Hybrid Magneto-Active Membrane for Fuel Slosh Damping
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Solution Overview
Problem
Existing propellant management devices for spacecraft and aircraft, such as passive and active baffles and elastomeric membranes, increase structural mass and reduce tank volume while providing limited damping of fuel slosh, which can lead to undesirable trajectory changes and fuel consumption issues.
Innovation Solution
A hybrid magneto-active membrane that combines a polymer diaphragm with a flexible magneto-active matrix, activated by a magnetic field to change shape, stiffness, or configuration, effectively damping fuel slosh across various amplitudes, fill levels, and attitudes, reducing the need for additional structural mass.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If passive or active baffle structures are used to damp fuel slosh, then slosh damping effectiveness is improved, but structural mass increases and tank volume decreases
Solution Approach 1:
The patent replaces traditional mechanical baffle structures with a magnetic field-based active membrane system. The magnetic field acts on magneto-active particles embedded in the membrane to provide slosh damping forces, eliminating the need for heavy mechanical baffles while maintaining damping effectiveness.
Solution Approach 2:
The patent changes the physical state and properties of the membrane by applying magnetic fields. The magneto-active particles within the membrane respond to magnetic field strength variations, allowing the membrane's stiffness and damping characteristics to be dynamically adjusted without changing the physical structure.
2Reliability
If elastomeric membranes are used for slosh suppression, then damping effect is improved, but the effective tank volume is reduced
Solution Approach 1:
The patent uses a thin flexible membrane embedded with magneto-active particles that can be activated by magnetic fields. This thin-film approach provides effective slosh suppression while occupying minimal space, preserving the effective tank volume compared to bulkier elastomeric membrane solutions.
Solution Approach 2:
The patent replaces thick elastomeric membranes with a thin active membrane system controlled by magnetic fields. The magnetic actuation provides the necessary damping forces without requiring the membrane to be thick or bulky, thus maximizing the effective tank volume.
3Adaptability or versatility
If active baffles are used to constrain slosh behavior, then control effectiveness is improved, but device complexity increases
Solution Approach 1:
The patent creates a multi-functional system where the magnetic field source serves multiple purposes: it provides slosh damping, controls membrane shape, and can be adjusted for different operating conditions. This single system replaces multiple separate control mechanisms, reducing overall complexity while maintaining adaptability.
Solution Approach 2:
The patent uses magnetic field parameters (strength, frequency, distribution) to control slosh behavior across different amplitudes and conditions. By adjusting magnetic field parameters rather than physically reconfiguring complex baffle systems, the patent achieves high adaptability with simpler device architecture.
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
The hybrid magneto-active membrane effectively absorbs energy from sloshing fuel, reducing oscillatory forces and maintaining stability in microgravity conditions, while maintaining adaptability and efficiency in fuel management.
Implementation Method 1
a flexible magneto-active matrix comprising a layer of magnetically permeable material configured to move with the at least one polymer membrane
Implementation Method 2
The hybrid magneto-active membrane is designed to actively control free surface effects of liquid materials such as fuels, and to reduce fuel slosh
Data Source
AI summary
This disclosure includes a hybrid magneto-active membrane, which can be used as part of a Magneto-active Propellant Management Device (MAPMD), to actively control free surface effects of liquid materials, such as fuels, and to reduce fuel slosh. The disclosed MAPMD merges aspects of a diaphragm membrane with a magneto-active inlay to control the membrane during in-flight conditions.


