Abstract
This paper describes performance enhancement of a regenerative blower used for a 20 kW fuel cell system. Two
design variables, bending angle of an impeller and blade thickness of an impeller tip, which are used to define an impeller shape,
are introduced to enhance the blower performance. Internal flow of the regenerative blower has been analyzed with threedimensional
Navier-Stokes equations to obtain the blower performance. General analysis code, CFX, is introduced in the
present work. SST turbulence model is employed to estimate the eddy viscosity. Throughout the numerical analysis, it is
found that the thickness of impeller tip is effective to increase the blower efficiency in the present blower. Pressure is
successfully increased up to 2.8% compared to the reference blower at the design flow condition. And efficiency is also enhanced
up to 2.98 % compared to the reference one. It is noted that low velocity region disturbs to make strong recirculation flow
inside the blade passages, thus increases local pressure loss. Detailed flow field inside the regenerative blower is also
analyzed and compared.
© 2014 Turbomachinery Society of Japan, Korean Fluid Machinery Association, Chinese Society of Engineering Thermophysics, IAHR