Gas compressor and method with an improved inlet and...

F - Mech Eng,Light,Heat,Weapons – 04 – B

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F04B 53/10 (2006.01) F04B 39/00 (2006.01) F04B 39/10 (2006.01) F04B 39/12 (2006.01)

Patent

CA 2416042

A gas compressor and method according to which a plurality of inlet valve assemblies are angularly spaced around a bore. A piston reciprocates in the bore to draw the fluid from the valve assemblies during movement of the piston unit in one direction and compress the fluid during movement of the piston unit in the other direction and the valve assemblies prevent fluid flow from the bore to the valve assemblies during the movement of the piston in the other direction. A discharge valve is associated with the piston to permit the discharge of the compressed fluid from the bore.

La présente décrit une méthode ainsi qu'un compresseur de gaz doté d'un grand nombre de soupapes d'admission espacées à angle tout autour d'un alésage cylindrique. Un piston se déplace dans l'alésage; lorsqu'il se déplace dans une direction, il aspire le fluide des soupapes d'admission réparties autour de l'alésage, puis comprime le fluide lorsqu'il se déplace dans la direction inverse. Les soupapes d'admission se ferment pour empêcher le fluide de refouler dans le dispositif d'admission au moment de la compression. Une soupape d'évacuation est associée au piston pour permettre l'évacuation du fluide comprimé de l'alésage.

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