By Hung Nguyen-Schäfer

ISBN-10: 3642350690

ISBN-13: 9783642350696

ISBN-10: 3642350704

ISBN-13: 9783642350702

Aero and Vibroacoustics of automobile Turbochargers is a subject regarding features from the operating fields of thermodynamics of turbomachinery, aerodynamics, rotordynamics, and noise propagation computation.

In this greatly interdisciplinary topic, thermodynamicsof turbomachinery is used to layout the turbocharger and to figure out its working stipulations. Aerodynamics is required to review the compressor stream dynamics and stream instabilities of rotating stall and surge, that can produce growling and whining-type noises. Rotordynamics is important to review rotor unbalance and self-excited oil-whirl instabilities, which result in whistling and incessant tone-type noises in rotating floating oil-film sort bearings. For the distinctive case of turbochargers utilizing ball bearings, a few high-order harmonic and put on noises additionally appear within the rotor working diversity. finally, noise propagation computation, based on Lighthill’s analogy, is needed to enquire airborne noises produced by way of turbochargers in passenger vehicles.

The content material of this ebook is meant for complicated undergraduates, graduates in mechanical engineering, study scientists and training engineers who are looking to larger comprehend the interactions among those operating fields and the ensuing influence at the attention-grabbing subject of Aero and Vibroacoustics of car Turbochargers.

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Additional info for Aero and Vibroacoustics of Automotive Turbochargers

Example text

M C ¼ m_ C ðr2 cu;2 À r1 cu;1 Þ ð4:1aÞ where m_ C is the compressor mass flow rate; r1 and r2 are the inlet (inducer) and outlet (exducer) radii of CW; cu,1 and cu,2 are the tangential (or whirl) velocities at the inlet and outlet. The compressor mass flow rate is resulted from the air density q, meridional velocity component cm, and compressor cross-sectional area AC. m_ C ¼ qcm AC ð4:1bÞ The compressor power is resulted from the compressor torque and angular rotor speed. PC ¼ M C x ¼ m_ C x ðr2 cu;2 À r1 cu;1 Þ ¼ m_ C ðu2 cu;2 À u1 cu;1 Þ ð4:2aÞ within u1 and u2 are the circumferential velocities at the CW inlet and outlet.

At low rotor speeds from the idle condition (about 30 % of Nmax), the compressor pressure ratio increases with a relatively high pressure gradient in the full load curve to ensure a good transient response in low-end torque (LET). 5, and the engine achieves the maximum torque M1. The nominal power Pnom occurs just before the maximum operating rotor speed Nmax. The maximum rotor speed corresponding with u2,max = 560 m/s is reached in highland applications where the rotor speed increases by 8–10 % (highland speed reserve) above the nominal operating rotor speed.

The maximum rotor speed corresponding with u2,max = 560 m/s is reached in highland applications where the rotor speed increases by 8–10 % (highland speed reserve) above the nominal operating rotor speed. The compressor pressure ratio is formulated in a function of the corrected mass flow rate and turbocharger speed in the performance map.

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Aero and Vibroacoustics of Automotive Turbochargers by Hung Nguyen-Schäfer


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