Cooling fan for internal combustion engine

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

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Details

416192, 415172A, F04D 2938

Patent

active

045056412

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.

REFERENCES:
patent: 855131 (1907-05-01), Preidel
patent: 1919250 (1931-11-01), Olson
patent: 1929690 (1933-10-01), Huntman
patent: 2370652 (1939-06-01), Frisbie
patent: 2754919 (1956-07-01), Blue
patent: 2972382 (1961-02-01), Manzolillo
patent: 3842902 (1974-10-01), Poslusny
patent: 4135858 (1979-01-01), Entat
patent: 4329946 (1982-05-01), Longhouse

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