Drive cascade system for a watercraft

Patent metadata

Field	Value
Publication number	US-9199711-B2
Application number	US-201314382916-A
Country	US
Kind code	B2
Filing date	Mar 7, 2013
Priority date	Mar 12, 2012
Publication date	Dec 1, 2015
Grant date	Dec 1, 2015

Abstract

A drive method is disclosed. An embodiment includes an operation of at least one drive propeller of the drive system below a first predefinable propeller rotational speed according to a first operating state by operating at least one drive motor, connected to the at least one drive propeller, of the drive system via a first alternating voltage. The method further includes operation of the at least one drive propeller above the first predefinable 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 operating state 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.

First claim

The invention claimed is:

1. A drive method for a drive system, comprising:
operating at least one drive propeller of the drive system below a first predefinable propeller rotational speed according to a first operating state by operating at least one drive motor, connected to the at least one drive propeller, of the drive system via a first alternating voltage,
wherein according to the first operating state, at least one power inverter makes the first alternating voltage available;
operating the at least one drive propeller above the first predefinable propeller rotational speed according to a second operating state by operating the at least one drive motor via a second alternating voltage,
wherein according to the second operating state, a first internal combustion engine drives a first generator, which generates the second alternating voltage; and
initially operating the first internal combustion engine, during a transition from the first operating state to the second or a transition from the second operating state to the first, at a rotational speed where the at least one drive propeller is operated at the first predefinable propeller rotational speed and where the at least one power inverter synchronizes the first alternating voltage with the second alternating voltage.

2. The drive method of claim 1 , further comprising:
operating the at least one drive propeller above a second definable propeller rotational speed, relatively higher than the first predefinable propeller rotational speed, according to a third operating state by operating the at least one drive motor via a third alternating voltage,
wherein, according to the third operating state, the first alternating voltage of the at least one power inverter, in synchronized combination with the second alternating voltage, produces the third alternating voltage, and
wherein, during a transition from the second operating state to the third operating state, the at least one drive motor is only operated via the third alternating voltage when the first alternating voltage is synchronized with the second alternating voltage via the at least one power inverter.

3. The drive method of claim 1 , further comprising:
operating the at least one drive propeller above a third predefinable propeller rotational speed, relatively higher than the first predefinable propeller rotational speed, according to a fourth operating state by operating the at least one drive motor via a fourth alternating voltage,
wherein, according to the fourth operating state, each at least one further internal combustion engine drives each respective at least one further generator, each of which generates a further respective alternating voltage, which in synchronized combination with the second alternating voltage produces the fourth alternating voltage, and
wherein, during a transition from the second operating state to the fourth, a respective polar wheel angle of the at least one further generator is synchronized with a first polar wheel angle of the first generator.

4. The drive method of claim 3 , further comprising:
operating the at least one drive propeller above a fourth predefinable propeller rotational speed according to a fifth operating state by operating the at least one drive motor via a fifth alternating voltage,
wherein, according to the fifth operating state, the first alternating voltage of the at least one power inverter, in synchronized combination with the fourth alternating voltage, produces the fifth alternating voltage, and
wherein, during a transition from the fourth operating state to the fifth operating state, the at least one drive motor is only operated via the fifth alternating voltage when the first alternating voltage is synchronized with the third alternating voltage via the at least one power inverter.

5. The drive method of claim 1 , wherein, during operation in one of the operating states, a transition is made to another of the operating states in the event of a failure of parts of the drive system required to generate the respective alternating voltage,
with synchronization of the respective alternating voltage of the other of the operating states being performed, taking into account the alternating voltage present at the at least one drive motor.

6. The drive method of claim 2 , wherein, during operation in one of the operating states, a transition is made to another of the operating states in the event of a failure of parts of the drive system required to generate the respective alternating voltage, with synchronization of the respective alternating voltage of the other of the operating states being performed, taking into account the alternating voltage present at the at least one drive motor.

7. The drive method of claim 3 , wherein, during operation in one of the operating states, a transition is made to another of the operating states in the event of a failure of parts of the drive system required to generate the respective alternating voltage, with synchronization of the respective alternating voltage of the other of the operating states being performed, taking into account the alternating voltage present at the at least one drive motor.

8. The drive method of claim 4 , wherein, during operation in one of the operating states, a transition is made to another of the operating states in the event of a failure of parts of the drive system required to generate the respective alternating voltage, with synchronization of the respective alternating voltage of the other of the operating states being performed, taking into account the alternating voltage present at the at least one drive motor.

Assignees

• Siemens Ag

Inventors

• Hartig Rainer
• Schröder Dierk
• Tigges Kay
• Wycisk Michael

Classifications

• H02J2105/31

  for ships or vessels · CPC title

• B63H21/21

  Control means for engine or transmission, specially adapted for use on marine vessels · CPC title

• B63H21/17

  by electric motor · CPC title

• Y04S10/126

  the energy generation units being or involving electric vehicles [EV] or hybrid vehicles [HEV], i.e. power aggregation of EV or HEV, vehicle to grid arrangements [V2G] · CPC title

• Y02T10/70

  Energy storage systems for electromobility, e.g. batteries · CPC title