Aircraft Liquid Transfer Modular Tank Bulkhead

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Solution Overview

Problem

Existing devices for receiving and releasing liquids in aircraft, such as for fire extinguishing, irrigation, or de-icing, face limitations in high-speed filling and discharge capabilities, and are constructed in a complex manner, lacking flexibility in handling varying liquid quantities.

Innovation Solution

A modular device comprising a tank module, bulkhead module, and filling module with a coiling hose pipe and double-walled receiving element, allowing for flexible assembly and rapid filling and discharge of liquids, including the use of flanges and pumping devices for efficient liquid transfer.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a complex device construction is used to receive and release liquids in aircraft, then the device can handle various liquid quantities, but the filling speed and discharge capability are reduced

Engineering Contradiction:
Improveflexibility in handling liquid quantitiesVSAvoidfilling speed and discharge capability
Core Design Contradiction:
Adaptability or versatilityVSProductivity

Solution Approach 1:

The device is divided into modular components: a tank module for liquid storage, a bulkhead module for flow control, and a filling module with a coiling hose pipe for liquid transfer. This segmentation allows each module to be optimized for its specific function while enabling flexible configuration for different liquid quantities without compromising filling speed or discharge capability.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If atmospheric pressure alone is used for discharge, then the device structure can be simplified, but high velocity discharge is not achieved

Engineering Contradiction:
Improvedevice structureVSAvoiddischarge velocity
Core Design Contradiction:
Device complexityVSSpeed

Solution Approach 1:

The bulkhead module incorporates a pumping device that uses hydraulic principles to generate high velocity discharge. The pump creates pressure differential that forces liquid through the discharge aperture at high speed, overcoming the limitations of atmospheric pressure alone while maintaining a relatively simple device structure.

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Device complexity

If a single tank container is used, then the device structure is simplified, but the ability to react to existing liquid quantities is reduced

Engineering Contradiction:
Improvedevice structureVSAvoidreaction to liquid quantities
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The bulkhead module includes a movable closing element that can dynamically adjust the opening size based on the quantity of liquid in the tank. This dynamic adjustment allows the device to adapt to different liquid quantities while maintaining a simple single-tank structure, enabling flexible response to varying operational requirements.

Inventive Principle:
Principle #15Dynamics

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

Enables rapid and flexible filling and discharge of liquids, accommodating variable quantities and facilitating efficient liquid transfer, with the modular design and double-walled receiving element reducing turbulence and enhancing pumping efficiency.

Implementation Method 1

the modular design and double-walled receiving element reducing turbulence and enhancing pumping efficiency

Methodology Applied
Scientific EffectTurbulence reduction: Turbulence

Data Source

PatentUS8096323B2Device for receiving liquids in aircraft and/or releasing liquids therefrom
Publication Date: 2012.01.17 VON MOHOS ZOLTAN
  • US8096323B2 patent drawing
  • US8096323B2 patent drawing
  • US8096323B2 patent drawing

AI summary

The invention relates to a device (1) for receiving liquids in an aircraft and/or releasing liquids therefrom, especially during the flight, said device being arranged especially in an airplane. The aim of the invention is to provide a device which can receive large quantities of liquids in a rapid, reliable and flexible manner. To this end, said device comprises a tank module (2) provided with at least one tank container (6) that is connected to a collector (8) by means of at least one connecting shaft (7), a bulkhead module (3) that can be connected to the tank module by means of the collecting tank and comprises a closing element (9) by which means, in the open position, liquids are released from the tank module, a refueling module (4) which is connected to the tank module by means of at least one supply line (10), and a tube which is arranged on a winding device (11) and comprises a receiving element (13) provided with at least one opening (14) which receives liquids released from the aircraft, so that the refueling of the device can take place.