only mass flow and velocity relations, hence, the developed code uses four balance equations to insure a perfect matching between the TC's components applying equations ( 26)- (29). Meanwhile, for more details about the CC's impeller design, see Chettibi et al 46 and Schiff. 50 Assumptions and design requirements used to start the TC design process are summarized in Table 3.…”

Section: Turbocharger Preliminary Designmentioning

confidence: 99%

See 1 more Smart Citation

An approach to select an appropriate turbocharger for matching with an internal combustion engine

Hameur

Sehili

Cerdoun

et al. 2022

International Journal of Engine Research

View full text Add to dashboard Cite

The present paper proposes a novel methodology of turbocharging automotive engines to reach targeted performance. The actual method is tested and validated against simulation test results of two turbocharged diesel engines; engine I, three cylinders, 1.5 L, and engine II, six cylinders, 5.9 L. The present procedure is subdivided into four key parts; namely, database construction, selection procedure, turbocharger preliminary design, and engine modeling. Based on geometric dimensions and aerodynamic parameters provided by the preliminary design procedure, 3D geometries of the turbine and compressor are generated for each studied engine. After integrating previous data into a constructed turbocharger database, two turbochargers are selected for the engine I, while only one turbocharger for the engine II. The findings show that, at the engine speed of 4000 rpm, engine I matched with the adequate turbocharger reached a target power about 2.7%, compared to the original turbocharger equipping engine I. Furthermore, engine II reached a rated power of 299.3 kW at 2500 rpm which is slightly under the original one by 2.64 kW. The superimposition of the engine operating area on compressor and turbine maps provided satisfactory results in terms of turbocharger-engine output performance, fuel consumption, secure functioning and engine thermal strength. Finally, the main advantage of the developed methodology consists of its ability to be applied at both earlier and last stages of the engine turbocharging process or to find new adequate turbochargers to replace the original one for economic, mechanical or for safety reasons.

show abstract

Section: Methodsmentioning

confidence: 99%

Section: Turbocharger Preliminary Designmentioning

confidence: 99%