Lavatory potable water system
To eliminate as many hoses and tubes as possible, reduce overall system size, weight and costs, the manifold system disclosed herein has been developed. The apparatus in some examples utilizes a unitary structure (solid cast) manifold to replace many of the hoses previously provided. Several versions/examples of this apparatus are disclosed herein such as a manifold system and an integrated water manifold wherein a mount for a hot water heater and/or water filter are integrated into the manifold body.
1. An Aircraft Lavatory Potable Water System comprising:
a. a unitary structure manifold body having;
i. a plurality of independent internal fluid conduits comprising a first fluid conduit and a second fluid conduit,
ii. a potable water inlet in fluid communication with the first fluid conduit,
iii. a water filter outlet in fluid communication with the first fluid conduit,
iv. a water filter inlet in fluid communication with the second fluid conduit,
v. a water heater outlet in fluid communication with the second fluid conduit,
vi. a cold water outlet in fluid communication with the second fluid conduit; and
b. a check valve mounted to the manifold body to allow one-way water flow from the second conduit to the first conduit during a purge of the system.
2. The manifold as recited in claim 1 further comprising: a shutoff valve in fluid communication between the potable water inlet and the first conduit.
3. The manifold as recited in claim 2 wherein the shutoff valve is a remotely operated valve.
4. The manifold as recited in claim 1 wherein the filter outlet comprises a filter housing mount directly coupled to the manifold body.
5. The manifold as recited in claim 1 further comprising: a toilet water flush outlet in fluid communication with the first fluid conduit.
6. The manifold as recited in claim 1 wherein the manifold body is formed by a process of injection molding.
7. The manifold as recited in claim 1 wherein the manifold body comprises fastening brackets attaching the manifold body to an aircraft fuselage.
8. The potable water system as recited in claim 1 further comprising: a water filter housing and a water filter therein in fluid communication between the water filter outlet and water filter inlet.
9. The manifold as recited in claim 1 wherein each of the a potable water inlet, water filter, water filter, water heater outlet, and cold water outlet comprises a hose coupling receiver.
10. The potable water system as recited in claim 9 further comprising: a hose coupling attached to each of the coupling receivers.
11. The manifold as recited in claim 1 further comprising a hot water reservoir formed as a unitary structure of the manifold body.