IP Library Granted Patent US 9,239,002
Granted Patent B2
US 9,239,002 · App. 14/036,694 · Granted Jan 19, 2016

Orbiting planetary gearing system and internal combustion engine employing the same

Inventor: Heinz-Gustav Reisser (Coshocton, OH)
F02B53/00F01C1/077F01C9/002F01C17/02F01C21/008F02B53/02Y02T10/17
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 9,239,002
App. No.
14/036,694
Granted
Jan 19, 2016
Kind
B2
Abstract

The innovation concerns an orbiting planetary gearing system and an internal-combustion engine employing the same. In aspects, the engine can comprise an engine housing having a first wall delimiting a first combustion chamber, a first primary member having a first piston and a second primary member having a second piston. The pistons can also delimit the first combustion chamber. The first wall defines at least a section of a toroid, and the pistons are guided along a curved path defined by the section of the toroid. The primary members can be coupled to an intermediate member. In various embodiments, the intermediate member can couple motion of the primary members to a crankshaft via an orbiting planetary gearing system.

Claims (42)

1. A system, comprising:

an intermediate member sub-assembly comprising an orbiting planetary gearing system;

at least one crankshaft coupled to the intermediate member sub-assembly; and

one or more sliders and one or more slider rods,

wherein the orbiting planetary gearing system couples linear motion of the intermediate member sub-assembly to rotational motion of the at least one crankshaft,

wherein the orbiting planetary gearing system comprises a plurality of planet gears coupled to a planet carrier,

wherein teeth of each of the plurality of planet gears engage with teeth of a ring gear and with teeth of a crank spur gear associated with the at least one crankshaft,

wherein the planet carrier moves vertically along the one or more slider rods,

wherein the one or more slider rods is coupled to one or more sliders, and

wherein each of the one or more sliders move horizontally along one or more slider bearings.

2. The system of claim 1 , further comprising:

a first primary member coupled to the intermediate member sub-assembly; and

a second primary member coupled to the intermediate member sub-assembly,

wherein the linear motion of the intermediate member sub-assembly is coupled to rotational motion of the first primary member and the second primary member.

3. The system of claim 2 , further comprising an engine housing comprising a first cylinder liner and a second cylinder liner, wherein the first primary member is coupled to a first piston, wherein the second primary member is coupled to a second piston, and wherein a combustion chamber is defined by the first piston, the second piston, the first cylinder liner, and the second cylinder liner.

4. An internal combustion engine, the engine comprising:

an engine housing comprising a first cylinder liner and a second cylinder liner defining at least a first section of a toroid between the first cylinder liner and the second cylinder liner and delimiting a first combustion chamber;

a first primary member coupled to a first piston, the first piston also delimiting the first combustion chamber, the first piston guided along a first curved path defined by the first section of the toroid;

a second primary member coupled to a second piston, the second piston also delimiting the first combustion chamber, the second piston guided along a second curved path defined by the first section of the toroid;

an intermediate member sub-assembly coupled to the first and the second primary members, the intermediate member sub-assembly comprising an orbiting planetary gearing system;

at least one crankshaft coupled to the intermediate member sub-assembly; and

one or more sliders and one or more slider rods,

wherein the orbiting planetary gearing system comprises a plurality of planet gears coupled to a planet carrier,

wherein teeth of each of the plurality of planet gears engage with teeth of a ring gear and with teeth of a crank spur gear associated with the at least one crankshaft,

wherein the planet carrier moves vertically along the one or more slider rods,

wherein the one or more slider rods is coupled to the one or more sliders, and

wherein each of the one or more sliders move horizontally along one or more slider bearings.

5. The internal combustion engine of claim 4 , wherein the first primary member and the second primary member rotate around the at least one crankshaft.

6. The internal combustion engine of claim 4 , wherein at least one of the first cylinder liner or the second cylinder liner comprises cooling channels that facilitate heat transfer away from the internal combustion engine.

7. The internal combustion engine of claim 4 , wherein at least one of the first piston or the second piston comprises contours that create vortices in the first combustion chamber.

8. The internal combustion engine of claim 4 , wherein the at least one crankshaft comprises at least two crankshafts connected by a spline joint.

9. The internal combustion engine of claim 4 ,

wherein the engine housing comprises a third cylinder liner and a fourth cylinder liner defining at least a second section of the toroid between the third cylinder liner and the fourth cylinder liner and delimiting a second combustion chamber;

wherein the first primary member coupled to a third piston, the third piston also delimiting the second combustion chamber, the third piston guided along a third curved path defined by the second section of the toroid; and

wherein the second primary member coupled to a fourth piston, the fourth piston also delimiting the second combustion chamber, the fourth piston guided along a fourth curved path defined by the second section of the toroid.

10. The internal combustion engine of claim 4 , wherein the first primary member is coupled to the intermediate member sub-assembly via a first roller and the second primary member is coupled to the intermediate member sub-assembly via a second roller.

11. The internal combustion engine of claim 10 , wherein the first roller couples to the first primary member via a first offset axis and the second roller couples to the second primary member via a second offset axis, whereby rotational motion of the first primary member and the second primary member is coupled to linear motion of the intermediate member sub-assembly.

12. The internal combustion engine of claim 4 , wherein the intermediate member sub-assembly slides linearly along a plurality of rails.

13. The internal combustion engine of claim 4 , wherein the at least one crankshaft is coupled to a flywheel and a cooling impeller.

14. The internal combustion engine of claim 4 , wherein at least one of the first piston or the second piston is ceramic.

15. The internal combustion engine of claim 4 , wherein the at least one crankshaft is coupled to a front-end pulley and to a back-end pulley.

16. The internal combustion engine of claim 4 , wherein the first primary member comprises a first primary member component and a second primary member component, the first primary member component and the second primary member component being coupled together, and wherein the second primary member comprises third primary member component and a fourth primary member component, the third primary member component and the fourth primary member component being coupled together.

Continuity (3)
Continuation In Part 12849406 · Aug 3, 2010
Provisional Application 61705490 · Sep 25, 2012
Related Publication 20140020651A1 · Jan 23, 2014