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:
May. 30, 2023

Filed:

Aug. 04, 2020
Applicants:

Paul Henning, Schwetzingen, DE;

Przemyslaw Kowalski, Wrocaw, PL;

Inventors:

Paul Henning, Schwetzingen, DE;

Przemyslaw Kowalski, Wrocaw, PL;

Assignee:

ZF CV SYSTEMS EUROPE BV, Brussels, BE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 55/08 (2006.01); F16D 65/00 (2006.01); F16D 55/2255 (2006.01); F16D 65/18 (2006.01); F16D 55/00 (2006.01); F16D 125/28 (2012.01); F16D 125/26 (2012.01);
U.S. Cl.
CPC ...
F16D 65/0075 (2013.01); F16D 55/2255 (2013.01); F16D 65/0006 (2013.01); F16D 65/18 (2013.01); F16D 2055/002 (2013.01); F16D 2055/0045 (2013.01); F16D 2125/26 (2013.01); F16D 2125/28 (2013.01); F16D 2250/0084 (2013.01);
Abstract

A brake caliper (') for a vehicle brake, in particular a disc brake of a commercial vehicle, includes a pressure piece (′), a thrust piece (′) configured to move axially relative to the pressure piece (′) in a thrust direction (A) to transmit a braking force and a guiding member () configured to limit the movement of the thrust piece (′) relative to the pressure piece (′) in at least one direction orthogonal to the thrust direction (A). The brake caliper (′) may further include a lever () pivotally supported between the thrust piece (′) and the pressure piece (′), wherein the guiding member () is configured to limit the movement of the lever () relative to the pressure piece (′) and/or the thrust piece (′) in at least one direction orthogonal to the thrust direction (A).


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