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:
Jul. 17, 2012

Filed:

Aug. 22, 2008
Applicants:

Tomohiko Tsuruta, Nukata-gun, JP;

Motonori Tominaga, Anjo, JP;

Haruo Arakawa, Toyota, JP;

Takayuki Takeshita, Anjo, JP;

Jin Yamada, Toyota, JP;

Takahisa Yokoyama, Anjo, JP;

Inventors:

Tomohiko Tsuruta, Nukata-gun, JP;

Motonori Tominaga, Anjo, JP;

Haruo Arakawa, Toyota, JP;

Takayuki Takeshita, Anjo, JP;

Jin Yamada, Toyota, JP;

Takahisa Yokoyama, Anjo, JP;

Assignees:

Nippon Soken, Inc, Nishio-shi, JP;

Advics Co., Ltd., Kariya, JP;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F16D 55/08 (2006.01);
U.S. Cl.
CPC ...
Abstract

An electric brake device comprises a caliper holding braking members and having an electric motor attached thereto, a reduction mechanism for transmitting an input rotation of one input element thereof from the electric motor to two output elements thereof at reduced speeds, a rotation-linear motion converting mechanism for converting the rotation of one of the output elements into a linear motion of one of the braking members, and a thrust force support member connected to the other output element and screw-engaged with the caliper, wherein the rotation-linear motion converting mechanism is supported by the thrust force support member to be movable together in a thrust direction and is provided with rotation limiting portions for limiting the rotation in a reverse direction of the one output element to a predetermined range, and wherein the thrust force support member is set to be greater in resistance to operation than the rotation-linear motion converting mechanism.


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