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. 19, 2026

Filed:

Mar. 02, 2023
Applicant:

Tolomatic, Inc., Hamel, MN (US);

Inventors:

Gary W. Rosengren, Brooklyn Park, MN (US);

Ryan H. Bourgoine, Buffalo, MN (US);

Assignee:

Tolomatic, Inc., Hamel, MN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H02K 7/06 (2006.01); F16D 121/24 (2012.01); F16D 125/40 (2012.01); H02K 1/278 (2022.01); H02K 3/28 (2006.01); H02K 21/14 (2006.01); H02K 1/14 (2006.01); H02K 1/16 (2006.01); H02K 9/22 (2006.01);
U.S. Cl.
CPC ...
H02K 7/06 (2013.01); H02K 1/278 (2013.01); H02K 3/28 (2013.01); H02K 21/145 (2013.01); F16D 2121/24 (2013.01); F16D 2125/40 (2013.01); H02K 1/145 (2013.01); H02K 1/165 (2013.01); H02K 9/225 (2021.01); H02K 2201/12 (2013.01);
Abstract

An integrated motor linear actuator system includes one or more stator stages inside a housing. The stator stages have a winding and a stator core disposed about a common longitudinal axis, with a plurality of stator teeth configured to guide magnetic flux generated by the winding. A rotor is disposed along the longitudinal axis, within the stator stages, with a plurality of magnetic poles distributed circumferentially about the outer surface, adjacent the stator teeth, so that the stator stages are configured to drive the rotor into rotational motion about the longitudinal axis via the magnetic flux. A thrust tube and screw assembly are operationally coupled to the rotor, and configured to convert the rotational motion into linear motion of the thrust tube.


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