FIELD: ventilation.
SUBSTANCE: invention relates to axial fan for cooling air movement, in particular to internal combustion engine of vehicle including the blades (13, 14, 15) of the fan fixed on the hub (12) and having a pressure side and suction side, rear edge (16, 17, 18) and depth (t), and the ramp (13a, 14a, 15a) of the hub on corresponding pressure side of the blades, with a lifting opposite to rotational direction (D) of axial fan (11). Rear edge (16, 17, 18) has outer zone (16a, 17a, 18a) located radially outside the hub ramp (13a, 14a, 15a) and inner zone (16b, 17b, 18b) located radially inside the hub ramp (13a, 14a, 15a).
EFFECT: invention is aimed at airflow improvement.
11 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
VANED FAN | 2011 |
|
RU2579800C2 |
BLADE, PARTICULARLY ADJUSTABLE-PITCH BLADE, PROPELLER WITH SUCH BLADE AND TURBOMACHINE | 2012 |
|
RU2590766C2 |
GROOVED CHANNEL FOR GAS FLOW IN COMPRESSOR (VERSIONS) | 2001 |
|
RU2232922C2 |
BLADE MADE FROM THERMOPLASTIC COMPOSITE MATERIAL FOR HELICOPTER TAIL ROTOR AND METHOD OF MANUFACTURE OF SUCH BLADE | 1993 |
|
RU2113379C1 |
MEMBRANE VALVE WITHOUT SUPPORT RING AND SUPPORT PLATE | 2018 |
|
RU2724425C1 |
TURBOGENERATOR ROTOR | 1994 |
|
RU2144252C1 |
HELICOPTER TAIL ROTOR BLADE IN FAIRING MADE FROM THERMOPLASTIC COMPOSITE MATERIAL (VERSIONS) AND METHOD OF ITS MANUFACTURE | 1993 |
|
RU2111894C1 |
RADIAL EXPANDER | 2010 |
|
RU2548998C2 |
AXIAL FAN | 2010 |
|
RU2546894C2 |
TURBO COMPRESSOR IMPELLER EROSION INDICATOR | 2010 |
|
RU2516755C2 |
Authors
Dates
2017-01-24—Published
2011-12-01—Filed