System and method for heating up water for a consumer unit in an aircraft

Patent metadata

Field	Value
Publication number	US-11946668-B2
Application number	US-202217848997-A
Country	US
Kind code	B2
Filing date	Jun 24, 2022
Priority date	Jun 25, 2021
Publication date	Apr 2, 2024
Grant date	Apr 2, 2024

Abstract

A system for heating up water for a consumer unit in an aircraft, having a water reservoir and a control unit. The water reservoir has a heating device to heat water held in the water reservoir to a consumer temperature. The control unit controls the heating device so water in the water reservoir is automatically heated to or above a disinfection temperature at which germ formation in the water reservoir is eliminated or suppressed, and a temperature of the water in the water reservoir is maintained at or above the disinfection temperature for a disinfection period, the heating to the disinfection temperature being effected only during flight phases or portions of flight phases of the aircraft during which use of the consumer unit by a user is not to be expected. A corresponding method and an aircraft having such a system are disclosed.

First claim

The invention claimed is:

1. A system for heating water for a consumer in an aircraft, the system comprising:
a water reservoir comprising a heater configured to heat water held in the water reservoir to a consumer temperature, so the water can be provided at the consumer temperature from the water reservoir to the consumer for immediate use; and
a controller configured to control the heater so the water held in the water reservoir is automatically heated to or above a disinfection temperature, which is a temperature at which germ formation in the water reservoir and on internal surfaces of the water reservoir is eliminated or suppressed by thermal treatment, the controller maintaining a temperature of the water in the water reservoir at or above the disinfection temperature for a disinfection period;
wherein the controller is configured to heat the water in the water reservoir to the disinfection temperature only during flight phases or portions of flight phases of the aircraft when a user is not expected to use the consumer.

2. The system according to claim 1 , the controller being configured to be connected to a data bus of the aircraft and to receive from the data bus a current flight phase of the aircraft.

3. The system according to claim 1 , wherein:
the consumer has a consumer valve that is configured so, when open, the water can be drawn from the water reservoir; and
the controller is configured to control an opening of the consumer valve so the water from the water reservoir, heated to disinfection temperature, is drawn from the water reservoir through the consumer valve, so the water can be provided at the consumer temperature from the water reservoir as soon as use of the consumer by the user is expected.

4. The system according to claim 1 , comprising an infeed valve and an overflow, the infeed valve being configured, when open, to enable the water in the water reservoir to be replenished from a central water tank into the water reservoir, and the overflow being configured so the water can flow out of the water reservoir via the overflow;
wherein the controller is configured to control the infeed valve to open, so the water, heated to the disinfection temperature, flows out of the water reservoir through the overflow, so the water can be provided at the consumer temperature from the water reservoir as soon as use of the consumer by the user is expected.

5. The system according to claim 1 , wherein the controller is configured to heat the water in the water reservoir to disinfection temperature only when one or more cabin data assume predetermined values.

6. The system according to claim 5 , wherein the consumer is a washbasin or shower in a washroom, and the one or more cabin data comprises a usage status of the washroom and/or a status of a presence sensor that senses a presence of the user in the washroom.

7. The system according to claim 1 , comprising a flow disinfection unit configured to disinfect the water flowing out of the water reservoir;
wherein the controller is configured to deactivate the flow disinfection unit when the water held in the water reservoir is heated to the disinfection temperature.

8. A method for heating up water for a consumer in an aircraft, the method comprising:
providing a water reservoir within the aircraft, the water reservoir comprising a heater;
providing water within the water reservoir;
heating, using the heater, the water within the water reservoir to a consumer temperature;
providing the water at the consumer temperature from the water reservoir to the consumer for immediate use; and
automatically heating the water held in the water reservoir to a disinfection temperature, which is a temperature at which germ formation in the water reservoir and on internal surfaces of the water reservoir is eliminated or suppressed by thermal treatment, a temperature of the water in the water reservoir being maintained at or above the disinfection temperature for a disinfection period;
wherein the water contained in the water reservoir is heated to the disinfection temperature only during flight phases or portions of flight phases of the aircraft when a user is not expected to use the consumer.

9. The method according to claim 8 , comprising obtaining a current flight phase of the aircraft from a data bus of the aircraft.

10. The method according to claim 8 , wherein:
the consumer has a consumer valve, the consumer valve being configured such that, when open, the water can be drawn from the water reservoir;
the method comprising:
opening the consumer valve so the water from the water reservoir, heated to disinfection temperature, is drawn from the water reservoir through the consumer valve, so the water can be provided at the consumer temperature from the water reservoir as soon as use of the consumer by the user is expected.

11. The method according to claim 8 , wherein:
opening of an infeed valve enables the water in the water reservoir to be replenished from a central water tank into the water reservoir and water is able to flow out of the water reservoir via an overflow; and
the infeed valve being opened so the water, heated to the disinfection temperature, flows out of the water reservoir, through the overflow, so the water can be provided at the consumer temperature from the water reservoir as soon as use of the consumer by the user is expected.

12. The method according to claim 8 , wherein the water in the water reservoir is heated to disinfection temperature only when one or more cabin data assume predetermined values.

13. The method according to claim 12 , wherein the consumer unit is a washbasin or shower in a washroom, and the one or more cabin data comprises a usage status of the washroom and/or a status of a presence sensor that senses a presence of the user in the washroom.

14. The method according to claim 8 , wherein the water flowing out of the water reservoir is disinfected by a flow disinfection unit, the flow disinfection unit being deactivated when the water in the water reservoir is heated to the disinfection temperature.

15. An aircraft having a system according to claim 1 .

Assignees

• Airbus Operations Gmbh

Inventors

• Rempe Michael
• Albers Frederik
• Schneider Frank
• Schreiner Axel
• Lübbert Tim

Classifications

• F24H15/14 Primary

  Cleaning; Sterilising; Preventing contamination by bacteria or microorganisms, e.g. by replacing fluid in tanks or conduits · CPC title

• B64D11/02 Primary

  Toilet fittings · CPC title

• G05D23/1917

  using digital means · CPC title

• B64D11/04 Primary

  Galleys · CPC title

• F24H1/20

  with immersed heating elements, e.g. electric elements or furnace tubes · CPC title