Watercraft and Method for Operating the Watercraft

Abstract

A watercraft and method for operating the watercraft, wherein the watercraft includes an electrical system that is present in a space that has an atmosphere that differs from air, where the space is formable by a pressure hull, where the atmosphere contains, for example, an inert gas, and where the space having the electrical system is filled with the atmosphere.

Claims

1.-14. (canceled)

15. A watercraft comprising: an electrical system arrange within a space of the watercraft; wherein the space has an atmosphere which is different from air.

16. The watercraft as claimed in claim 15, wherein the space is formed by a reaction valve.

17. The watercraft as claimed in claim 15, wherein the atmosphere has a low-reaction gas.

18. The watercraft as claimed in claim 16, wherein the atmosphere has a low-reaction gas.

19. The watercraft as claimed in claim 15, wherein the atmosphere has a power fuel.

20. The watercraft as claimed in claim 16, wherein the atmosphere has a power fuel.

21. The watercraft as claimed in claim 17, wherein the atmosphere has a power fuel.

22. The watercraft as claimed in claim 15, wherein the space has an overpressure.

23. The water craft as claimed in claim 15, wherein the space is flushed predominantly with the atmosphere.

24. The watercraft as claimed in claim 15, wherein the electrical system includes at least one of (i) a current converter, (ii) an electrical motor and (iii) a power distribution network.

25. The watercraft as claimed in claim 15, wherein the watercraft is a submarine.

26. The watercraft as claimed in claim 15, wherein the watercraft is an unmanned submarine.

27. A method for operating a watercraft, comprising: arranging an electrical system within a space of the watercraft; and filling the space with an atmosphere.

28. The method as claimed in claim 27, wherein the atmosphere of the watercraft is different from air.

29. The method as claimed in claim 27, wherein a pressure greater than air pressure is produced in the space.

30. The method as claimed in claim 28, wherein a pressure greater than pressure of the air is produced in the space.

31. The method as claimed in claim 27, wherein the atmosphere is used as a motor fuel.

32. The method as claimed in claim 27, wherein the space is cleared of all people before being filled with the atmosphere.

33. The method as claimed in claim 29, wherein the pressure has a dependency on an immersion depth.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0028] The invention is described by way of example below with reference to exemplary embodiments, in which:

[0029] FIG. 1 an unmanned under water vehicle;

[0030] FIG. 2 a ship as a watercraft; and

[0031] FIG. 3 is a flowchart of the method in accordance with the invention.

DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS

[0032] The diagram according to FIG. 1 shows a submarine 1 as an example of a watercraft. The submarine has a technical system 15. As components, the technical system 15 has, for example, an electric motor, a current converter, a battery, a fuel cell and/or a mains supply, where these elements are not shown in FIG. 1. The electrical system 15 is disposed in a space 8. The electrical system 15 can also be disposed entirely or partially in a space 18 of a tower 14 of the submarine 1. The space 8 or 18 has an atmosphere 20, which is different from air and is symbolized with three sinuous lines. The atmosphere 20 has predominantly a low-reaction gas or a low-reaction gas mixture or consists of the same. The space 8 is formed by a reaction valve 19. A simpler, more reliable operation of the electrical system 15 is possible via the special atmosphere 20. The reaction valve 19 separates the inner space 8 of the underwater vehicle 1 from the surrounding water masses.

[0033] The diagram of FIG. 2 shows a ship 2 as an example of a watercraft. The ship 2 has superstructures 13. The ship 2 can be driven by way of a propeller 26, which is connected to a transmission 23 by way of a shaft 27. An internal combustion engine 24 that is supplied with fuel by way of a fuel pipe 25 is connected to the transmission 23. The transmission 23 is also connected to an electrical machine 3 by way of a shaft 31. The ship has a space 8 irrespective of the type of drive with or without a propeller or with or without a transmission or with or without an internal combustion engine 24, such as a diesel engine. The space 8 is bounded by side walls 9 and 10, a ceiling 11 and a floor 12. The space 8 is accessible by a person 30. If an atmosphere 20, such as predominantly nitrogen as a low-reaction gas with few or no oxygen portions, is disposed in the space 8, the space 8 is cleared of all people 30. At least one part of the drive train of the ship 2 is disposed in the space 8. The drive train has the electrical motor 3. The electrical motor 3 can also be operated with a generator, for instance. The electrical motor 3 is powered by a current converter 4 by way of a three-phase electrical connection 6. The current converter 4 receives its electrical energy by way of a two-phase DC bus 7, for instance. A battery 5, a fuel cell 22 and a distribution network 21 is connected to this two-phase DC bus 7. The distribution network 21, the fuel cell 22, the battery 5, the DC bus 7, the current converter 4 and/or the motor 3 are a technical system individually and/or in combination. This technical system is disposed in the atmosphere 20, which has little or no oxygen 02. In one embodiment, the atmosphere is a motor fuel such as natural gas or hydrogen, for instance. Natural gas can be fed as power fuel to the internal combustion engine 25 by way of the fuel pipe 25. Hydrogen H2 as a reaction gas in the fuel cell 22 can alternatively be used as an alternative energy store.

[0034] FIG. 3 is flowchart of the method for operating a watercraft 1, 2. The method comprise arranging an electrical system 3, 4, 5, 6, 7, 15, 21, 22 within a space of the watercraft 1, 2, as indicated in step 310. Next, the space 8, 18 is filled with an atmosphere 20, as indicated in step 320.

[0035] Thus, while there have been shown, described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/ore method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures method steps and/or elements shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.