Injection and mixture formation process and apparatus to implement same
AssigneeM.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft
InventorsHans-Jurgen Zurner, Wolfram Emmerling, Werner Steimer
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AssigneeM.A.N. Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft
InventorsHans-Jurgen Zurner, Wolfram Emmerling, Werner Steimer
Estimating the term…
The invention sets forth a method and apparatus for improving the injection and mixture of fuel and air in air-compressing combustion engines. The fuel is admitted into a rotationally symmetrical combustion chamber in such a manner that all droplets of the fuel stream are finely atomized at all speed and/or load ranges of the engine, and that the complete spray on entering the combustion chamber is so broken up that, from the combustion chamber wall to a point approximately one third of the combustion chamber radius, the broken-up spray matches the combustion chamber geometry, the injection of the fuel being effected in such a manner as to match the velocity and/or density distribution of the combustion air which rotates in the combustion chamber.
Process for introducing and mixing combustion air and fuel in air compressing, self-igniting, internal combustion engines having a piston crown formed with a rotation-symmetrical combustion chamber having a substantially flat bottom wall and a circumferential side wall, the inner diameter of said chamber increasing in a direction toward said bottom wall, in which combustion air is caused to be rotated about a longitudinal axis of the combustion chamber, and wherein a cylinder head is provided with a fuel injection nozzle in the region of a rim of the combustion chamber at an angle relative to said longitudinal axis and substantially in the direction of rotation of the combustion air, comprising the steps of injecting at least one spray of fuel into said chamber in the direction of air rotation and, in such a manner, that the individual droplets of fuel in said spray are finely atomized in all operating ranges of the engine and a substantially fuel-free zone is formed at the center of said combustion chamber, the radius of said zone being approximately one-third the radius of said chamber;
Dependencies are inferred from the claim text.