Radial cam driven internal combustion engine

Information

  • Patent Grant
  • 6691648
  • Patent Number
    6,691,648
  • Date Filed
    Thursday, July 25, 2002
    22 years ago
  • Date Issued
    Tuesday, February 17, 2004
    20 years ago
  • Inventors
  • Examiners
    • Kamen; Noah P.
    Agents
    • Lebens; Thomas F.
    • Sinsheimer, Schiebelhut & Baggett
Abstract
A radial cam driven internal combustion engine has connecting rod guide pins that slide into ends of the connecting rods, allowing the connecting rods to slide freely linearly while applying side loads on the connecting rods to the crankcase. The stationary guide pins protrude out from a center ring that floats over the central drive shaft. These pins are grooved to allow the pressure inside the connecting rod to escape. Each piston dwells at top dead center long enough to create a fixed volume environment and for all the fuel in the cylinder to be consumed.
Description




BACKGROUND OF INVENTION




The present invention relates generally to engines, and more particularly to radial cam driven internal combustion engines.




Radial cam driven internal combustion engines have multiple cylinders located radially about a central drive shaft. The pistons operating inside the cylinders have connecting rods with rollers at one end that push against and thereby rotate a cam, as opposed to the connecting rods being attached to a crank pin and crankshaft. Radial cam driven engines have been plagued with problems related to side loading of the connecting rod due to the tangent force vector resulting from the angular contact of the connecting rod roller against the cam, especially during the power stroke (or combustion stroke). Also, especially in the area of light aircraft and Ultralight vehicles, the engines traditionally available produce excess noise, vibration and lack efficiency.




There is thus a need in the art for an efficient, quiet and smooth running radial cam driven engine that alleviates the tangential force resulting from the angular contact of the connecting rod roller against the cam.




SUMMARY OF INVENTION




The present invention advantageously addresses the needs above as well as other needs by providing an efficient, quiet and smooth running radial cam driven engine having connecting rods and connecting rod guide pins that alleviate the tangential force resulting from the angular contact of the connecting rod roller against the cam.




In one embodiment, the invention can be characterized as a radial cam driven internal combustion engine. The engine has a crankcase, a camshaft rotatably attached to the crankcase and a cam fixedly attached to the camshaft. A plurality of cylinders are located radially about the camshaft and are attached to the crankcase. A plurality of pistons are located within the cylinders and a plurality of connecting rods are each attached at a first end to an associated piston. At the second end of each connecting rod is a hollow area. Each connecting rod cam roller in a plurality of connecting rod cam rollers is rotatably attached to the second end of an associated connecting rod and is located against the cam. Also, a first end of each connecting rod guide pin in a plurality of connecting rod guide pins is located slidably inside the hollow area of an associated connecting rod. A second end of each connecting rod guide pin is fixedly attached to the crankcase.




In another embodiment, the invention can be characterized as an apparatus for use in a radial cam driven internal combustion engine comprising a connecting rod having a hollow portion in one end and a connecting rod guide pin located slidably inside the hollow area. The connecting rod guide pin is stationary and the connecting rod slides on it during operation.




In yet another embodiment, the invention can be characterized as a process of piston operation in an internal combustion engine comprising the steps of pushing a piston in a cylinder during a compression stroke with a cam of a cam driven internal combustion engine and dwelling the piston at top dead center long enough to substantially consume all fuel in the cylinder when ignited.




A better understanding of the features and advantages of the present invention will be obtained by reference to the following detailed description of the invention and accompanying drawings which set forth an illustrative embodiment in which the principles of the invention are utilized.











BRIEF DESCRIPTION OF DRAWINGS




The above and other aspects, features and advantages of the present invention will be more apparent from the following more particular description thereof, presented in conjunction with the following drawings wherein:





FIG. 1

is a top planar cross sectional view of a radial cam driven engine according to the present invention.





FIG. 2

is a side cross sectional view of the radial cam driven engine of FIG.


1


.





FIG. 3

is a perspective side view a single piston and rod assembly of the engine of FIG.


1


.





FIG. 4

is an exploded perspective side view of a single piston and rod assembly of the engine of FIG.


1


.




Corresponding reference characters indicate corresponding components in the views of the drawings.











DETAILED DESCRIPTION




The following description of the presently contemplated best mode of practicing the invention is not to be taken in a limiting sense, but is made merely for the purpose of describing the general principles of the invention. The scope of the invention should be determined with reference to the claims.




Referring to

FIGS. 1 and 2

, shown is a top planar cross sectional view and a side cross sectional view of a radial cam driven engine


100


employing connecting rods


105


and connecting rod guide pins


110


according to one embodiment of the present invention.




Shown is a crankcase


115


, a plurality of cylinders


120


(eight in this case) and associated intake


121


and exhaust ports


122


, pistons


125


, spark plugs


130


, connecting rods


105


, connecting rod cam rollers


135


and connecting rod guide pins (shown in phantom)


110


. Also shown is a roller cam return track


140


, a stationary guide pin ring


145


, a cam


150


, a cam center connector


155


, a camshaft


160


and a power take off shaft


165


.




Referring next to

FIGS. 3 and 4

, shown is a perspective side view and an exploded perspective side view of a single piston and rod assembly of the engine of FIG.


1


. Shown are the piston


125


, connecting rods


105


, connecting rod cam rollers


135


and connecting rod guide pins


110


. Also shown are a roller cam return track


140


, a stationary guide pin ring


145


and a half of the cam


150


.




Each cylinder


120


is located in the same plane radially about the camshaft


160


. Each cylinder


120


also has a spark plug


130


operably attached thereto and has operable intake


121


and exhaust ports


122


. The pistons


125


located within the cylinders


120


are each rigidly attached


170


to a first end of their respective connecting rods


105


. A connecting rod cam roller


135


is rotatably attached on a second end of each connecting rod


105


. Each connecting rod


105


is also hollow and fits slidably over a first end of a connecting rod guide pin


110


. The stationary connecting rod guide pins


110


lead from each connecting rod


105


toward the center of the crankcase


115


between forward and rear halves of the cam


150


, but stop short of reaching the cam shaft


160


and are securely attached at their second ends to a stationary guide pin ring


125


which is in turn attached to the crankcase


115


. The connecting rod cam rollers


135


are located between the roller cam return track


140


and the cam


150


. The guide pins


110


pass between the wheels of each individual roller


135


and lead into the hollow areas of the connecting rods


105


. The cam


150


is fixedly attached to the camshaft


160


via the cam center connector


155


and the camshaft


160


is rotatably attached to the crankcase


115


.




The engine


100


is preferably two-stroke and as each piston


125


fires during a power stroke (or combustion stroke), the associated connecting rod


105


and connecting rod cam roller


135


push against the cam


150


. Simultaneously, the connecting rod


105


slides over the stationary connecting rod guide pin


110


as the cam


150


rotates. This alleviates the side loading of the connecting rod


105


due to the tangent force vector resulting from the angular contact of the connecting rod roller


135


against the cam


150


, especially during the combustion stroke. The connecting rod guide pins


110


address these loads and allow the connecting rods


105


to slide freely linearly while applying the side loads to the crankcase


115


. The connecting rod guide pins


110


are also grooved to allow the pressure inside the connecting rod


105


to escape. The cam


150


is 100% dynamically balanced. As each piston


125


fires, two opposing pistons are pushed so that all rotational and reciprocating forces are equally and effectively dampened out.




Each piston


125


dwells at top dead center at the end of the compression stroke long enough to create a fixed volume environment for all the fuel in the cylinder


120


to be consumed when combustion occurs. This allows the power stroke (or combustion stoke) to act as an expansion stroke cooling the spent exhaust gasses before they exit the exhaust port


122


. Preferably, each piston


125


dwells at the top of the stroke for 17.5 degrees of the cam


150


rotation. The major source of noise from the exhaust is the temperature differential. The hotter the gasses entering the cold ambient air, the faster the expansion at their boundary causing a popping sound at the exhaust port


122


. Since the spent exhaust gasses are cooled before they exist the exhaust port


122


, the noise is significantly reduced.




The radial design of the engine


100


allows many pistons


125


to be sequentially acting on a relatively small cam


150


surface as the cam


150


rotates. Also, the power pulses are divided up and are overlapping, thereby making the engine


100


run more smoothly. Thus, there are no tortional pressure reversals as there are on conventional engines. This is very important for light aircraft since the air frames are so light that the tortional resonance that is sent up through the drive train in single and two cylinder Ultralight engines is the biggest portion of the vibration felt by the pilot.




While the invention herein disclosed has been described by means of specific embodiments and applications thereof, numerous modifications and variations could be made thereto by those skilled in the art without departing from the scope of the invention set forth in the claims.



Claims
  • 1. A radial cam driven internal combustion engine comprising:a crankcase; a camshaft rotatably attached to the crankcase; a cam fixedly attached to the camshaft; a plurality of engine cylinders located radially about the camshaft and attached to the crankcase; a plurality of operable pistons located within the cylinders; a plurality of connecting rods, each connecting rod in the plurality of connecting rods attached at a first end to an associated piston and each connecting rod having a hollow area at the second end; a plurality of connecting rod cam rollers, each cam roller in the plurality of cam rollers attached at the second end of each connecting rod and located against the cam; and a plurality of connecting rod guide pins, each connecting rod guide pin in the plurality of connecting rod guide pins located slidably inside a hollow area of an associated connecting rod at a first end of each connecting rod guide pin wherein a second end of each connecting rod guide pin is fixedly attached to the crankcase.
  • 2. The engine of claim 1 wherein the connecting rod guide pins have grooves along the pins.
  • 3. An apparatus for use in a radial cam driven internal combustion engine comprising:a connecting rod having a hollow portion one end; and a connecting rod guide pin slidably inserted into the hollow area, wherein the connecting rod guide pin is stationary and on which the connecting rod slides during operation.
  • 4. The apparatus of claim 3 wherein the connecting rod guide pin has grooves along the pin.
CROSS REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of U.S. Provisional Patent Application No. 60/307,578, for RAD-CAM ENGINE, of Mark H. Beierle, filed Jul. 25, 2001, incorporated herein by reference.

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Provisional Applications (1)
Number Date Country
60/307578 Jul 2001 US