Claims
- 1. In an internal combustion engine having one or more cylinders, each cylinder having one port in the combustion chamber for the admission of air or combustible mixture and the discharge of combustion products, said engine having a rotary valve mechanism with a stationary sleeve communicating with the ports, a rotary member disposed in said sleeve and being rotatably driven, said rotary member comprising concentrically arranged and spaced inner and outer tubular members with the inner tubular member defining an exhaust passage and the annular space between the inner and outer tubular members defining an intake passage, said outer tubular member including an intake port for alignment with the port in communication with the combustion chamber, said inner tubular member including a radially extended passageway extending to the periphery of the outer tubular member is isolated relation to the annular space for communication with the port in the combustion chamber for selectively admitting air or a combustible mixture into the combustion chamber and discharging exhaust products therefrom through the port in the combustion chamber, said inner tubular member defining the exhaust passage and the annular space defining the intake passage being substantially straight throughout the length thereof, said inner tubular exhaust member being made in sections connected together with expansion joints, said outer tubular member being constructed of unitary construction, said expansion joints enabling transverse and longitudinal expansion of the inner tubular member thereby eliminating distortion of the outer tubular member due to differences in expansion and contraction.
- 2. The structure as defined in claim 1 wherein said outer tubular member includes longitudinally spaced, peripherally extending seal means disposed between adjacent pairs of inlet and exhaust ports therein.
- 3. The structure as defined in claim 2 wherein the engine includes a plurality of combustion chambers each of which is in the form of a cylinder having a reciprocating piston therein, said port extending laterally of the combustion chamber, said rotary valve assembly extending longitudinally alongside of the cylinders with the rotary member including duplicate intake and exhaust ports communicating with the intake passage and exhaust passage respectively with the single port in the combustion chamber enabling the firing order of the engine to be varied.
- 4. The structure as defined in claim 3 wherein said rotary member includes gear drive means associated with one end thereof, said inner tubular member being in axial communication with an exhaust pipe at one end thereof, said outer tubular member being in axial communication with an intake manifold at the same end thereof.
- 5. The structure as defined in claim 4 together with longitudinal seal strips sealing the space between the valve and sleeve, said seal strips being mounted in the stationary sleeve in which said rotary member rotates.
- 6. The structure as defined in claim 5 wherein the other end of the inner tubular member is closed and spaced from the adjacent end of the outer tubular member to enable circulation of intake air over substantially the entire external surface of the inner tubular member for heat transfer between counterflowing exhaust and intake gases.
- 7. The structure as defined in claim 6 having the rotary member floating or suspended in the sleeve, supported on each end by bearings, and having sufficient clearance or space between the outer surface and the inner surface of the sleeve so as not to come in contact with each other under any heat or expansion condition.
- 8. The structure as defined in claim 1 wherein said sleeve includes a roller rotatably supported in peripheral contact with the outer tubular member for simultaneous rotation therewith, a lubricating oil supplying blade assembly contacting the roller throughout its length and transferring a substantially constant but thin film of oil to the roller which transfers a thin coating of oil to the outer tubular member during rotation.
CROSS REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of my copending application Ser. No. 398,789, filed Sept. 19, 1974, now abandoned.
US Referenced Citations (6)
Foreign Referenced Citations (1)
Number |
Date |
Country |
445,211 |
Aug 1912 |
FR |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
398789 |
Sep 1974 |
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