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US4505641A Expired / Lapsed US ⏱️ 0.0 years remaining

Cooling fan for internal combustion engine

Assignee: Aisin Corp
•
Filing: 1983-12-22
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Granted: 1985-03-19
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Expires: 2003-12-22
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Abstract

Abstract A cooling fan to be located between an internal combustion engine and a radiator and rotatingly driven from a rotational shaft of the engine. The fan includes a plurality of blade elements radially projecting from a boss portion and a cylindrical ring formed at the outer ends of the blade elements coaxially with the boss portion. In each blade element, a base line, which is drawn through a base point located on a chord of blade between leading and trailing edges of the blade element at a distance of 40% from the leading edge in percentage to the length of the chord, describes a straight or moderately curved line from the inner to the outer end of the blade element, which is inclined rotationally forward of a radial line passing through the base point at the inner end of the blade element. This fan construction produces air flows containing axial and radial components of velocity to increase the air flows through the radiator irrespective of the existence of the internal combustion engine on the downstream side of the fan. Maximum air flow is obtained by projecting the trailing edge of the outer end of each blade element from the trailing edge of the above-mentioned ring by a length corresponding to 1/3 of the chord length of the outer blade end.

Inventors

  • 👤 Shunzo Tsuchikawa
  • 👤 Masaharu Hayashi
  • 👤 Takanobu Hori

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 14:28
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/26; F04D29/32; F04D29/325; F04D29/326; F01; F01P; F01P5/00; F01P5/02

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 293 words
A cooling fan located in association with a radiator of an internal combustion engine and having a plurality of radially extending blade elements around a boss portion for passing cooling air through said radiator, said fan comprising: a cylindrical ring member provided coaxially with the rotational axis of the fan and connecting outer end portions of said blade elements; and a base line connecting base points in airfoil sections of each of said blade elements on chords thereof located between a leading edge and a trailing edge of the airfoil section at a point 2/5ths the length of each chord from the leading edge so as to describe a moderately curved line from the inner to the outer end of said blade elements in a plane of rotation thereof and being inclined rotationally forward of a radial line passing through a base point at the inner end of said blade elements; said base line describing a moderately curved line from the inner to the outer end of said blade elements in a plane containing the rotational axis of said blade elements and inclined toward a suction side from said plane of rotation of said blade elements; a leading edge portion of the outer end of each of said blade elements being secured to said ring over a length corresponding to 1/3 to 3/4 of the width of said outer blade end as projected perpendicularly to the rotational axis of the fan, a remainder of the outer blade end forming a free end portion, and the trailing edges of said blade elements projecting on the discharge side of said ring and the end portion on the suction side of said ring diverging radially outward and then bending toward a discharge side of the fan.
Claim 2
Dependent Claim 293 words
A cooling fan located in association with a radiator of an internal combustion engine and having a plurality of radially extending blade elements around a boss portion for passing cooling air through said radiator, said fan comprising: a cylindrical ring member provided coaxially with the rotational axis of the fan and connecting outer end portions of said blade elements; and a base line connecting base points in airfoil sections of each of said blade elements on chords thereof located between a leading edge and a trailing edge of the airfoil section at a point 2/5ths the length of each chord from the leading edge so as to describe a moderately curved line from the inner to the outer end of said blade elements in a plane of rotation thereof and being inclined rotationally forward of a radial line passing through a base point at the inner end of said blade elements; said base line describing a moderately curved line from the inner to the outer end of said blade elements in a plane containing the rotational axis of said blade elements and inclined toward a suction side from said plane of rotation of said blade elements; a leading edge portion of the outer end of each of said blade elements being secured to said ring over a length corresponding to 1/3 to 3/4 of the width of said outer blade end as projected perpendicularly to the rotational axis of the fan, a remainder of the outer blade end forming a free end portion, and the trailing edges of said blade elements projecting on the discharge side of said ring and the end portion on the suction side of said ring diverging radially outward and then bending toward a discharge side of the fan.
Claim 3
Dependent Claim 30 words
A cooling fan as set forth in claim 1, wherein said ring includes notches formed therein along the rear edge thereof at positions adjoining fixed portions of said blade elements.

References Cited (Backward Citations)

US855131A Cited
US1929690A Cited
US1919250A Cited
US2370652A Cited
US2754919A Cited
FR1178215A Cited
US2972382A Cited
US3842902A Cited
JPS51915A Cited
US4135858A Cited
US4329946A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-03-18 1988-09-17 1989-03-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-03-18 1992-09-17 1993-03-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-03-18 1996-09-17 1997-03-19 $7700.00 Window Closed / Lapsed

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