Waste system pressure management system

Patent metadata

Field	Value
Publication number	US-10994845-B2
Application number	US-201916433341-A
Country	US
Kind code	B2
Filing date	Jun 6, 2019
Priority date	Jun 6, 2019
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

A system for waste system pressure management is disclosed. In one or more embodiments, the system includes an electronically controlled valve and a controller communicatively coupled to the electronically controlled valve. The electronically controlled valve is coupled to a suction path of an aircraft waste system. The controller is configured to determine a pressure differential between an aircraft cabin and a vacuum source for the suction path. The controller is further configured to generate one or more signals to actuate the electronically controlled valve from a first position to a second position to regulate a pressure in the suction path when the pressure differential between the aircraft cabin and the vacuum source exceeds a threshold pressure differential. In embodiments, the electronically controlled valve is configured to allow more airflow through the electronically controlled valve in the second position than in the first position.

First claim

What is claimed is:

1. A system for waste system pressure management, comprising:
an electronically controlled valve coupled to a suction path of an aircraft waste system; and
a controller communicatively coupled to the electronically controlled valve, the controller configured to:
determine a pressure differential between an aircraft cabin and a vacuum source for the suction path; and

generate one or more signals to actuate the electronically controlled valve from a first position to a second position to regulate a pressure in the suction path when the pressure differential between the aircraft cabin and the vacuum source exceeds a threshold pressure differential, wherein the electronically controlled valve is configured to allow more airflow through the electronically controlled valve in the second position than in the first position, wherein the electronically controlled valve is coupled to a portion of the suction path between a waste tank and the vacuum source.

2. The system of claim 1 , wherein the electronically controlled valve is also coupled to a flow path that directs air from the aircraft cabin into the suction path when the electronically controlled valve is in the second position.

3. The system of claim 2 , further comprising an end fitting coupled to the flow path to reduce noise generated by airflow through the electronically controlled valve.

4. The system of claim 1 , wherein the vacuum source comprises a connection to atmosphere outside the aircraft cabin.

5. The system of claim 4 , further comprising an additional vacuum source, wherein the additional vacuum source comprises a vacuum blower.

6. The system of claim 5 , wherein the controller is configured to maintain the electronically controlled valve in a closed position when the aircraft cabin is at an altitude requiring operation of the vacuum blower.

7. The system of claim 5 , wherein the electronically controlled valve is coupled to a portion of the suction path between a waste tank and the vacuum blower or between the vacuum blower and the connection to the atmosphere outside the aircraft cabin.

8. An aircraft waste system, comprising:
a toilet disposed within an aircraft cabin;
a waste tank;
a vacuum source;
an additional vacuum source, wherein the additional vacuum source comprises a vacuum blower;
a suction path coupling the toilet, the waste tank, and the vacuum source;
an electronically controlled valve coupled to the suction path; and
a controller communicatively coupled to the electronically controlled valve, the controller configured to:
determine a pressure differential between the aircraft cabin and the vacuum source; and

generate one or more signals to actuate the electronically controlled valve from a first position to a second position to regulate a pressure in the suction path when the pressure differential between the aircraft cabin and the vacuum source exceeds a threshold pressure differential, wherein the electronically controlled valve is configured to allow more airflow through the electronically controlled valve in the second position than in the first position, wherein the controller is configured to maintain the electronically controlled valve in a closed position when the aircraft cabin is at an altitude requiring operation of the vacuum blower.

9. The aircraft waste system of claim 8 , wherein the electronically controlled valve is coupled to a portion of the suction path between the waste tank and the vacuum source.

10. The aircraft waste system of claim 8 , wherein the electronically controlled valve is also coupled to a flow path that directs air from the aircraft cabin into the suction path when the electronically controlled valve is in the second position.

11. The aircraft waste system of claim 10 , further comprising an end fitting coupled to the flow path to reduce noise generated by airflow through the electronically controlled valve.

12. The aircraft waste system of claim 8 , wherein the vacuum source comprises a connection to atmosphere outside the aircraft cabin.

13. The aircraft waste system of claim 8 , wherein the electronically controlled valve is coupled to a portion of the suction path between the waste tank and the vacuum blower or between the vacuum blower and the connection to the atmosphere outside the aircraft cabin.

14. An aircraft waste system, comprising:
a toilet disposed within an aircraft cabin;
a waste tank;
a vacuum source;
a suction path coupling the toilet, the waste tank, and the vacuum source;
an electronically controlled valve coupled to the suction path; and
a controller communicatively coupled to the electronically controlled valve, the controller configured to:
determine a pressure differential between the aircraft cabin and the vacuum source; and
generate one or more signals to actuate the electronically controlled valve from a first position to a second position to regulate a pressure in the suction path when the pressure differential between the aircraft cabin and the vacuum source exceeds a threshold pressure differential, wherein the electronically controlled valve is configured to allow more airflow through the electronically controlled valve in the second position than in the first position, wherein the electronically controlled valve is coupled to a portion of the suction path between the waste tank and the vacuum source.

Assignees

• Be Aerospace Inc

Inventors

• Forster Charles F
• Hashberger Frank E

Classifications

• B64D11/00

  Passenger or crew accommodation; Flight-deck installations not otherwise provided for · CPC title

• B64D47/00

  Equipment not otherwise provided for · CPC title

• B64D11/02 Primary

  Toilet fittings · CPC title

• E03F1/006

  Pneumatic sewage disposal systems; accessories specially adapted therefore · CPC title