Airfoils with automatic pitch control

F - Mech Eng,Light,Heat,Weapons – 03 – B

Patent

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Details

F03B 17/06 (2006.01)

Patent

CA 2677808

An airfoil (30) arranged for use in a fluid flow of varying direction relative to the airfoil, has arranged thereon a plural axis hinge (50) for automatic adjustment of the angle of pitch of the airfoil. The airfoil can be applied to a rotary crossflow device for use in a fluid flow of varying apparent flow direction, an oscillating device for use in a fluid flow, a force generation device for use in a fluid flow of varying direction, or a flow control device for use in a fluid flow of alternating direction.

L'invention concerne un profil aérodynamique (30) s'utilisant dans un écoulement de fluide qui présente une direction variable par rapport audit profil, et sur lequel est placée une charnière à axes multiples (50) qui règle automatiquement l'angle d'attaque du profil aérodynamique. Le profil aérodynamique peut être appliqué dans un dispositif tournant à écoulement transversal utilisé dans un écoulement de fluide dont la direction apparente d'écoulement est variable, un dispositif oscillant s'utilisant dans un écoulement de fluide, un dispositif de production de force s'utilisant dans un écoulement de fluide à direction variable ou dans un dispositif de commande d'écoulement s'utilisant dans un écoulement de fluide à direction alternée.

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