Wing structure of air swirling device for internal...

F - Mech Eng,Light,Heat,Weapons – 02 – B

Patent

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Details

F02B 31/00 (2006.01) F02M 29/06 (2006.01) F02M 35/10 (2006.01) F02B 29/00 (2006.01)

Patent

CA 2472236

Disclosed is a wing structure of air swirling device for internal combustion engine, which has a swirling device body mounted in an air cleaner, a plurality of wings mounted slantingly and radially on the swirling device body for accelerating or increasing an airflow revolution, and one or more slits formed on prescribed positions of the plurality of wings for suppressing the formation of eddy in a negative pressure zone on the rear surface of each of the plurality of wings, includes a plurality of auxiliary wings protrudedly provided to the outside with reference to the surface of each of the wings, so that the airflow collided against the surface of each of said wings go straight ahead.

La présente invention concerne une structure d'aile pour un dispositif à turbulence d'air destiné à un moteur à combustion interne, qui présente un corps de dispositif à turbulence monté dans un filtre à air, une pluralité d'ailes montées radialement et avec une inclinaison oblique sur le corps du dispositif à turbulence pour accélérer ou augmenter la rotation de l'air et une ou plusieurs fentes formées aux endroits prescrits sur lesdites ailes afin de supprimer la formation de vent tourbillonnant dans une zone à pression négative, sur la surface arrière de chacune des ailes. Ce dispositif comprend une pluralité d'ailes auxiliaires prévues de manière à dépasser à l'extérieur par rapport à la surface de chacune des ailes, de sorte que le flux d'air ayant heurté la surface de chacune desdites ailes se dirige en ligne droite.

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