Rotary piston internal combustion engine

Abstract

An internal combustion engine, and more particularly a rotary internal combustion engine, is provided with said engine having multiple combustion chambers delimited by piston heads and an engine housing wall that defines at least a section of a torus. Additionally, a method for operating the internal combustion engine is described.

1 . An internal combustion engine ( 1 ), the engine ( 1 ) comprising:
 an engine housing ( 5 ) having a first wall ( 10 ) delimiting a first combustion chamber ( 11 ) and a second wall ( 15 ) delimiting a second combustion chamber ( 16 ) with the first and second walls ( 10 ,  15 ) each defining at least a section of a torus;   a first piston ( 20 ) having a first piston head ( 21 A) further delimiting said first combustion chamber ( 11 ), a second piston head ( 21 B) further delimiting said second combustion chamber ( 16 ), a first pivot arm ( 22 A) coupled to a first connecting rod ( 25 ), and a second pivot arm ( 22 B) coupled to a common pivot point ( 30 );   a second piston ( 35 ) having a third piston head ( 36 A) further delimiting said first combustion chamber ( 11 ), a fourth piston head ( 36 B) further delimiting said second combustion chamber ( 16 ), a third pivot arm ( 37 A) coupled to a second connecting rod ( 40 ), and a fourth pivot arm ( 37 B) coupled to said common pivot point ( 30 );   a first crankshaft ( 45 ) coupled to said first connecting rod ( 25 ), and a second crankshaft ( 50 ) coupled to said second connecting rod ( 40 );   wherein said first and second pistons ( 20 ,  35 ) are guided along a curved path defined by said common pivot point ( 30 );   wherein said first and second pistons ( 20 ,  35 ) move in opposite directions;   wherein said second pivot arm ( 22 B) of said first piston ( 20 ) and said fourth pivot arm ( 37 B) of said second piston ( 35 ) oscillate about said common pivot point ( 30 ); and   wherein said first crankshaft ( 45 ) and said second crankshaft ( 50 ) are located outside the curved path of said first piston ( 20 ) and said second piston ( 35 ) as defined by said common pivot point ( 30 ).   
     
     
         2 . The combustion engine ( 1 ) of  claim 1 , wherein said first and second pistons ( 20 ,  35 ) move simultaneously. 
     
     
         3 . The combustion engine ( 1 ) of  claim 1 , wherein at least one of said first wall ( 10 ) and said second wall ( 15 ) are comprised of a right component and a left component coupled together. 
     
     
         4 . The combustion engine ( 1 ) of  claim 1 , wherein said first and said second walls ( 10 ,  15 ) further comprise cooling channels ( 17 ). 
     
     
         5 . The combustion engine ( 1 ) of  claim 4 , wherein said cooling channels ( 17 ) use either air or a liquid to provide cooling by a thermal heat transfer mechanism. 
     
     
         6 . The combustion engine ( 1 ) of  claim 1 , wherein said engine ( 1 ) further comprises at least one of an intake port ( 62 ), an exhaust port ( 63 ), a fuel injector port ( 55 ), and a glow plug ( 61 ) disposed in at least one of said first and second walls ( 10 ,  15 ). 
     
     
         7 . The combustion engine ( 1 ) of  claim 1 , wherein at least one of said first piston ( 20 ), said second piston ( 35 ), said first piston head ( 21 A), said second piston head ( 21 B), said third piston head ( 36 A), said fourth piston head ( 36 B), said first wall ( 10 ) or said second wall ( 15 ) are comprised of one selected from the group of aluminum, steel, a carbon composite, or a engineered composite. 
     
     
         8 . The combustion engine ( 1 ) of  claim 7 , wherein the carbon or engineered composite is fiber reinforced. 
     
     
         9 . The combustion engine ( 1 ) of  claim 1 , wherein a combination of piston plates ( 65 ) and primary member plates ( 70 ) are used to couple the first, second, third, and fourth piston heads ( 21 A,  21 B,  36 A,  36 B) to the corresponding first and second pistons ( 20 ,  35 ). 
     
     
         10 . The combustion engine ( 1 ) of  claim 6  wherein said intake port intersects with a combustion chamber ( 11 ,  16 ) in at least one of said first and second walls ( 10 ,  15 ) at an angle of about 90 degrees. 
     
     
         11 . The combustion engine ( 1 ) of  claim 6 , wherein said exhaust port ( 63 ) is open for a longer period of time than said intake port ( 62 ). 
     
     
         12 . The combustion engine ( 1 ) of  claim 1 , wherein the engine ( 1 ) is one of a two-cycle engine, a four-cycle engine, an Otto engine, and a diesel engine. 
     
     
         13 . The combustion engine ( 1 ) of  claim 1 , wherein the angle (α1, α2) between the first piston head ( 21 A) and the second piston head ( 21 B) of each piston ( 20 ,  35 ) is at least 110 degrees. 
     
     
         14 . The combustion engine ( 1 ) of  claim 1 , wherein said first connecting rod ( 25 ) is coupled to said first pivot arm ( 22 A) of said first piston ( 20 ) at a first junction comprising a first junction axis ( 100 A) and said second connecting rod ( 40 ) is coupled to said third pivot arm ( 37 A) of said second piston ( 35 ) at a second junction comprising a second junction axis ( 100 C); wherein said first junction axis ( 100 A), said second junction axis ( 100 C), and said common pivot axis ( 100 B) each being parallel to each other when aligned in a common plane ( 101 ). 
     
     
         15 . The combustion engine of  claim 14 , wherein said first crankshaft ( 45 ) comprises a first rotary axis ( 102 A) and said second crankshaft ( 50 ) comprises a second rotary axis ( 102 C), wherein said first rotary axis ( 102 A) and said first junction axis ( 100 A) are parallel to each other and aligned within a first plane ( 103 A); said second rotary axis ( 102 C) and said second junction axis ( 100 C) being parallel to each other and aligned within a second plane ( 103 C), wherein in a mid-center position of said first piston ( 20 ) and said second piston ( 35 ), said first plane ( 103 A) and said second plane ( 103 C) are perpendicular to said common plane ( 101 ). 
     
     
         16 . The combustion engine ( 1 ) of  claim 1 , wherein said first crankshaft ( 45 ) and second crankshaft ( 50 ) are coupled to a flywheel ( 75 ). 
     
     
         17 . The combustion engine ( 1 ) of  claim 16 , wherein said first crankshaft ( 45 ) and second crankshaft ( 50 ) rotate in the same direction. 
     
     
         18 . An internal combustion engine ( 1 ), the engine ( 1 ) comprising:
 an engine housing ( 5 ) having a first wall ( 10 ) delimiting a first combustion chamber ( 11 ) and a second wall ( 15 ) delimiting a second combustion chamber ( 16 ) with the first ( 10 ) and second ( 15 ) walls each defining at least a section of a torus;   a first piston ( 20 ) having a first piston head ( 21 A) further delimiting said first combustion chamber ( 11 ), a second piston head ( 21 B) further delimiting said second combustion chamber ( 16 ), a pivot arm ( 22 B) coupled to a common pivot point ( 30 ) and an engaging member ( 91 );   a second piston ( 35 ) having a first piston head ( 36 A) further delimiting said first combustion chamber ( 11 ), a second piston head ( 36 B) further delimiting said second combustion chamber ( 16 ), a pivot arm ( 37 B) coupled to said common pivot point ( 30 ) and an engaging member ( 91 );   a guide frame ( 90 ) having open receiving areas for a rotational crank pin ( 150 ) and engaging members ( 91 ), which translate the guide frame ( 90 ) from one linear end position to another and rotates rotational crank pin ( 150 );   a guiding means that includes two parallel guide columns ( 93 ); wherein the motion of the guide frame ( 90 ) is defined; and wherein said first ( 20 ) and second ( 35 ) pistons are guided along a curved path defined by said common pivot point ( 30 );   wherein said first ( 20 ) and second ( 35 ) pistons move in opposite directions; and wherein said pivot arm ( 22 B) of said first ( 20 ) piston and said pivot arm ( 37 B) of said second ( 35 ) piston oscillate about said common pivot point ( 30 ).   
     
     
         19 . The combustion engine of  claim 18 , wherein at least one of said first wall ( 10 ) and said second wall ( 15 ) are comprised of a right component and a left component coupled together. 
     
     
         20 . The combustion engine of  claim 18 , wherein said first and said second walls ( 10 ,  15 ) further comprise cooling channels ( 17 ).