Grey water interface for high flow applications in vacuum systems

US9448563B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9448563-B2
Application numberUS-201414284726-A
CountryUS
Kind codeB2
Filing dateMay 22, 2014
Priority dateMay 22, 2013
Publication dateSep 20, 2016
Grant dateSep 20, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Embodiments of the present invention relate generally to a flow control unit for controlling liquid flow in a vacuum waste system. In one embodiment, the flow control unit provides a series of valves that direct liquid flow. The unit may also have an intermediate transfer tube that holds a portion of the liquid to be directed, prior to delivery of the liquid to left and right transfer tubes. In one embodiment, the unit may be installed on board a passenger transport vehicle. A particularly beneficial use of the flow control unit is on a private aircraft for use as a shower control unit.

First claim

Opening claim text (preview).

What is claimed is: 1. A flow control unit for controlling liquid flow in a vacuum waste system, comprising: (a) an incoming liquid line; (b) an intermediate transfer tube; (c) a left transfer tube comprising an upper left flush valve and a lower left flush valve; and (d) a right transfer tube comprising an upper right flush valve and a lower right flush valve, wherein the upper left and upper right valves are configured to control liquid flow between the intermediate transfer tube and the left and right transfer tubes, and wherein the left and right lower valves are configured to control liquid flow between the left and right transfer tubes and one or more waste tanks of the vacuum waste system. 2. The flow control unit of claim 1 , further comprising: (e) a first interface between the left transfer tube and the vacuum waste system; and (f) a second interface between the right transfer tube and the vacuum waste system. 3. The flow control unit of claim 1 , wherein the liquid flow comprises grey water from a shower on-board a passenger transport vehicle. 4. The flow control unit of claim 1 , wherein the incoming liquid line is fluidly connected to a liquid intake portion. 5. The flow control unit of claim 4 , wherein the liquid intake portion comprises a shower drain. 6. The flow control unit of claim 1 , wherein the intermediate transfer tube receives fluid flow from the incoming liquid line and is positioned upstream of the left and right transfer tubes. 7. The flow control unit of claim 1 , wherein liquid flows into the left transfer tube when the upper left flush valve is open. 8. The flow control unit of claim 1 , wherein liquid flows into the right transfer tube when the upper right flush valve is open. 9. The flow control unit of claim 1 , wherein liquid flows into the vacuum waste system when one or both of the lower left flush valve or the lower right flush valve is open. 10. The flow control unit of claim 1 , further comprising a timer for controlling opening and closing of the upper left flush valve, the lower left flush valve, the upper right flush valve, and the lower right flush valve. 11. The flow control unit of claim 1 , further comprising a level sensor to control opening and closing of the upper left flush valve, the lower left flush valve, the upper right flush valve, and the lower right flush valve. 12. The flow control unit of claim 1 , wherein the vacuum system comprises a left trunk line and a right trunk line, and wherein the left transfer tube joins the left trunk line at a first interface, and wherein the right transfer tube joins the right trunk line at a second interface. 13. The flow control unit of claim 1 , wherein the flow control unit is installed on board a passenger transport aircraft. 14. The flow control unit of claim 13 , wherein the aircraft comprises two waste tanks for receiving downstream liquid flow, one waste tank on either side of the aircraft. 15. The flow control unit of claim 1 , wherein each of the valves comprises a valve controller. 16. A flow control unit for controlling liquid flow in a vacuum waste system, comprising: (a) a liquid intake portion; (b) the liquid intake portion in fluid communication with an intermediate transfer tube; (c) a left transfer tube fluidly separated from the intermediate transfer tube via an upper left flush valve, and further comprising a lower left flush valve; (d) a right transfer tube fluidly separated from the intermediate transfer tube via an upper right flush valve, and further comprising a lower right flush valve; (e) a left interface between the left transfer tube and the vacuum waste system, wherein liquid in the left transfer tube flows into a left vacuum waste system trunk line upon application of vacuum; and (f) a right interface between the right transfer tube and the vacuum waste system, wherein liquid in the right transfer tube flows into a right vacuum waste system trunk line upon application of vacuum. 17. A method for controlling a valve system sequence for a flow control unit comprising: (a) receiving input that a water generating unit activated; (b) receiving water flow into a liquid intake portion; (c) directing the water flow into an intermediate transfer tube; (d) causing an upper valve on a first side of the flow control unit to be open while two lower valves are closed; (e) after water fills a transfer tube that corresponds to the open upper valve and once the transfer tube is at a specified percentage full or at a specified time, closing the upper valve on the first side and opening an upper valve on a second side to allow water to enter a corresponding transfer tube on the second side; (f) sending a vacuum request and opening a lower valve on the first side; (g) allowing vacuum to pull water from the transfer tube on the first side to a first side waste tank; (h) once the transfer tube corresponding to the upper valve on the second side is at a specified percentage full or at a specified time full, closing the upper valve on the second side and reopening the upper valve on the first side; (i) opening a lower valve on the second to allow vacuum to pull water from the transfer tube on the second side to a second side waste tank; and (j) causing the sequence to repeat for a duration of water input. 18. The method of claim 17 , wherein each of the valves is operated by a controller. 19. The method of claim 17 , wherein one or more controllers communicate for synchronization of the valves, in the event of valve failure, for re-set timing, or any combination thereof.

Assignees

Inventors

Classifications

  • Processes · CPC title

  • Repeating cycle · CPC title

  • G05D7/0641Primary

    using a plurality of throttling means (G05D7/067 takes precedence) · CPC title

  • B64D11/02Primary

    Toilet fittings · CPC title

  • automatically actuating supply or draining valves · CPC title

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What does patent US9448563B2 cover?
Embodiments of the present invention relate generally to a flow control unit for controlling liquid flow in a vacuum waste system. In one embodiment, the flow control unit provides a series of valves that direct liquid flow. The unit may also have an intermediate transfer tube that holds a portion of the liquid to be directed, prior to delivery of the liquid to left and right transfer tubes. In…
Who is the assignee on this patent?
Mag Aerospace Ind Llc
What technology area does this patent fall under?
Primary CPC classification G05D7/0641. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Sep 20 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).