Rotor of a compression-wave engine

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

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230/134, 123/21

F04D 29/26 (2006.01) F04F 13/00 (2009.01)

Patent

CA 2010583

ABSTRACT OF THE DISCLOSURE The rotor (1) of a compression-wave engine has cells (6) on its periphery which are concavely curved on the two end faces of the rotor (1) inwards towards its center and towards the rotor axis. Consequently, the absolute trajectory of a particle runs from its entry point (7) into a cell (6) up to its exit point (8) therefrom in a virtually recti- linear fashion, whereby in the scavenging process the mixing zone between the two media participating in the compression-wave process, and thus the scavenging losses, are greatly reduced by comparison with straight cells. (Fig. 2)

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