# US 2026/0062279 A1 · Pre-Warmed Potable Water System and Method for Aircraft Galley Appliance Water Heater > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2026/0062279 A1 - Document ID: US20260062279A1 - Status: Published application - Kind: A1 - Application number: 18/820,739 - Filed: 2024-08-30 - Published: 2026-03-05 - Earliest claimed: 2024-08-30 - Assignees: The Boeing Company - Applicants: The Boeing Company - Inventors: Andrew L. Pucker; Thomas Joseph Moran; Sami Movsesian - Web page: https://patentgrep.com/patent/US20260062279A1 ## CPC - B67D 1/0895: {Heating arrangements} - B64D 11/02: Toilet fittings - B64D 11/04: Galleys - B64D 47/00: Equipment not otherwise provided for - B67D: DISPENSING, DELIVERING OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR (cleaning pipes or tubes or systems of pipes or tubes B08B9/02; emptying or filling of bottles, jars, cans, casks, barrels, or similar containers, not otherwise provided for B67C; water supply E03; pipe systems F17D; domestic hot-water supply systems F24D; measuring volume, volume flow, mass flow or liquid level, metering by volume G01F; coin-freed or like apparatus G07F) - B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT ## Abstract Systems and methods for establishing a warmed potable water flow from an aircraft potable water supply with an ambient temperature absorbs and scavenges waste heat at a heat exchanger to pre-warm a potable water flow delivered to an aircraft galley appliance water heater, and to increase appliance water heating efficiency and to conserve electrical power for aircraft galley appliance water heater operation are disclosed. ## Claims ### Claim 1 An onboard aircraft system for pre-warming a potable water flow to an aircraft galley water heating appliance, the onboard aircraft system comprising: a potable water pathway comprising: a potable water supply comprising a volume of potable water in a potable water supply vessel, said potable water supply comprising a potable water supply initial temperature; a potable water flow line in communication with the potable water supply; a chilled air circuit, said chilled air circuit comprising an air chiller unit, said air chiller unit comprising an air chiller condenser, said air chiller condenser comprising an air chiller condenser air intake; a heat exchanger positioned proximate to the air chiller condenser intake, said heat exchanger in communication with the potable water flow line, said heat exchanger further in communication with the chilled air circuit, said heat exchanger comprising: a heat exchanger potable water flow intake and a heat exchanger warmed potable water flow outlet; a heat exchanger ambient air inlet and a heat exchanger cooled air outlet, said heat exchanger cooled air outlet positioned to deliver a cooled air flow from the heat exchanger to the air chiller condenser ambient air intake, said heat exchanger further configured to form a pre-warmed potable water flow; a pre-warmed potable water flow line in direct communication with the heat exchanger potable water flow outlet; an aircraft galley appliance comprising an aircraft galley appliance water heater, said aircraft galley appliance water heater in communication with the pre-warmed potable water flow line, said aircraft galley appliance water heater configured to further heat the pre-warmed potable water flow delivered to the aircraft galley appliance water heater via the pre-warmed potable water flow line; and a pre-warmed potable water storage vessel in communication with the pre-warmed potable water flow line, said pre-warmed potable water storage vessel further in communication with the aircraft galley appliance water heater. ### Claim 2 (depends on 1) The onboard aircraft system of claim 1, wherein the aircraft galley appliance is at least one of an aircraft galley coffee maker, an aircraft galley water boiler, and an aircraft galley steam oven. ### Claim 3 (depends on 1) The onboard aircraft system of claim 1, wherein, in operation, the potable water pathway is a potable water closed circuit, said potable water closed circuit further comprising a valve, said valve positioned between the aircraft potable water supply and the potable water pathway, and wherein said valve is configured to move from an open position configured to release potable water from the potable water supply into the potable water pathway to a closed position configured to restrict re-entry of the pre-warmed potable water flow back into the potable water supply. ### Claim 4 (depends on 1) The onboard aircraft system of claim 1, wherein, in operation, the potable water pathway is a potable water open circuit in communication with a continuous potable water flow directed from the aircraft potable water supply into the potable water circuit, and wherein a volume of the pre-warmed potable water flow downstream of at least one of the aircraft galley appliance and the pre-warmed potable water storage vessel is permitted to reenter the aircraft potable water supply. ### Claim 5 (depends on 1) The onboard aircraft system of claim 1, wherein, in operation, said pre-warmed potable water flow is configured to exit the heat exchanger warmed potable water flow outlet at a warmed potable water flow temperature ranging from about 60° F. to about 80° F. ### Claim 6 (depends on 1) The onboard aircraft system of claim 1, wherein the chilled air circuit is in communication with the potable water pathway. ### Claim 7 (depends on 1) The onboard aircraft system of claim 1, wherein the potable water pathway is at least in communication with the chilled air circuit at the heat exchanger, said potable water pathway configured to augment cooling in the chilled air circuit. ### Claim 8 (depends on 1) The onboard aircraft system of claim 1, wherein the pre-warmed potable water storage vessel is in communication with the potable water supply via the pre-warmed potable water flow line, said pre-warmed potable water flow line configured to direct a volume of pre-warmed potable water flow from the pre-warmed potable water storage vessel to the potable water supply. ### Claim 9 (depends on 1) An aircraft comprising the onboard aircraft system of claim 1. ### Claim 10 (depends on 4) An aircraft comprising the onboard aircraft system of claim 4. ### Claim 11 (depends on 5) An aircraft comprising the onboard aircraft system of claim 5. ### Claim 12 A method for decreasing electrical energy demand in an operating aircraft galley appliance water heater, the method comprising: directing a potable water flow from a potable water supply into a potable water pathway, said potable water flow having an initial potable water flow temperature ranging from about 35° F. to about 77° F.; directing the potable water flow into a heat exchanger potable water inlet of a heat exchanger, said heat exchanger positioned proximate to an air chiller condenser in a chilled air circuit, said heat exchanger comprising a heat exchanger warmer air inlet and a heat exchanger cooler air outlet, said heat exchanger further comprising a heat exchanger potable water flow inlet and a heat exchanger pre-warmed potable water flow outlet; directing an ambient airflow into the heat exchanger warmer air inlet, said ambient airflow having a temperature greater than the initial potable water flow temperature; directing a cooler airflow from the heat exchanger cooler air outlet to the air chiller condenser intake, said cooler airflow having a temperature lower than the ambient airflow; forming a pre-warmed potable water flow at the heat exchanger, said pre-warmed potable water flow comprising a pre-warmed potable water flow temperature higher than the initial potable water flow temperature; and directing the pre-warmed potable water flow from the heat exchanger pre-warmed potable water flow outlet to the aircraft galley appliance water heater via a pre-warmed potable water flow line. ### Claim 13 (depends on 12) The method of claim 12 further comprising: directing a portion of the pre-warmed potable water flow to a pre-warmed potable water storage vessel. ### Claim 14 (depends on 13) The method of claim 13, further comprising: directing a portion of the pre-warmed potable water flow from the pre-warmed potable water storage vessel to the aircraft galley appliance water heater. ### Claim 15 (depends on 13) The method of claim 13, further comprising: directing a portion of the pre-warmed potable water flow from the pre-warmed potable water storage vessel to the potable water supply. ### Claim 16 (depends on 13) The method of claim 13 further comprising: directing a portion of the pre-warmed potable water flow from the potable water flow pathway into the potable water supply, said potable water pathway configured to be a potable water open circuit. ### Claim 17 (depends on 12) The method of claim 12, wherein the potable water pathway is in communication with the chilled air circuit, said potable water pathway configured to augment cooling in the chilled air circuit. ### Claim 18 (depends on 12) The method of claim 12, wherein, in operation, the potable water pathway comprises a potable water closed circuit. ### Claim 19 (depends on 12) The method of claim 12, wherein, in operation, the potable water pathway comprises a potable water open circuit, said potable water open circuit configured to remain in open communication with the potable water supply. ### Claim 20 (depends on 12) The method of claim 12, wherein the potable water supply maintains an average temperature ranging from about 35° F. to about 77° F. and the pre-warmed potable water flow leaving the heat exchanger in the potable water pathway comprises a pre-warmed potable water flow temperature ranging from about 60° F. to about 80° F.