Cooling system for internal combustion engines

• US 4,357,914 A
• Filed: 11/14/1979
• Issued: 11/09/1982
• Est. Priority Date: 11/16/1978
• Status: Expired due to Term

• Current Assignee: Suddeutsche Kuhlerfabrik Julius FR BEHR GmbH & Company KG
• Original Assignee: Suddeutsche Kuhlerfabrik Julius FR BEHR GmbH & Company KG
• Inventors: Hauser, Kurt
• Primary Examiner(s): Feinberg, Craig R.
• Assistant Examiner(s): Wolfe, W. R.
• Application Number:
  US06/094,154
• Time in Patent Office: 1,091 Days
• Field of Search: 123/41.49, 123/41.65, 123/41.66, 165/51, 165/125, 415/52, 415/53 R, 415/DIG. 1, 415/207, 416/186 R
• US Class Current: 123/41.49
• CPC Class Codes: F01P 5/06 Guiding or ducting air to, or from, ducted fans
• CPC Class Codes: F04D 17/16 for displacing without appreciable compression
• CPC Class Codes: F04D 29/282 the leading edge of each vane being substantially parallel to the rotation axis
• CPC Class Codes: F04D 29/4213 suction ports
• CPC Class Codes: F04D 29/4226 Fan casings
• CPC Class Codes: Y10S 415/914 Device to control boundary layer

Abstract

The air flow between the outlet of a centrifugal fan and the inlet of a surrounding annular radiator or heat exchanger for cooling an internal combustion engine is made uniform by rounding the peripheral edges of the fan wheel support discs so as to enlarge the effective outlet channel for the air and to guide the air in the direction of the lateral regions of the radiator. One or more baffle rings controls the short circuit flow to the inlet of the fan as well as the leakage flow at the shaft side of the fan.

Claims

1. In a cooling system for an internal combustion engine comprising a centrifugal fan and an annular radiator disposed thereabout whereby air is received axially by said centrifugal fan and blown generally radially therefrom to said annular radiator, said centrifugal fan comprising a pair of rotatable fan wheel discs which define the axial length of said centrifugal fan, and wherein the axial length of said annular radiator is approximately 2-3.3 times the axial length of said centrifugal fan, the improvement wherein

the peripheral edges of said fan wheel discs are rounded and curved away from one another to define an enlarged air exit orifice cross section, wherein said annular radiator is attached between a front wall and a rear wall, said cooling system further comprising an annular baffle ring attached to said front wall and extending axially toward, and terminating close to, the one of said pair of rotatable fan wheel discs which is closest thereto.

2. A cooling system according to claim 1, wherein at least a portion of the axial extent of said baffle ring has openings permitting air flow therethrough.

6. A cooling system according to claims 3 or 1, wherein said annular radiator is attached between a front wall and a rear wall, said cooling system further comprising an annular baffle ring attached to said rear wall and extending axially toward, and terminating close to, the one of said pair of rotatable fan wheel discs which is closest thereto.

3. In a cooling system for an internal combustion engine comprising a centrifugal fan and an annular radiator disposed thereabout whereby air is received axially by said centrifugal fan and blown generally radially therefrom to said annular radiator, said centrifugal fan comprising a pair of rotatable fan wheel discs which extend substantially at right angles to the axis of said fan and very close to the edges of said discs, and which discs define the axial length of said centrifugal fan, and wherein the axial length of said annular radiator is approximately 2-3.3 times the axial length of said centrifugal fan, the improvement wherein the peripheral edges of said fan wheel discs are rounded and curved away from one another to define an enlarged air exit orifice cross section, and said annular radiator is closely spaced from said peripheral edges of said discs so as to define only a small annular gap therebetween.

4. A cooling system according to claim 3, wherein a plurality of fan blades extend between said fan wheel discs, and said peripheral rounded curved edges begin to curve within the radial extent of the fan blades.

5. A cooling system according to claim 3, wherein the radius of curvature of each said curved edge of each said fan wheel disc is less than the axial length of said centrifugal fan.