Compact check valve for aircraft galley plumbing system

Patent metadata

Field	Value
Publication number	US-9469402-B2
Application number	US-201514676062-A
Country	US
Kind code	B2
Filing date	Apr 1, 2015
Priority date	May 22, 2012
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

A check valve for an aircraft galley plumbing system having a valve body including an inlet for a potable water supply line, and first and second outlet ports leading to a distribution manifold. In a preferred embodiment, quick disconnects that include reverse flow inhibitors seal the valve's output ports. A vertical channel extends through the valve body for draining water through the valve, which is coupled to a pressure line connection port that exerts pressure from the aircraft's pressure system. A piston reciprocating across the vertical channel and biased by a spring is in fluid communication with the pressure line connection port, such that when water pressure is introduced from a pressure line to the connection port of sufficient pressure to collapse said spring, the piston blocks said channel, and when the water pressure is insufficient to collapse said spring then the piston retracts to open said channel.

First claim

I claim:

1. A four-way check valve for an aircraft galley plumbing system, comprising:
a valve body including an inlet on an upper surface for a potable water supply line;
first and second outlet ports extending perpendicular to the inlet, including quick disconnect fittings with reverse flow inhibitors to automatically seal the valve when no conduit is connected to the outlet ports, the reverse flow inhibitors managed by a spring and a detector for detecting the presence of a conduit;
a pressure line connection port that communicates a fluid pressure to the four way check valve;
a fluid outlet opposed to the inlet at a lower surface of the valve body; and
a piston actuated by the fluid pressure, whereby the piston transversely occludes the fluid outlet when a pressure overcomes a first piston spring, the piston including a poppet therein that is biased by a second spring, and the piston spring and the piston poppet spring are concentrically aligned.

2. The check valve for an aircraft galley plumbing system of claim 1 , wherein the reverse flow inhibitors are poppets.

3. The check valve for an aircraft galley plumbing system of claim 1 , wherein the first and second outlet ports are diametrically opposed to each other.

4. A four-way check valve for an aircraft galley plumbing system, comprising:
a valve body including an inlet on an upper surface for a potable water supply line;
first and second outlet ports extending perpendicular to the inlet, including quick disconnect fittings with reverse flow inhibitors to automatically seal the valve when no conduit is connected to the outlet ports, the reverse flow inhibitors managed by a spring and a detector for detecting the presence of a conduit;
a pressure line connection port that communicates a fluid pressure to the four way check valve;
a fluid outlet opposed to the inlet at a lower surface of the valve body; and
a piston actuated by the fluid pressure, whereby the piston transversely occludes the fluid outlet when a pressure overcomes a first piston spring, the piston including a poppet therein that is biased by a second spring, wherein the poppet spring is mounted inside an annular recess.

Assignees

• Be Aerospace Inc

Inventors

• Burd Peter John Leslie

Classifications

• Y10T137/2663

  Pressure responsive · CPC title

• Y10T137/2617

  Bypass or relief valve biased open · CPC title

• B64D11/02 Primary

  Toilet fittings · CPC title

• B64D11/04

  Galleys · CPC title

• Y10T137/87877

  Single inlet with multiple distinctly valved outlets · CPC title