Method and arrangement for sealing a propeller shaft located under water

Patent metadata

Field	Value
Publication number	US-11702182-B2
Application number	US-202217650467-A
Country	US
Kind code	B2
Filing date	Feb 9, 2022
Priority date	Feb 16, 2021
Publication date	Jul 18, 2023
Grant date	Jul 18, 2023

Abstract

A method and an arrangement for sealing a propeller shaft located under water. The propeller shaft is arranged at a pod of a ship and an air chamber is provided circumferentially around the propeller shaft. The method includes supplying compressed air from a compressed air source to the air chamber, discharging compressed air from the air chamber in an air return line and colleting liquid present in the compressed air discharged from the air chamber in an intermediate leakage tank that is provided in the air return line. The method includes closing the air return line upstream of the intermediate leakage tank, and supplying compressed air to the intermediate leakage tank to effect flowing of liquid present in the intermediate leakage tank to a leakage tank.

First claim

The invention claimed is:

1. A method for sealing a propeller shaft located under water, wherein the propeller shaft is arranged at a pod that is suspended at a hull of a ship and wherein an air chamber is provided circumferentially around the propeller shaft, the method comprising
supplying compressed air from a compressed air source in an air supply line to the air chamber,
discharging compressed air from the air chamber in an air return line and out of the air return line, and
colleting liquid present in the compressed air discharged from the air chamber in an intermediate leakage tank that is provided in the air return line within a
pod housing of the pod, wherein
by closing the air return line upstream of the intermediate leakage tank, and
by supplying compressed air to the intermediate leakage tank to effect flowing of liquid present in the intermediate leakage tank to a leakage tank.

2. The method according to claim 1 , wherein
by closing the air return line downstream of the intermediate leakage tank in connection with closing the air return line.

3. The method according to claim 2 , wherein
by supplying said compressed air to the intermediate leakage tank by supplying compressed air to an upstream end of a connecting air line from the air supply line, and by supplying compressed air from a downstream end the connecting air line to the air return line at a point of the air return line downstream of the intermediate leakage tank, and by supplying compressed air in the air return line to the intermediate leakage tank to effect said flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

4. The method according to claim 3 , wherein
by providing a first valve in the form of a check valve in the air return line upstream of the intermediate leakage tank,
by supplying compressed air from the compressed air source to the air chamber through a first pressure regulator in the air supply line,
by supplying compressed air in the connecting air line through a third valve and through a second pressure regulator configured to provide a higher pressure than the first pressure regulator, and
by said closing of the air return line upstream of the intermediate leakage tank is affected by a difference between the pressure provided by the first pressure regulator and the pressure provided by the second pressure regulator causing the first valve in the form of a check valve to close.

5. The method according to claim 4 , wherein
by sending a signal from a pressure sensor functionally connected to the air supply line to the third valve provided in the connecting air line and triggering an alarm and/or closing the third valve provided in the connecting air line if the pressure in the air supply line exceeds a predetermined threshold value when the third valve provided in the connecting air line is open.

6. An arrangement for sealing a propeller shaft located under water, wherein the propeller shaft is arranged at a pod that is suspended at a hull of a ship comprising:
an air chamber that is provided circumferentially around the propeller shaft,
an air supply line configured to supply compressed air from a compressed air source to the air chamber,
an air return line configured to discharge compressed air from the air chamber and out of the air return line, and
an intermediate leakage tank for collecting liquid present in the air is provided in the air return line, wherein the intermediate leakage tank being provided within a pod housing of the pod,
by a drainage arrangement including:
a first valve in the air return line upstream of the intermediate leakage tank,
a leakage tank in fluid connection with the intermediate leakage tank by means of a connecting liquid line, and
a connecting air line in fluid connection with the intermediate leakage tank,
the drainage arrangement configured to close the first valve in the air return line, to supply compressed air in the connecting air line to the intermediate leakage tank to effect flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

7. The arrangement according to claim 6 , wherein the drainage arrangement comprises a second valve in the air return line downstream of the intermediate leakage tank, and the drainage arrangement being configured to close the second valve in the air return line in connection with the closing of the first valve in the air return line.

8. The arrangement according to claim 7 , wherein the connecting air line being in fluid connection with the intermediate leakage tank so that an upstream end of the connecting air line is in fluid connection with the air supply line and so that a downstream end of the connection air line is in fluid connection with the air return line at a point upstream of the second valve in the air return line and downstream of the intermediate leakage tank, and the drainage arrangement being configured to supply said compressed air to the upstream end of the connecting air line from the compressed air source that is configured to supply compressed air to the air chamber that is provided circumferentially around the propeller shaft, and from downstream end of the connecting air line to the air return line and in the air return line to the intermediate leakage tank leakage to effect said flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

9. The arrangement according to claim 8 , wherein the connecting air line being provided with a third valve, and the drainage arrangement being configured to open the third valve provided in the connecting air line to supply compressed air to the intermediate leakage tank to effect flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

10. The arrangement according to claim 8 , including:
a first pressure regulator in the air supply line, and
the connecting air line being provided with a third valve and with a second pressure regulator configured to provide a higher pressure than the first pressure regulator, and
the drainage arrangement being configured to open the third valve provided in the connecting air line to supply compressed air through the second pressure regulator in the connecting air line and in the air return line into the intermediate leakage tank to effect flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

11. The arrangement according to claim 8 , including:
a first pressure regulator in the air supply line,
the connecting air line being provided with a third valve and with a second pressure regulator configured to provide a higher pressure than the first pressure regulator,
the first valve in the air return line upstream of the intermediate leakage tank being in the form of a check valve, and
the drainage arrangement being configured to open the third valve provided in the connecting air line to supply compressed air through the second pressure regulator in the connecting air line and in the air return line into the intermediate leakage tank to effect closing of the first valve and to effect flowing of liquid present in the intermediate leakage tank to the leakage tank in the connecting liquid line.

12. The arrangement according to claim 9 , including:
connecting a pressure sensor to the air supply line, and
sending a signal from the pressure sensor to the third valve provided in the connecting air line of the drainage circuit arrangement and triggering an alarm and closing the third valve provided in the connecting air line of the drainag

Assignees

• Abb Schweiz Ag

Inventors

• Vähätalo Veikko
• Laine Jukka
• Maja Otto
• Niska Toni

Classifications

• B63H23/321 Primary

  Bearings or seals specially adapted for propeller shafts · CPC title

• B63H2023/327

  Sealings specially adapted for propeller shafts or stern tubes · CPC title

• F16N7/02

  with gravity feed or drip lubrication · CPC title

• F16N21/00

  Conduits; Junctions (in general F16L); Fittings for lubrication apertures · CPC title

• B63H2005/1254

  Podded azimuthing thrusters, i.e. podded thruster units arranged inboard for rotation about vertical axis · CPC title