Abstract: An axial-flow fan structure is disclosed, having a localized area expansion between the rotor (i.e. front rotating impeller) and stator blades (i.e. rear stationary or fixed blades, sometimes called de-swirl vanes). The area expansion is provided by utilizing an impeller having a (slightly) falling tip contour (FTC).
Type:
Grant
Filed:
June 22, 2011
Date of Patent:
August 26, 2014
Assignee:
Minebea Co., Ltd. (Minebea)
Inventors:
Hirofuni Shoji, Yousef Jarrah, Kevin Wackerly
Abstract: An axial-flow fan structure is disclosed, having a localized area expansion between the rotor (i.e. front rotating impeller) and stator blades (i.e. rear stationary or fixed blades, sometimes called de-swirl vanes). The area expansion is provided by utilizing an impeller having a (slightly) falling tip contour (FTC).
Type:
Application
Filed:
June 22, 2011
Publication date:
February 9, 2012
Applicant:
MINEBEA CO., LTD. (MINEBEA)
Inventors:
Hirofumi Shoji, Yousef Jarrah, Kevin Wackerly