Prior art variable compression ratio engines have eccentric hinge pin expandable joints. These engines have hinge pins with off-set journals bearing for adjusting engine compression ratio. The prior art engines employ removable bearing caps for assembly of the eccentric hinge pins in the engine. A problem with these engines is that they would be expensive to manufacture and expensive to assemble due to the large number of bearing caps that need to be bolted together. A second problem is low mechanical stiffness and strength. The problem of low strength and stiffness is compounded in engines where the parting line of the bearing cap is oriented vertically rather than horizontally for best supporting the high mechanical forces encountered in internal combustion engines.
Eichi Kamiyama shows in U.S. Pat. No. 7,806,092 a variable compression ratio engine having an eccentric hinge pin assembly 25c, 25c1, 25c2, 25c3 and 25c4 retained in crankcase bearing caps 25a, 25a2 and jug bearing caps or bearing blocks 25b. Crankcase bearing caps 25a2 are bolted to crankcase 21, and jug bearing caps or bearing blocks 25b are bolted to jug 23. A problem with the invention taught in U.S. Pat. No. 7,806,092 is that it is expensive to manufacture and expensive to assemble due to the large number of bearing caps that need to be bolted to the jug and crankcase. A second problem is low mechanical stiffness and strength.
Per Gillbrand shows in U.S. Pat. No. 5,611,301 a variable compression ratio engine having an eccentric hinge pin 44 and removable bearing caps 46 and links 41. These components collectively result in a relatively large, heavy and expensive engine.
According to the present invention an expandable joint is made without removable bearing caps by preassembling eccentric bushings onto the hinge pin.
The expandable joint has a hinge type construction, but with the journals for each side of the hinge being spaced apart so that the distance between the two sides of the hinge changes with rotation of the hinge pin.
The expandable joint of the present invention is assembled by sliding the hinge pin into the hinged joint with the eccentric bushings attached. Once the hinge pin is in place, the eccentric bushings are locked in place with fasteners so that they do not rotate. After the eccentric bushings are locked in place, the hinge pin can be turned to expand the joint.
The expandable joint is intended for use in variable compression ratio engines, where expansion of the joint changes the compression ratio of the engine. A major benefit of the present invention is that it is robust and can support the large forces encountered in internal combustion engines. Another benefit of the present invention is that removable bearing caps are not required, resulting in a lower cost and a smaller size than expandable joints used in prior art variable compression ratio engines.
Eccentric hinged joint 2 has a primary or first bearing housing 4 having a plurality of primary journal bearings 6, and a second bearing housing 8 having a plurality of secondary journal sockets 10.
Eccentric hinged joint 2 has a hinge pin 12 having a plurality of primary journals 14 and a plurality of secondary journals 16. The primary journals 14 define a first journal axis 18 and the secondary journals 16 define a second journal axis 20, second journal axis 20 being offset from said first journal axis 18.
According to the preferred embodiment of the present invention, eccentric hinged joint 2 further includes one or more eccentric bushings 22. The eccentric bushings 22 are located in secondary journal sockets 10 after assembly of the eccentric hinged joint 2.
The primary journals 14 are rotatably mounted in the primary journal bearings 6, and the secondary journals 16 are rotatably mounted in the eccentric bushings 22 for providing eccentric motion of the eccentric hinged joint 2.
Referring now to
The eccentric hinged joint 2 further includes eccentric bushing retaining means 24 for preventing movement of the eccentric bushings 22 in the secondary journal sockets 10 after assembly of the eccentric hinged joint 2. In more detail, the bushing retaining means 24 secure or fixes the offset location of the eccentric bushing 22 in the secondary journal sockets 10, and in more detail bushing retaining means 24 fixes the location of bushing minor axis 42 in second bearing housing 8. The eccentric bushing retaining means 24 may optionally be a threaded fastener 26, a compression fastener 26b, a pin, a key, adhesive, solder, braze, weld, an interference fit, a combination of the above or other functional means. Retaining means 24 may be located above secondary journal socket 10 as shown, or optionally below or to the side of secondary journal socket 10.
In the embodiment of the present invention shown in
According to the present invention, eccentric hinged joint 2 has at least one eccentric bushing 22 assembled onto hinge pin 12 between two primary journals 14.
Eccentric hinge joint 2 further has a first axial assembly clearance for slidably assembling an eccentric bushing 22 on hinge pin 12 through at least one primary journal bearing 6. Eccentric hinge joint 2 further has a second axial assembly clearance for slidably assembling a primary journal 14 on hinge pin 12 through at least one secondary journal socket 10. Preferably, according to the present invention, eccentric hinge joint 2 has a first axial assembly clearance for slidably assembling an eccentric bushing 22 on hinge pin 12 through at least one primary journal bearing 6, and eccentric hinge joint 2 has a second axial assembly clearance for slidably assembling a primary journal 14 on hinge pin 12 through at least one secondary journal socket 10. In more detail, second bearing housing 8 and secondary journal socket 10 have an internal diameter and primary journal 14 has an outer primary journal diameter, where the internal diameter is larger than the outer primary journal diameter, thereby providing assembly clearance for the primary journal 14 to pass through the secondary bearing housing 8 and secondary journal socket 10 for assembly of the eccentric hinged joint 2.
Eccentric bushing 22 also has an outer bushing diameter and primary journal 14 has an outer primary journal diameter. Preferably, according to the present invention, the outer bushing diameter is within 0.007 inches of the outer primary journal diameter thereby enabling hinge pin 12 to slide into hinged joint 2.
A significant benefit of the present invention is that removable bearing caps are not required for assembling the hinge pins in the engine. Referring now to
According to the present invention, hinge pin 12 may be a contiguous metal shaft including at least on primary journal 14 and at least one secondary journal 16. Assembled eccentric bushings 22a are typically employed in embodiments of the present invention having a secondary journal 16 located between two primary journals 14, and in more detail when the secondary journal has a smaller diameter than the two outer primary journals.
Referring now to
Referring now to
Assembled hinge pin 12b has a central shaft 44 and at least one primary journal eccentric 14b rigidly assembled onto central shaft 44. Hinge pin 12b further includes retaining means 45 for rigidly retaining primary journal eccentric 14b on central shaft 44. Preferably the retaining means 45 is selected from a group consisting of an interference fit; a key; a pin; a threaded fastener; adhesive; solder; braze; weld, or other functional means.
Eccentric bushing 22b has a slip fit assembly onto central shaft 44. Central shaft 44 has a secondary journal surface 16b for supporting eccentric bushings 22b.
Referring now to
According to an embodiment of the present invention, eccentric bushings 22 are mounted in first bearing housing 4, and primary journal bearings 6 are mounted in second bearing housing 8, and secondary journals 16 are repositioned to align with eccentric bushings 22, and primary journals 14 are repositioned to align with journal bearings 6, and retaining means 24 is repositioned to align with eccentric bushings 22.
The present invention is intended for use in variable compression ratio engines, but may also be used for other purposes where an expandable joint is needed.
This application relates to Provisional Application No. 62/176,649 having a filing date of Feb. 24, 2015, and Provisional Application No. 62/230,277 having a filing date of Jun. 1, 2015, and Provisional Application Docket No. VC3-00C having a filing date of Feb. 1, 2016 and a US Express Mail No. EK 886663519 US with a Provisional Application No. not yet assigned.
Filing Document | Filing Date | Country | Kind |
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PCT/US16/00017 | 2/22/2016 | WO | 00 |
Number | Date | Country | |
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62176649 | Feb 2015 | US |