scholarly journals Dynamic Response in Transient Operation of a Variable Geometry Turbine Stage: Influence of the Aerodynamic Performance

2013 ◽  
Vol 2013 ◽  
pp. 1-11 ◽  
Author(s):  
Nicolas Binder ◽  
Jaime Garcia Benitez ◽  
Xavier Carbonneau
Keyword(s):  
Response Time ◽  
Transient Response ◽  
Aerodynamic Performance ◽  
Variable Geometry ◽  
Transient Phase ◽  
Theoretical Expectation ◽  
Turbine Stage ◽  
Experimental Campaign ◽  
Variable Geometry Turbine ◽  
Operating Points

The transient response of a radial turbine stage with a variable geometry system is evaluated. Mainly, the consequences of the variations of the aerodynamic performance of the stage on the response time are checked. A simple quasi-steady model is derived in order to formalize the expected dependences. Then an experimental campaign is conducted: a brutal step in the feeding conditions of the stage is imposed, and the response time in terms of rotational speed is measured. This has been reproduced on different declinations of the same stage, through the variation of the stator geometry, and correlated to the steady-state performance of the initial and final operating points of the transient phase. The matching between theoretical expectation and results is surprisingly good for some configurations, less for others. The most important factor identified is the mass-flow level during the transient phase. It increases the reactivity, even far above the theoretical expectation for some configurations. For those cases, it is demonstrated that the quasi-steady approach may not be sufficient to explain how the transient response is set.

Behavior of a Variable Geometry Turbine Wheel to High Cycle Fatigue

2020 ◽  
Author(s):  
Calogero Avola ◽  
Alberto Racca ◽  
Angelo Montanino ◽  
Carnell E. Williams ◽  
Alfonso Renella ◽  
...  
Keyword(s):  
High Cycle Fatigue ◽  
Combustion Engine ◽  
Turbine Blades ◽  
Variable Geometry ◽  
Cycle Fatigue ◽  
Turbine Stage ◽  
Turbine Wheel ◽  
Variable Geometry Turbine ◽  
Turbine Design ◽  
Mechanical Optimization

Abstract Maximization of the turbocharger efficiency is fundamental to the reduction of the internal combustion engine back-pressure. Specifically, in turbochargers with a variable geometry turbine (VGT), energy losses can be induced by the aerodynamic profile of both the nozzle vanes and the turbine blades. Although appropriate considerations on material limits and structural performance of the turbine wheel are monitored in the design and aero-mechanical optimization phases, in these stages, fatigue phenomena might be ignored. Fatigue occurrence in VGT wheels can be categorized into low and high cycle behaviors. The former would be induced by the change in turbine rotational speed in time, while the latter would be caused by the interaction between the aerodynamic excitation and blades resonating modes. In this paper, an optimized turbine stage, including unique nozzle vanes design and turbine blades profile, has been assessed for high cycle fatigue (HCF) behavior. To estimate the robustness of the turbine wheel under several powertrain operations, a procedure to evaluate HCF behavior has been developed. Specifically, the HCF procedure tries to identify the possible resonances between the turbine blades frequency of vibrations and the excitation order induced by the number of variable vanes. Moreover, the method evaluates the turbine design robustness by checking the stress levels in the component against the limits imposed by the Goodman law of the material selected for the turbine wheel. In conclusion, both the VGT design and the HCF approach are experimentally assessed.

A Physics-Based Control-Oriented Model for the Turbine Power of a Variable-Geometry Turbo-Charger

2016 ◽  
Author(s):  
Kang Song ◽  
Devesh Upadhyay ◽  
Tao Zeng ◽  
Harold Sun
Keyword(s):  
Dimensionless Parameter ◽  
Transmission Loss ◽  
Empirical Relationship ◽  
Variable Geometry ◽  
Turbine Stage ◽  
Turbo Charger ◽  
Variable Geometry Turbine ◽  
Polytropic Process ◽  
Nozzle Orientation ◽  
Bearing Friction

In this paper, we discuss the development of a control-oriented model for the power developed by a Variable Geometry Turbine (VGT). The turbine exit flow velocity, Cex, is obtained based on a polytropic process assumption for the full turbine stage. The rotor inlet velocity, Cin, is estimated, through an empirical relationship between Cex and Cin as a function of a dimensionless parameter ψ. The turbine power is developed based on Euler’s equations of Turbomachinery under the assumptions of zero exit swirl and alignment between the nozzle orientation and the Cin velocity vector. A power loss sub-model is also designed to account for the transmission loss associated with the power transfer between the turbine and compressor. The loss model is an empirical model and accounts for bearing friction and windage losses. Model validation results, for both steady state and transient operation, are shown.

Design and Analysis of a Novel Split Sliding Variable Nozzle for Turbocharger Turbine

2017 ◽  
Author(s):  
Leon Hu ◽  
Harold Sun ◽  
James Yi ◽  
Eric Curtis ◽  
Jizhong Zhang
Keyword(s):  
Suction Side ◽  
Nozzle Flow ◽  
Leakage Flow ◽  
Variable Geometry ◽  
Efficiency Improvement ◽  
Turbine Stage ◽  
Flow Passage ◽  
Flow Capacity ◽  
Variable Geometry Turbine ◽  
Stage Efficiency

Variable geometry turbine (VGT) has been widely applied in internal combustion engines to improve the engine transient response and torque at low speed. One of the most popular variable geometry turbine is the variable nozzle turbine (VNT), in which the nozzle vanes can be rotated along the pivoting axis and thus the flow passage through the nozzle can be adjusted to match with different engine operating conditions. One disadvantage of the VNT is the turbine efficiency degradation due to the leakage flow in the nozzle endwall clearance, which is needed to allow the nozzle vanes to rotate without sticking. Especially at small nozzle open condition, there is large loading on the nozzle and high pressure gradient between the nozzle pressure and suction side. Strong leakage flow exists inside the nozzle endwall clearance from pressure side to suction side, leading to large flow loss and turbine stage efficiency degradation. In the present paper, a novel split sliding variable nozzle turbine (SSVNT) has been proposed to reduce the nozzle leakage flow and to improve turbine stage efficiency. The idea is to divide the nozzle into two parts: one part is fixed and the other part can slide along the partition surface. The mechanism of nozzle flow passage variation in SSVNT is different from that of the traditional pivoting VNT. The sliding vane and the fixed vane together form an integrated vane. The flow of the turbine is determined by the passage of the integrated vanes. When moving the sliding vane to large radius position, the nozzle flow passage opens up and the turbine has high flow capacity. When moving the sliding vane towards small radius position, the nozzle flow passage closes down and the turbine has low flow capacity. As the fixed vane doesn’t need endwall clearance, there is no leakage flow inside the fixed vane and the total leakage flow through the integrated vane can be reduced. Based on calibrated numerical modeling, the analysis results showed that there is up to 12% turbine stage efficiency improvement with the SSVNT design at small nozzle open condition while maintaining the same flow capacity and efficiency at large nozzle open condition, compared to the conventional VNT. The mechanism of efficiency improvement in the SSVNT design has also been discussed.

scholarly journals Transient response of a large two-stroke marine diesel engine coupled to a selective catalytic reduction exhaust aftertreatment system

2019 ◽  
Author(s):  
Μιχαήλ Φωτεινός
Keyword(s):  
Diesel Engine ◽  
Selective Catalytic Reduction ◽  
Transient Response ◽  
Catalytic Reduction ◽  
Exhaust Aftertreatment ◽  
Marine Diesel Engine ◽  
Variable Geometry ◽  
Aftertreatment System ◽  
Marine Diesel ◽  
Variable Geometry Turbine

Οι μεγάλοι δίχρονοι ναυτικοί κινητήρες diesel χρησιμοποιούνται ως μέσο πρόωσης στην πλειονότητα των ποντοπόρων ναυτικών εφαρμογών. Με στόχο τη μείωση του περιβαλλοντικού αποτυπώματος του θαλάσσιου τομέα, ο Διεθνής Ναυτιλιακός Οργανισμός έχει θεσπίσει κανονισμούς που θέτουν αυστηρά όρια στις εκπεμπόμενες εκπομπές οξειδιών του αζώτου (ΝΟx) από ναυτικούς κινητήρες, γνωστούς και ως κανονισμούς ΙΜΟ Tier III. Η Επιλεκτική Καταλυτική Αναγωγή (Selective Catalytic Reduction, SCR) είναι μια τεχνολογία μετεπεξεργασίας καυσαερίων που επιτρέπει την συμμόρφωση με τα νέα πρότυπα εκπομπών NOx. Λόγω της απαίτησης υψηλών θερμοκρασιών για ομαλή λειτουργία του συστήματος SCR, σε ναυτικές εφαρμογές 2-Χ κινητήρων, το SCR τοποθετείται ανάντη του στροβίλου, δηλαδή μεταξύ του κινητήρα και του υπερπληρωτή (στην πλευρά υψηλής πίεσης του στροβίλου). Αυτό έχει ως αποτέλεσμα την διατάραξη της σύζευξης του κινητήρα και του υπερπληρωτή εισάγοντας προκλήσεις στην μεταβατική λειτουργία του κινητήρα. Λόγω της μεγάλης θερμικής αδράνειας του συστήματος SCR, ο υπερπληρωτής αποκρίνεται σε μία μεταβολή φορτίου του κινητήρα με μία σημαντική χρονική καθυστέρηση, η οποία σε χαμηλό φορτίο του κινητήρα μπορεί να οδηγήσει το σύστημα σε θερμική αστάθεια. Ερευνητές έχουν υπογραμμίσει την ευαισθησία του συστήματος και έχουν προτείνει περίπλοκες και κοστοβόρες λύσεις για να διασφαλίσουν την εύρωστη λειτουργία του, όπως το σύστημα στροβίλου μεταβλητής γεωμετρίας (Variable Geometry Turbine, VTG).Η διατριβή αυτή διερευνά τη μεταβατική απόκριση μεγάλου δίχρονου ναυτικού κινητήρα diesel, χωρίς μεταβλητότητα υπερπληρωτή, συνδεδεμένου με σύστημα απορρύπανσης καυσαερίων SCR. Σκοπός της εργασίας είναι η διερεύνηση της επίδρασης του συστήματος SCR υψηλής πίεσης στην μεταβατική απόκριση του κινητήρα με έμφαση στη λειτουργία σε χαμηλό φορτίο κινητήρα. Λόγω του υψηλού κόστους που εμπεριέχεται στα πειράματα με μεγάλους δίχρονους κινητήρες, η έρευνα διεξήχθη μέσω μοντελοποίησης και προσομοίωσης. Αναπτύχθηκαν μοντέλα μηδενικής διάστασης (zero dimensional models) για την προσομοίωση του κινητήρα πρόωσης και του συστήματος SCR. Το μοντέλο του κινητήρα αναπτύχθηκε χρησιμοποιώντας τον κώδικα προσομοίωσης κινητήρων του Εργαστηρίου Ναυτικής Μηχανολογίας MOTHER και επιβεβαιώθηκε με χρήση διαθέσιμων μετρήσεων από τις δοκιμές αγοράς του κινητήρα (shop trials). Επιπλέον, αναπτύχθηκε ένα μοντέλο για το σύστημα SCR ώστε να ληφθεί υπόψη η θερμοκρασιακή δυναμική του συστήματος. Το μοντέλο SCR επιβεβαιώθηκε μέσω σύγκρισης των αποτελεσμάτων του, με διαθέσιμες μετρήσεις από μία κλίνη δοκιμών ναυτικού κινητήρα με σύστημα SCR. Σε μεταβατικές καταστάσεις φόρτισης, το φορτίο που πρέπει να υπερνικήσει ο κινητήρας, δηλαδή η ροπή της έλικας, δεν είναι γνωστό εκ των προτέρων αλλά είναι προιόν περίπλοκων αλληλεπιδράσεων μεταξύ του κινητήρα, της έλικας και της γάστρας του πλοίου. Προκειμένου να επιτευχθή ακριβής πρόβλεψη του φορτίου του κινητήρα κατά τη διάρκεια των μεταβατικών φαινομένων, μοντέλα για την έλικα και τη γάστρα του πλοίου αναπτύχθηκαν και ενσωματώθηκαν στα μοντέλα γάστρας και έλικας. Το συζευγμένο μοντέλο του συστήματος πρόωσης επικυρώθηκε υπό συνθήκες μεταβατικής φόρτισης χρησιμοποιώντας διαθέσιμα μετρημένα δεδομένα επί πλοίου.Το συνολικό σύστημα προσομοιώθηκε υπό μεταβατική φόρτιση υπό καλές και δυσμενείς καιρικές συνθήκες. Τα αποτελέσματα έδειξαν ότι η μεταβατική απόκριση του κινητήρα επηρεάζεται πράγματι από την παρουσία του συστήματος SCR και το αποτέλεσμα είναι πιο έντονο στην περιοχή χαμηλότερου φορτίου κινητήρα. Ωστόσο, η θερμική αστάθεια του συστήματος μπορεί να αποφευχθεί και το σύστημα είναι σε θέση να λειτουργεί ακόμη και κατά τη λειτουργία σε πολύ χαμηλό φορτίο.

Mild Hybridization via Electrification of the Air System: Electrically Assisted and Variable Geometry Turbocharging Impact on an Off-Road Diesel Engine

2013 ◽  
Vol 136 (3) ◽  
Author(s):  
Nicola Terdich ◽  
Ricardo F. Martinez-Botas ◽  
Alessandro Romagnoli ◽  
Apostolos Pesiridis
Keyword(s):  
Energy Efficiency ◽  
Diesel Engine ◽  
Transient Response ◽  
Engine Speed ◽  
Variable Geometry ◽  
Flow Capacity ◽  
Electrically Assisted ◽  
Air System ◽  
Variable Geometry Turbine ◽  
Reduction Of Co2

Electric turbocharger assistance consists in incorporating an electric motor/generator within the turbocharger bearing housing to form a mild hybrid system without altering other mechanical parts of the engine. This makes it an ideal and economical short-to-medium-term solution for the reduction of CO2 emissions. The scope of the paper is to assess the improvements in engine energy efficiency and transient response correlated to the hybridization of the air system. To achieve this, an electrically assisted turbocharger with a variable geometry turbine has been compared to a similar, not hybridized system over step changes of engine load. The variable geometry turbine has been controlled to provide different levels of initial boost, including one optimized for efficiency, and to change its flow capacity during the transient. The engine modeled is a 7-liter, 6-cylinder diesel engine with a power output of over 200 kW and a sub-10-kW turbocharger electric assistance power. To improve the accuracy of the model, the turbocharger turbine has been experimentally characterized by means of a unique testing facility available at Imperial College and the data has been extrapolated by means of a turbine meanline model. Optimization of the engine boost to minimize pumping losses has shown a reduction in brake-specific fuel consumption up to 4.2%. By applying electric turbocharger assistance, it has been possible to recover the loss in engine transient response of the efficiency-optimized system, as it causes a reduction in engine speed drop of 71%–86% and of 79%–94% in engine speed recovery time. When electric assistance is present in the turbocharger, actuating the turbine vanes to assist transient response has not produced the desired result but only a decrement in energy efficiency. If the variable geometry turbine is opened during transients, an improvement in specific energy efficiency with negligible decrement in engine transient performances has been achieved.

Transient Response of Mixed Flow Variable Geometry Turbine for a Turbocharger

2015 ◽  
Author(s):  
Ramesh Kannan ◽  
Bhamidi Prasad ◽  
Sridhara Koppa
Keyword(s):  
Steady State ◽  
Transient Response ◽  
Velocity Ratio ◽  
Typical Result ◽  
Variable Geometry ◽  
Flow Variable ◽  
Data Logging ◽  
Mixed Flow ◽  
Response Behaviour ◽  
Variable Geometry Turbine

A specific design of mixed flow variable geometry turbine for an automotive sub 1.5 litre diesel engine turbocharger is proposed in this paper. An experimental set up is developed for measuring the steady state and transient response behaviour of the turbine at different nozzle vane opening positions. The rotor speed, pressure and temperature before and after the turbine are measured and recorded using high frequency data logging system. The steady state performance for mass flow, efficiency, velocity ratio, specific speed and the transient response behaviour of the mixed flow variable geometry turbine (MFVGT) are compared against the same parameters of a radial flow variable geometry turbine (RFVGT) of similar dimensions. Typical result indicates that the transient response of the MFVGT is faster by about 350 milliseconds than the radial at turbine inlet pressure of 0.2 bar (g).

Mild Hybridization via Electrification of the Air System: Electrically Assisted and Variable Geometry Turbocharging Impact on an Off-Road Diesel Engine

2013 ◽  
Author(s):  
Nicola Terdich ◽  
Ricardo F. Martinez-Botas ◽  
Alessandro Romagnoli ◽  
Apostolos Pesiridis
Keyword(s):  
Energy Efficiency ◽  
Diesel Engine ◽  
Transient Response ◽  
Engine Speed ◽  
Variable Geometry ◽  
Flow Capacity ◽  
Electrically Assisted ◽  
Air System ◽  
Variable Geometry Turbine ◽  
Reduction Of Co2

Electric turbocharger assistance consists in incorporating an electric motor/generator within the turbocharger bearing housing to form a mild-hybrid system, without altering other mechanical parts of the engine. This makes it an ideal and economical short to medium term solution for the reduction of CO2 emissions. The scope of the paper is to assess the improvements in engine energy efficiency and transient response correlated to the hybridization of the air system. To achieve this, an electrically assisted turbocharger with a variable geometry turbine has been compared to a similar, not hybridized, system over step changes of engine load. The variable geometry turbine has been controlled to provide different levels of initial boost, including one optimized for efficiency, and to change its flow capacity during the transient. The engine modeled is a 7-litre, 6-cylindres diesel engine with a power output of over 200 kW and a sub-10 kW turbocharger electric assistance power. To improve the accuracy of the model, the turbocharger turbine has been experimentally characterized by means of a unique testing facility available at Imperial College and the data has been extrapolated by means of a turbine meanline model. Optimization of the engine boost to minimize pumping losses has shown a reduction in brake specific fuel consumption up to 4.2%. By applying electric turbocharger assistance, it has been possible to recover the loss in engine transient response of the efficiency optimized system, as it causes a reduction in engine speed drop of 71% to 86% and of 79% to 94% in engine speed recovery time. When electric assistance is present in the turbocharger, actuating the turbine vanes to assist transient response has not produced the desired result but only a decrement in energy efficiency. If the variable geometry turbine is opened during transients, an improvement in specific energy efficiency with negligible decrement in engine transient performances has been achieved.

Variable Geometry and Waste-Gated Automotive Turbochargers: Measurements and Comparison of Turbine Performance

1992 ◽  
Vol 114 (3) ◽  
pp. 553-560 ◽  
Author(s):  
M. Capobianco ◽  
A. Gambarotta
Keyword(s):  
Experimental Investigation ◽  
Unsteady Flow ◽  
Transient Response ◽  
Test Facility ◽  
Variable Geometry ◽  
Flow Conditions ◽  
Turbine Performance ◽  
Variable Geometry Turbine ◽  
The University ◽  
And Control

In turbocharging automotive Diesel engines, an effective method to extend the turbine flow range and control the boost level is the use of a variable geometry turbine (VGT): This technique can be very helpful to improve the transient response of the engine and reduce exhaust emissions. In order to compare the performance of variable geometry and conventional waste-gated turbines, a thorough experimental investigation was developed on a test facility at the Department of Energetic Engineering of the University of Genoa (DINE). Two VG turbines were considered: a variable area turbine (VAT) and a variable nozzle turbine (VNT). The VG turbines were compared with a fixed geometry waste-gated turbine in both steady and unsteady flow conditions, referring to mass flow and efficiency characteristics.

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