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:
Jun. 14, 2016

Filed:

Aug. 12, 2015
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Rainer Hartig, Buxtehude, DE;

Dierk Schröder, Selent, DE;

Kay Tigges, Hamburg, DE;

Michael Wycisk, Moenkeberg, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B63H 21/17 (2006.01); B63H 21/20 (2006.01); B63H 21/14 (2006.01); B63H 5/08 (2006.01); F02D 29/02 (2006.01); B60L 11/08 (2006.01); B63H 23/24 (2006.01); B63H 1/04 (2006.01); B63H 5/07 (2006.01); B63H 21/21 (2006.01); H02J 3/38 (2006.01); H02J 3/46 (2006.01);
U.S. Cl.
CPC ...
B63H 21/20 (2013.01); B60L 11/08 (2013.01); B63H 1/04 (2013.01); B63H 5/07 (2013.01); B63H 5/08 (2013.01); B63H 21/14 (2013.01); B63H 21/17 (2013.01); B63H 21/21 (2013.01); B63H 23/24 (2013.01); F02D 29/02 (2013.01); H02J 3/38 (2013.01); H02J 3/46 (2013.01); B63H 2021/205 (2013.01); Y02E 60/721 (2013.01); Y02T 10/70 (2013.01); Y02T 10/7077 (2013.01); Y02T 70/5236 (2013.01); Y04S 10/126 (2013.01);
Abstract

A watercraft and controller are disclosed. An embodiment includes a controller for the water craft being configured to operate at least one drive propeller of the drive system of the watercraft below a first propeller rotational speed according to a first operating state by operating at least one drive motor, connected to the at least one drive propeller, via a first alternating voltage; and operate the at least one drive propeller above the first propeller rotational speed according to a second operating state by operating the at least one drive motor via a second alternating voltage. In a transition from the first into the second operating state or vice versa, the first internal combustion engine is operated at such a rotational speed that the at least one drive propeller is driven at the first propeller rotational speed, and the first alternating voltage is synchronized with the second alternating voltage.


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