Pressureless water tank for operation in an aircraft, aircraft section and aircraft having a water tank

Patent metadata

Field	Value
Publication number	US-12434906-B2
Application number	US-202318239266-A
Country	US
Kind code	B2
Filing date	Aug 29, 2023
Priority date	Sep 2, 2022
Publication date	Oct 7, 2025
Grant date	Oct 7, 2025

Abstract

A water tank for operation in an aircraft includes a rigid tank shell, and a pressure compensation mechanism to equalize a pressure inside of the rigid tank shell with an environment. The pressure compensation mechanism includes a shutoff member to move between a closed position, a first open position allowing air to enter the rigid tank shell and a second open position allowing air to leave the rigid tank shell.

First claim

The invention claimed is:

1. A water tank for an aircraft, the water tank comprising:
a rigid tank shell; and
a pressure compensation mechanism configured to equalize a pressure inside of the rigid tank shell with an environment,
the pressure compensation mechanism comprising a shutoff member in a form of a flap that is pivotable about a hinge that connects the flap to the rigid tank shell, wherein the flap is configured to move between:
a closed position;
a first open position, which allows air to enter the rigid tank shell from the environment; and
a second open position, which allows air to leave the rigid tank shell and flow into the environment;
wherein, when the flap is in the first open position, the flap is opened inwardly, into the rigid tank shell, and, when the flap is in the second open position, the flap is opened outwardly, extending out of the rigid tank shell, such that a direction of movement of the flap from the closed position to the first open position is opposite a direction of movement of the flap from the closed position to the second open position; and
wherein, when the flap is in the first open position, the flap is positioned with a first degree of aperture and, when the flap is in the second open position, the flap is positioned with a second degree of aperture, which is larger than the first degree of aperture.

2. The water tank of claim 1 , wherein the flap is hingedly attached to the rigid tank shell directly and only on one side of the flap.

3. The water tank of claim 1 , wherein the pressure compensation mechanism comprises an air filter arranged to cover an opening evolving when the shutoff member moves from the closed position to the first open position.

4. The water tank of claim 1 , comprising:
a controller configured to receive a status signal from the pressure compensation mechanism,
wherein the pressure compensation mechanism is configured to generate and transmit the status signal indicating a position of the shutoff member.

5. The water tank of claim 4 , wherein:
the controller is configured to send a control signal to the pressure compensation mechanism; and
the pressure compensation mechanism is configured to receive the control signal and to move the shutoff member into a position corresponding to the control signal.

6. The water tank of claim 1 , wherein the pressure compensation mechanism further comprises a rupture disc configured to rupture when a pressure difference between the interior and a surrounding environment of the rigid tank shell exceeds a threshold value.

7. The water tank of claim 1 , comprising at least one water level sensor configured to measure a water level in the rigid tank shell and to transmit a water level signal.

8. The water tank of claim 1 , comprising a pump configured to pump water from inside the rigid tank shell to a water supply line.

9. The water tank of claim 1 , comprising:
an overflow port connected to an overflow line and configured to release water from the rigid tank shell when a water level in inside the rigid tank shell exceeds a threshold,
wherein the overflow port fluidly connects the overflow line with a housing of the pressure compensation mechanism.

10. The water tank of claim 9 , wherein the overflow port is configured to release air from inside the rigid tank shell when the air inside the rigid tank shell exceeds a threshold pressure.

11. The water tank of claim 1 , comprising at least one actuator configured to move the shutoff member between the closed position and the first open position and or between the closed position and the second open position.

12. An aircraft section comprising:
at least one tank according to claim 1 ; and
a water consumer fluidly connected with the at least one tank and configured to receive water from the at least one tank.

13. The aircraft section according to claim 12 , comprising:
a water connection configured to be connected to a water supply; and
a fill valve configured to open and close a fluid connection between the water connection and the rigid tank shell.

14. An aircraft comprising at least one tank according to claim 1 .

15. An aircraft comprising at least one aircraft section according to claim 12 .

16. A water tank for an aircraft, the water tank comprising:
a rigid tank shell; and
a pressure compensation mechanism configured to equalize a pressure inside of the rigid tank shell with an environment,
the pressure compensation mechanism comprising a shutoff member in a form of a diaphragm that is configured to control a size of an opening in the rigid tank shell, wherein the diaphragm has, for controlling whether the opening is open or closed, an aperture that is adjustable between:
a closed position, in which the opening is closed;
a first open position, in which the aperture has a first size for allowing air to enter the rigid tank shell from the environment; and
a second open position, in which the aperture has a second size for allowing air to leave the rigid tank shell and flow into the environment;
wherein the second size of the aperture is larger than the first size of the aperture;

wherein the shutoff member comprises a filter configured to prevent passage of contaminants and particulate matter from the environment into the rigid tank shell;
wherein the filter has an outer diameter that is smaller than an outer diameter of the diaphragm; and
wherein an outer diameter of the aperture, when the aperture is the first size, is a same as the outer diameter of the filter, such that all of the air passing from the environment into the rigid tank shell must pass through the filter when the aperture is the first size.

17. The water tank of claim 16 , wherein the second size of the aperture is larger than the outer diameter of the filter, such that, when the aperture is the second size, a concentric annular passage is formed around an outer perimeter of the filter to allow a portion of the air passing from the rigid tank shell into the environment to bypass the filter.

18. A water tank for an aircraft, the water tank comprising:
a rigid tank shell; and
a pressure compensation mechanism configured to equalize a pressure inside of the rigid tank shell with an environment,
the pressure compensation mechanism comprising a shutoff member in a form of a flap that is pivotable about a hinge that connects the flap to the rigid tank shell, wherein the flap is configured to move between:
a closed position; and
a second open position, which allows air to leave the rigid tank shell and flow into the environment;

wherein the shutoff member comprises a diaphragm arranged in or on the flap, the diaphragm having an aperture that is adjustable between the closed position and a first open position, which allows air to enter the rigid tank shell from the environment through the aperture; and
wherein, when the flap is in the second open position, the flap is opened outwardly, extending out of the rigid tank shell.

19. The water tank of claim 18 , wherein:
the shutoff member comprises a filter configured to prevent passage of contaminants and particulate matter from the environment into the rigid tank shell when the aperture of the diaphragm is in the first open position; and
the filter is positioned relative to the aperture such that, when the diaphragm is adjusted to be in the first open position, air flowing into the rigid tank shell through the aperture also passes through the filter.

Assignees

• Airbus Operations Gmbh

Inventors

• Schneider Frank
• Albers Frederik

Classifications

• F16K17/19

  Equalising valves predominantly for tanks {(when combined with safety valve by change of position F16K17/36)} · CPC title

• F16K3/03

  with a closure member in the form of an iris-diaphragm · CPC title

• F16K2200/202

  one valve arranged inside of the valve member of a second valve, e.g. nested valve members · CPC title

• E03B11/02

  for domestic or like local water supply · CPC title

• B64D11/0007

  Devices specially adapted for food or beverage distribution services · CPC title