Disc-type rotary engine

F - Mech Eng,Light,Heat,Weapons – 01 – C

Patent

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Details

F01C 1/063 (2006.01) F01B 3/00 (2006.01) F01C 9/00 (2006.01) F02B 53/00 (2006.01)

Patent

CA 2215219

A rotary disc having at least two radial concave portions and two radial convex portions on one end is opposed at the concave/convex surface to a concave/convex surface of a non-rotary disc having the concave/convex surface of the same shape, and one of the discs is made axially slidably and engaged to the other resiliently. Two variable volume chambers formed between the concave/convex surfaces of the two disc are used as a set of engine chambers in which a suction port is disposed to a slope of the first chamber on the side that the concave/convex surfaces of discs get into engagement, and the exhaust port is disposed to the slope of the second chamber on the side that the concave/convex surfaces of discs get out of the engagement. A gas reservoir combustion chamber communicating by way of a compression communication channel is disposed between the first chamber and the second chamber, and the compression stroke and the exhaust stroke are conducted simultaneously, while the expansion stroke and the suction stroke are conducted simultaneously in the two concave portions of the rotary disc passing through the two chambers.

Disque rotatif possédant au moins deux parties radiales concaves et deux parties radiales convexes sur une extrémité. Sa surface concave/convexe est opposée à une surface concave/convexe d'un disque non rotatif ayant une surface concave/convexe de même forme, et un des disques est fabriqué de façon à glisser dans le sens axial et est engagé dans l'autre de manière élastique. Les deux chambres à volume variable formées entre les surfaces concaves/convexes des deux disques servent de chambres de moteur dans lesquelles un orifice d'admission est placé en pente par rapport à la première chambre sur le côté où les surfaces concaves/convexes des disques s'engagent, et l'orifice de sortie est placé en pente par rapport à la deuxième chambre sur le côté où les surfaces concaves/convexe des disques se désengagent. Une chambre de combustion du carburant provenant du réservoir disposant d'un canal de communication de la compression se trouve entre la première et la deuxième chambres, et la course de compression et le temps d'échappement s'effectuent simultanément, alors que la course de détente et le temps d'admission s'effectuent simultanément dans les deux parties concaves du disque rotatif traversant les deux chambres.

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