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. 27, 2018

Filed:

Feb. 12, 2014
Applicant:

Cpac Systems Ab, Göteborg, SE;

Inventors:

Mathias Lindeborg, Göteborg, SE;

Yoshikazu Nakayasu, Shizuoka, JP;

Assignee:

CPAC Systems AB, Göteborg, SE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B63H 25/42 (2006.01); B63H 20/12 (2006.01); B63H 25/02 (2006.01); B63J 99/00 (2009.01); B63H 5/08 (2006.01); B63H 5/125 (2006.01); B63H 21/21 (2006.01); B63H 20/00 (2006.01);
U.S. Cl.
CPC ...
B63H 25/42 (2013.01); B63H 5/08 (2013.01); B63H 5/125 (2013.01); B63H 20/12 (2013.01); B63H 21/21 (2013.01); B63H 25/02 (2013.01); B63J 99/00 (2013.01); B63H 2020/003 (2013.01); B63H 2025/026 (2013.01); B63J 2099/008 (2013.01);
Abstract

The present disclosure relates to a propulsion control system () for controlling a marine vessel () comprising at least four propulsion units (). The marine vessel () comprises a longitudinal centre line (L) and a transversal line (T). The transversal line (T) extends in a direction perpendicular to the longitudinal centre line (L) and also extends through the steering axis of the aftmost of the propulsion units. The marine vessel () comprises four quadrants (I, II, III, IV) defined by the longitudinal centre line (L) and the transversal line (T) wherein a first (I) and a second (II) quadrant are located on the same side of said longitudinal centre line (L). When a combined sway and yaw motion is desired, the thrust of one propulsion unit is directed towards the second (I) quadrant, and the thrust of the other propulsion units is directed towards the first (II) quadrant.


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