Modified Tuned Liquid Column Damper
Mechanical and Fluid Systems
Modified Tuned Liquid Column Damper (MFS-TOPS-135)
Optimizing Vibration Suppression for Floating Offshore Turbines
Overview
Tuned liquid column dampers (TLCDs) are widely used for vibration suppression, yet their application to floating wind turbine systems presents unique challenges due to the strict geometric constraints of offshore platforms. Achieving the desired frequency, damping, and stiffness is often difficult within the limited space available, as these parameters are highly dependent on the TLCD’s column length, cross-sectional area, and fluid properties. This geometric limitation restricts flexibility in tuning the device to match the turbine’s dynamic response.
To address these limitations, researchers at NASA’s Marshall Space Flight Center have developed the Modified Tuned Liquid Column Damper (MTLCD). By adding valves, orifices, or pressurization, TLCDs can be modified to optimize parameters such as stiffness and frequency without altering their geometry. The MTLCD builds on this capability, enabling tailored vibration suppression and providing a versatile solution for enhancing the stability and performance of floating wind turbine systems.
The Technology
When waves move a floating wind turbine, they drive fluid motion inside the MTLCD. This forces air in the vertical tanks through an orifice, increasing pressure much like a spring. As the air discharges, the fluid’s motion is damped and energy is dissipated. The MTLCD also incorporates added damping elements, such as an orifice or variable-aperture reciprocating reed valve, that create resistance to air flow, further controlling fluid motion and dissipating energy.
By integrating these modifications, the MTLCD is easily tuned to the platform’s motions, reducing dependency on platform geometry. Eliminating damping elements from the fluid removes the need for marine-grade hardware, reducing system costs. The MTLCD can also be integrated into existing ballast tanks, maximizing space efficiency with minimal added parts.
While initially developed for NASA’s Floating Wind Turbine Development project, this invention can support vibration mitigation applications across multiple industries, such as infrastructure, maritime systems, and aerospace. By enabling precise tuning of dynamic response characteristics, the MTLCD offers a compact solution for platforms requiring vibration suppression. The technology has completed preliminary design and simulation, is at a TRL 3 (proof-of-concept), and is available for patent licensing.
Benefits
- Tunable Performance: Variable stiffness and damping improve system stability, control, and operational reliability.
- Damping Efficiency: Added orifices and valves boost damping, resulting in improved energy dissipation and reduced motion.
- Flexible Integration: Pressure can be adjusted without redesign, enabling adaptability across platforms and reducing development costs.
- Compact Design: Integrated ballast tanks conserve space and minimize added parts, supporting lightweight, efficient system architectures.
Applications
- Wind Energy: Mitigates vibrations and enhances performance of floating offshore wind turbines.
- Aerospace: Improves vibration suppression in launch vehicles and spacecrafts with geometric constraints.
- Construction: Enhances vibration control in tall buildings and structures against wind or seismic activity.
- Maritime Platforms: Reduces motions in oil and gas platforms with compact, tunable dampers.
Technology Details
Mechanical and Fluid Systems
MFS-TOPS-135
MFS-33051-1
MFS-34084-1
MFS-34473-1
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Similar Results
Ocean Platform Motion Control
The NASA innovation leverages existing ballast fluid of a maritime structure to proactively mitigate undesirable resonant response characteristics of the platform or vessel. Essentially, this innovation couples water ballast as a functional working mass to the dynamic motion of a floating structure in order to provide passive motion management of the primary structure.
The system can be implemented pre-design or post manufacture. The systems are simple and are easily manufactured, transported, and implemented onto a primary structure.
The NASA technology has been designed (patents applied for) for a range of platform designs and can be further customized depending on the final application requirements. Prototypes have been built and tested in a wind-wave tank test bed at the University of Maine.
Fluid-Filled Frequency-Tunable Mass Damper
NASA MSFC’s Fluid-Filled Frequency-Tunable Mass Damper (FTMD) technology implements a fluid-based mitigation system where the working mass is all or a portion of the fluid mass that is contained within the geometric configuration of either a channel, pipe, tube, duct and/or similar type structure. A compressible mechanism attached at one end of the geometric configuration structure enables minor adjustments that can produce large effects on the frequency and/or response attributes of the mitigation system.
Existing fluid-based technologies like Tuned Liquid Dampers (TLD) and Tuned Liquid Column Dampers (TLCD) rely upon the geometry of a container to establish mitigation frequency and internal fluid loss mechanisms to set the fundamental mitigation attributes. The FTMD offers an innovative replacement since the frequency of mitigation and mitigation attributes are established by the compressible mechanism at the end of the container. This allows for simple alterations of the compressible mechanism to make frequency adjustments with relative ease and quickness.
FTMDs were recently successfully installed on a building in Brooklyn, NYC as a replacement for a metallic TMD, and on a semi-submersible marine-based wind turbine in Maine.
The FTMD technology is available for non-exclusive licensing and partially-exclusive licensing (outside of building construction over 300 feet).
Compact Vibration Damper
Structural vibrations frequently need to be damped to prevent damage to a structure. To accomplish this, a standard linear damper or elastomeric-suspended masses are used. The problem associated with a linear damper is the space required for its construction. For example, if the damper's piston is capable of three inches of movement in either direction, the connecting shaft and cylinder each need to be six inches long. Assuming infinitesimally thin walls, connections, and piston head, the linear damper is at least 12 inches long to achieve +/-3 inches of movement. Typical components require 18+ inches of linear space. Further, tuning this type of damper typically involves fluid changes, which can be tedious and messy. Masses suspended by elastomeric connections enable even less range of motion than linear dampers.
The NASA invention is for a compact and easily tunable structural vibration damper. The damper includes a rigid base with a slider mass for linear movement. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A rack-and-pinion gear coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement. To achieve +/- 3 inches of movement, this design requires slightly more than six inches of space.
Self-Tuning Compact Vibration Damper
Structural vibrations frequently need to be damped to prevent damage to a structure or payload. To accomplish this, a standard linear damper or elastomeric-suspended masses are used. The problem associated with a linear damper is the space required for its construction. For example, if the damper's piston is capable of three inches of movement in either direction, the connecting shaft and cylinder each need to be six inches long. Assuming infinitesimally thin walls, connections, and piston head, the linear damper is at least 12 inches long to achieve +/3 inches of movement. Typical components require 18+ inches of linear space. Further, tuning this type of damper typically involves fluid changes, which can be tedious and messy. Masses suspended by elastomeric connections enable even less range of motion than linear dampers.
The NASA invention is a compact and self-tunable structural vibration damper. The damper includes a rigid base with a slider mass for linear movement. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A rack-and-pinion gear coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement. To achieve +/- 3 inches of movement, this design requires slightly more than six inches of space.
Fluid Structure Coupling Technology
FSC is a passive technology that can operate in different modes to control vibration:
Harmonic absorber mode: The fluid can be leveraged to act like a classic harmonic absorber to control low-frequency vibrations. This mode leverages already existing system mass to decouple a structural resonance from a discrete frequency forcing function or to provide a highly damped dead zone for responses across a frequency range.
Shell mode: The FSC device can couple itself into the shell mode and act as an additional spring in a series, making the entire system appear dynamically softer and reducing the frequency of the shell mode. This ability to control the mode without having to make changes to the primary structure enables the primary structure to retain its load-carrying capability.
Tuned mass damper mode: A small modification to a geometric feature allows the device to act like an optimized, classic tuned mass damper.



