The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 25, 2016

Filed:

Oct. 27, 2012
Applicant:

Daimler Ag, Stuttgart, DE;

Inventors:

Herbert Zoeller, Stuttgart, DE;

Naima Seddouk, Aichwald, DE;

Assignee:

Daimler AG, Stuttgart, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02F 3/28 (2006.01); F02B 17/00 (2006.01); F02B 23/06 (2006.01);
U.S. Cl.
CPC ...
F02B 17/005 (2013.01); F02B 23/0651 (2013.01); Y02T 10/125 (2013.01);
Abstract

A combustion process with auto-ignition for direct-injection internal combustion engines involves dividing injection jets at a jet divider contour into a first partial quantity, a second partial quantity, and third partial quantities. The first partial quantity enters into the piston cavity, the second partial quantity enters via the piston step into a region between the piston crown and the cylinder head, and the third partial quantities, starting from the respective injection jet, spread out on both sides in the peripheral direction in opposite directions along the piston step, and the respective third partial quantities collide with one another between two adjacent injection jets within the piston step and are deflected radially inwardly. The first partial quantity and the second partial quantity form a first combustion front and a second combustion front, and the partial quantities which in each case are jointly deflected inwardly form a third combustion front radially inwardly into a gap between the injection jets. The injection jets are deflected upstream from the jet divider contour in the direction of the piston by means of a resultant flow formed essentially from a swirl, a squish gap flow, and a jet flow.


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