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:
Apr. 16, 2013

Filed:

Jul. 24, 2009
Applicants:

Erkan Hodza, Asperg, DE;

Henry Schuett, Sachsenheim, DE;

Uwe Kretzschmann, Besigheim, DE;

Inventors:

Erkan Hodza, Asperg, DE;

Henry Schuett, Sachsenheim, DE;

Uwe Kretzschmann, Besigheim, DE;

Assignee:

Komet Group GmbH, Besigheim, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23B 27/16 (2006.01); B23B 47/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

The invention relates to a rotating cutting tool, in particular a boring tool for use in machine tools. The cutting tool comprises at least one cutting insert, designed as an indexable insert, that has an active main blade located near a corner of the insert, the outer end of said blade defining a circular flight path radius (R) as the blade rotates, said blade penetrating into a work piece at a pre-determined cutting depth (t) near a pre-formed round hole. Also provided is a secondary blade that is disposed opposite to an advancing direction and that aligns with the outermost end of the main blade, the entire length of said blade having a smaller radius than the circular flight path radius (R) of the main blade, wherein a secondary blade free surface aligns with the secondary blade opposite to the direction of rotation. A unique characteristic of the invention is that the secondary blade free surface comprises a support part disposed at a distance from the secondary blade, the peripheral radius of said part being larger than the circular flight path radius R of the active main blade by an overshoot amount (Y).


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