Aircraft Water Distribution With Buffer Tank Redistribution

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Solution Overview

Problem

Conventional aircraft water supply systems require individual buffer tanks for each water consumer unit, increasing aircraft weight and fuel consumption due to predefined water amounts, and lack efficient methods to manage water distribution and freezing prevention.

Innovation Solution

A water supply system with a main tank, buffer tanks, and a controller that operates in two modes: filling buffer tanks and redistributing water between them, allowing water reuse and efficient management to reduce overall water carry-on-board, and includes features like reverse pumps and consumer conveying devices for faster redistribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If individual buffer tanks with predefined water amounts are provided for each water consumer unit, then water pressure requirements for consumers are met, but aircraft weight increases and fuel consumption increases

Engineering Contradiction:
Improvewater pressure supplyVSAvoidaircraft weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent merges the water storage function from multiple individual buffer tanks into a single centralized buffer tank. This centralized tank serves all water consumer units through the pressurized water network, eliminating the need for separate predefined water amounts in each consumer unit while maintaining reliable water pressure supply to all consumers.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The centralized buffer tank performs multiple functions: it maintains water pressure for the entire aircraft water system, serves as a redistribution point for water between different consumer units, and enables draining operations. This universal buffer tank replaces the need for multiple specialized small tanks, reducing total weight while maintaining system reliability.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Reliability

If individual buffer tanks with predefined water amounts are provided for each water consumer unit, then water pressure requirements for consumers are met, but fuel consumption increases

Engineering Contradiction:
Improvewater pressure supplyVSAvoidfuel consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

By combining all buffer tank capacities into a single centralized buffer tank, the system reduces the total amount of water that must be carried on board. Since aircraft weight directly correlates with fuel consumption, this consolidation reduces fuel consumption while the centralized buffer tank continues to provide reliable water pressure to all consumer units through the pressurized network.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The system enables water recovery and redistribution from the centralized buffer tank to various consumer units as needed. Instead of each unit carrying its own predefined water amount, water is supplied on-demand from the centralized buffer, allowing the aircraft to carry only the minimum necessary water总量 and reducing fuel consumption.

Inventive Principle:
Principle #34Discarding and recovering

3Ease of operation

If water is stored in multiple buffer tanks throughout the aircraft, then water availability to consumers is ensured, but the amount of water to be carried increases

Engineering Contradiction:
Improvewater availabilityVSAvoidwater amount
Core Design Contradiction:
Ease of operationVSQuantity of substance

Solution Approach 1:

The centralized buffer tank acts as an intermediary between the main water tank and various consumer units. It receives water from the main tank via the pressurized network and distributes water to consumer units as needed, ensuring water availability without requiring large amounts of water to be distributed throughout the aircraft in multiple separate tanks.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

By merging all buffer storage into a single centralized location, the system ensures water availability to all consumer units through the pressurized distribution network while minimizing the total quantity of water that must be carried on board, compared to distributing buffer tanks throughout the aircraft.

Inventive Principle:
Principle #5Merging (Combining)

4Volume of moving object

If a pressurized water network operates at higher pressure, then pipe size can be reduced, but the pressure must be reduced before reaching individual consumers

Engineering Contradiction:
Improvepipe sizeVSAvoidpressure control system
Core Design Contradiction:
Volume of moving objectVSDevice complexity

Solution Approach 1:

The centralized buffer tank serves as a universal pressure control point for the entire water system. It receives high-pressure water from the main tank via the pressurized network, maintains appropriate pressure levels, and distributes water to all consumer units. This eliminates the need for multiple pressure control devices at each consumer location, reducing overall system complexity while allowing the use of smaller pipes in the pressurized network.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Reduces aircraft weight and fuel consumption by optimizing water distribution, enabling efficient water reuse and preventing freezing, while maintaining water pressure requirements for consumers.

Implementation Method 1

providing the water from the buffer tank solely via gravity (e.g., for a water dispenser)

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 2

A newly developed pressurised water network operates at a higher pressure than usually required for all water consumers

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Data Source

PatentUS20250319989A1Water supply and distribution system with optimized utilization of onboard water
Publication Date: 2025.10.16 AIRBUS OPERATIONS GMBH
  • US20250319989A1 patent drawing
  • US20250319989A1 patent drawing
  • US20250319989A1 patent drawing

AI summary

A water supply system including a main tank, a water network and buffer tanks, each being associated with a respective water consumer unit. A controller is configured to operate in a first mode, where water from the main tank is filled into the buffer tanks, and a second mode, where water from one more first buffer tanks is conducted to the main tank and/or to one more second buffer tanks being different from the one or more first buffer tanks.