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An internal combustion aircraft engine comprising a cylinder head having a cylindrical head bore formed therein, a piston, and spark plugs, the cylinder head bore and piston designed to reduce engine knock. The cylinder head is fixedly attached to a top end of a cylinder barrel formed with cylindric

An internal combustion aircraft engine comprising a cylinder head having a cylindrical head bore formed therein, a piston, and spark plugs, the cylinder head bore and piston designed to reduce engine knock. The cylinder head is fixedly attached to a top end of a cylinder barrel formed with cylindrical walls, the cylinder head bore and the cylindrical walls defining a cylinder. The cylinder head bore has formed therein an outwardly protruding cavity with respect to the top end of the cylinder barrel. The piston has a piston crown, and the piston contained within the cylinder, the piston crown, the cylinder walls, and the cylinder head bore define a combustion chamber. The piston crown has a concavity formed therein, and the piston is constructed and arranged to reciprocate within the cylinder. The concavity of the piston crown and the cavity cooperate at a top dead center position of the piston to form a swirl chamber. The piston crown has formed along a peripheral edge thereof a squish area that corresponds to a second squish area formed in the cylinder head bore, so that when the piston approaches top dead center, the squish area and the second squish area cooperate to cause combustion gases to move radially inward of the combustion chamber and into the swirl chamber. Spark plugs extend through the cylinder head, the tips of which are disposed within the swirl chamber.

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1. An internal combustion engine for powering an aircraft, the internal combustion engine comprising:a cylinder head having a cylindrical head bore and a high swirl port integrally formed therein, said cylinder head fixedly attached to a top end of a cylinder barrel formed with cylindrical walls, th

1. An internal combustion engine for powering an aircraft, the internal combustion engine comprising:a cylinder head having a cylindrical head bore and a high swirl port integrally formed therein, said cylinder head fixedly attached to a top end of a cylinder barrel formed with cylindrical walls, the cylinder bore and the cylindrical walls defining a cylinder, said cylinder head bore having an outwardly protruding cavity with respect to the top end of the cylinder barrel, wherein said cavity is a bell-shaped dome;a piston having a piston crown, said piston contained within the cylinder, said piston crown, said cylinder walls, and said cylinder head bore defining a combustion chamber, said piston crown having a concavity formed therein, and the piston construction arranged to reciprocate within the cylinder;said concavity of the piston crown and said cavity cooperating at a top dead center position of the piston to form a swirl chamber;said piston crown having formed along a peripheral edge thereof a squish area that corresponds to a second squish area formed in the cylindrical bore head, so that when said piston approaches said top dead center, said squish area and said second squish area cooperate to cause combustion gases to move radially inward of the combustion chamber and into the swirl chamber; and spark plugs extending through the cylinder head, said spark plugs each having a tip whereupon a spark is adapted to be generated, each of said tips being disposed within said swirl chamber;wherein a first spark plug of said spark plugs is tilted toward an exhaust port at an approximate angle of 19.4 degrees and a second spark plug of said spark plugs is tilted toward said exhaust port at an approximate angle of 9.9 degrees;wherein said spark plugs enter said combustion chamber at an approximate angle of 30 degrees;wherein the distance between said spark plug tips is at an approximate distance of 0.6 times the diameter of said cylinder head bore; andwherein the clearance between said squish area and said second squish area when said piston reaches said top dead center is approximately 0.047 inches. 2. An internal combustion engine for powering an aircraft, the internal combustion engine comprising:a cylinder head having a cylindrical head bore formed therein, said cylinder head fixedly attached to a top end of a cylinder barrel formed with cylindrical walls, the cylinder head bore and the cylindrical walls defining a cylinder, said cylinder head bore having an outwardly protruding cavity with respect to the top end of the cylinder barrel;a piston having a piston crown, said piston contained within the cylinder, said piston crown, said cylinder walls, and said cylinder head bore defining a combustion chamber, said piston crown having a concavity formed therein, and the piston construction arranged to reciprocate within the cylinder;said concavity of the piston crown and said cavity cooperating at a top dead center position of the piston to form a swirl chamber;said piston crown having formed along a peripheral edge thereof a squish area that corresponds to a second squish area formed in the cylinder head bore, so that when said piston approaches said top dead center, said squish area and said second squish area cooperate to cause combustion gases to move radially inward of the combustion chamber and into the swirl chamber; and spark plugs extending through the cylinder head, said spark plugs each having a tip whereupon a spark is adapted to be generated, each of said tips being disposed within said swirl chamber, wherein said spark plugs are tilted toward an exhaust port. 3. The internal combustion engine of claim 2, wherein a first spark plug of said spark plugs is tilted toward said exhaust port at an approximate angle between 15 and 25 degrees and a second spark plug of said spark plugs is tilted toward said exhaust port at an approximate angle between 5 and 15 degrees. 4. The internal combustion engine of claim 3, wherein s aid first spark plug is tilted toward said exhaust port at an approximate angle of 19.4 degrees and said second spark plug is tilted toward said exhaust port at an approximate angle of 9.9 degrees.