The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 23, 2002

Filed:

Apr. 14, 2000
Applicant:
Inventors:

Eugene E. Williams, Frankfort, IN (US);

Jonathan B. Stagg, Greencastle, IN (US);

Assignee:

BorgWarner Inc., Troy, MI (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 2/900 ;
U.S. Cl.
CPC ...
F04D 2/900 ;
Abstract

An engine cooling system include a ring-type cooling fan ( ) that includes a central hub ( ), a plurality of blades ( ) projecting radially from the hub ( ) and an outer circumferential ring ( ) connected to the blade tips ( ). In one aspect of the invention, the outer ring ( ) includes a flared rim ( ) at the outlet side ( ) of the fan ( ) that improves the stackability and stability of multiple fans. In another aspect of the invention, each of the blades ( ) includes a support vane ( ) defined on the rear face ( ) of the blade ( ). The support vane ( ) is curved to follow the curvature of the airflow (F) across the back ( ) of the fan blades ( ). Each support vane ( ) originates at the blade root ( ) and terminates at the trailing edge ( ) of the blade in the first half of the blade length. The support vanes ( ) provide first mode stiffness for the fan ( ). In certain embodiments, a support ring ( ) is defined at the central hub ( ) inboard of the support vanes ( ). A vane support superstructure ( ) is configured between the support vanes ( ) and the support ring ( ) to react the aerodynamic loads experienced by the support vanes ( ). A further support superstructure ( ) can be configured between the support ring ( ) and the central hub ( ). Other features of the invention provide a stress-reducing blend region ( ) between the blade tips ( ) and the flared rim ( ) of the outer ring ( ), and an improved blade geometry.


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