Granted Patent B2

US 12,263,913 · App. 17/918,486 · Granted Apr 1, 2025

Inventors: Jari Keinaenen (Brugg, CH); Jean-Francois Tissot (Bergheim, FR)

Assignee: ACCELLERON SWITZERLAND LTD.

B63B1/38F02B37/005F02B37/183F02B39/10B63B2001/385B63B2001/387

Abstract

Claims (30)

1. An air supply apparatus for a ship, comprising:

a first turbocharger having a first compressor and a first turbine being drivable by exhaust gas provided from one or more engines, wherein the first compressor is coupled to the first turbine via a transmission between the first compressor and the first turbine, said transmission having a variable transmission ratio such that a speed of the first compressor is changeable with respect to a speed of the first turbine; and

wherein the first compressor supplies air to generate bubbles under a hull of the ship to reduce water-hull friction of the ship.

2. The air supply apparatus of claim 1 , wherein the transmission is a mechanical, electrical, pneumatic or hydraulic transmission.

3. The air supply apparatus of claim 1 , further comprising a second turbine in parallel to the first turbine, the first turbine and the second turbine being coupled to the first compressor via the transmission.

4. The air supply apparatus of claim 1 , wherein the transmission comprises a generator and an electric motor.

5. The air supply apparatus of claim 1 , further comprising a second turbocharger having a second compressor and a second turbine, the second turbine being drivable by at least one of exhaust gas provided from the one or more engines and exhaust gas provided from the first turbine, the second compressor being coupled to the second turbine via a further transmission configured for changing a speed of the second compressor.

6. The air supply apparatus of claim 5 , wherein the further transmission is a mechanical, electrical, pneumatic or hydraulic transmission.

7. The air supply apparatus of claim 1 , further comprising a third turbocharger having a third compressor and a third turbine being connected with an exhaust gas receiver of the one or more engines via a first exhaust gas pipe, the first exhaust gas pipe being connected to a flow controller for controlling an exhaust gas flow provided from the exhaust gas receiver to the third turbine, particularly the flow controller being provided in a first bypass piping bypassing the third turbine.

8. The air supply apparatus of claim 7 , the first turbine being connected with the third turbine via a second exhaust gas pipe, the second exhaust gas pipe being connected to a bypass valve for controlling an exhaust gas flow provided from the third turbine to the first turbine.

9. The air supply apparatus of claim 7 , the third compressor being connected with an air receiver of the one or more engines via a first air supply pipe.

10. A ship comprising an air supply apparatus, the air supply apparatus comprising:

a first turbocharger having a first compressor and a first turbine being drivable by exhaust gas provided from one or more engines, wherein the first compressor is coupled to the first turbine via a transmission between the first compressor and the first turbine, said transmission having a variable transmission ratio such that a speed of the first compressor is changeable with respect to a speed of the first turbine; and

wherein the first compressor supplies air to generate bubbles under a hull of the ship to reduce water-hull friction of the ship lubrication device.

11. A method of supplying air for air lubrication of a hull of a ship, comprising:

driving a first turbocharger by using exhaust gas from one or more engines;

changing a speed of a first compressor with respect to a first turbine of the first turbocharger by using a transmission coupled to the first turbine and to the first compressor of the first turbocharger, said transmission between the first turbine and the first compressor, wherein the transmission has a variable transmission ratio such that the speed of the first compressor is changeable with respect to a speed of the first turbine; and

supplying air from the first compressor of the first turbocharger to generate bubbles under a hull of the ship to reduce water-hull friction of the ship.

12. The method of claim 11 , wherein changing the speed of the first compressor comprises using a second turbine in parallel to the first turbine, the first turbine and the second turbine being coupled to the first compressor via the transmission.

13. The method of claim 11 , further comprising:

driving a second turbocharger by at least one of using exhaust gas from the one or more engines and using exhaust from the first turbine, the second turbocharger having a second compressor being coupled to a second turbine via a further transmission configured for changing a speed of the second compressor,

changing a speed of the second compressor by using the further transmission, and

supplying air from the second compressor of the second turbocharger to generate the bubbles under the hull of the ship to reduce the water-hull friction of the ship.

14. The method of claim 11 , further comprising controlling an amount of air provided to generate the bubbles under the hull of the ship to reduce the water-hull friction of the ship by controlling a rotational speed of the first turbocharger by controlling an exhaust gas flow provided to a third turbine of a third turbocharger being connected with an exhaust gas receiver of the one or more engines by using a flow controller.

15. The method of claim 11 , further comprising controlling an amount of air provided to generate the bubbles under the hull of the ship to reduce the water-hull friction of the ship by controlling a rotational speed of the first turbocharger by controlling an exhaust gas flow provided to the first turbine by using a bypass valve, the bypass valve being provided in a second bypass piping bypassing the first turbine.

16. The air supply apparatus of claim 7 , wherein the flow controller is provided in a first bypass piping bypassing the third turbine.

17. The air supple apparatus of claim 8 , wherein the bypass valve is provided in a second bypass piping bypassing the first turbine.

18. The air supple apparatus of claim 9 , wherein the first air supply pipe comprises a charge air cooler.

19. The air supply apparatus of claim 1 , wherein the first turbocharger is a secondary turbine-compressor pair provided in addition to a turbocharger for charging the one or more engines.

20. The method of claim 14 , wherein the flow controller is provided in a first bypass piping bypassing the third turbine.

Assignments (2)

Priority Claims (1)

Continuity (1)

References Cited (14)

Cited By (1)

US 1,091,803