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:
Nov. 10, 2020

Filed:

Dec. 17, 2014
Applicant:

Medartis Holding Ag, Basel, CH;

Inventors:

Dirk Thiel, Staufen, DE;

Andreas Mullis, Tenniken, CH;

Jürgen Schonhardt, Rheinfelden, DE;

Hermann Zeuner, Freiburg, DE;

Simon Martin Schätzle, Gottenheim, DE;

Assignee:

MEDARTIS HOLDING AG, Basel, CH;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
A61B 17/80 (2006.01); A61B 17/68 (2006.01); A61F 2/28 (2006.01); A61B 17/86 (2006.01);
U.S. Cl.
CPC ...
A61B 17/683 (2013.01); A61B 17/8052 (2013.01); A61B 17/8071 (2013.01); A61B 17/8085 (2013.01); A61B 17/8635 (2013.01); A61B 17/8645 (2013.01); A61F 2/2803 (2013.01); A61B 17/8057 (2013.01); A61B 2017/8655 (2013.01); A61F 2002/2807 (2013.01);
Abstract

A bone plate for reconstruction or trauma treatment of a bone which comprises first and second ends, a first contact surface for contacting and securing on a first region of the bone, and a plurality of receiving mechanism each having at least one opening for receiving at least one securing element. At least two adjacent wings extend at least from the first end of the main section, each has a second contact surface for contacting and securing to a second region of the bone, as well as at least one receiving mechanism having at least one opening for each receiving a securing element. A minimum bending stiffness of the main section, in relation to an axis (x) running perpendicular to the first contact surface, is greater than the minimum bending stiffnesses of the wings, but smaller than the total minimum bending stiffness of all wings extending from the first end.


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