Micro scale electro hydrodynamic (EHD) modular cartridge pump

mechanical and fluid systems
Micro scale electro hydrodynamic (EHD) modular cartridge pump (GSC-TOPS-139)
EHD modular cartridge pump that is designed and engineered to be the smallest and simplest iteration in NASAs arsenal.
Overview
This NASA innovation incorporates a simplistic design that reduces the number of components required to make an assembly by up to 90% over previous iterations, insuring a solid reliable electrical connection to the electrodes that form the pumping sections and is modular in overall design to allow for flexibility in incorporating the pump cartridge into various assemblies and applications.

The Technology
NASA GSFCs EHD pump uses electric fields to move a dielectric fluid coolant in a thermal loop to dissipate heat generated by electrical components with a low power system. The pump has only a few key components and no moving parts, increasing the simplicity and robustness of the system. In addition, the lightweight pump consumes very little power during operation and is modular in nature. The pump design takes a modular approach to the pumping sections by means of an electrically insulating cartridge casing that houses the high voltage and ground electrodes along with spacers that act as both an insulator and flow channel for the dielectric fluid. The external electrical connections are accomplished by means of commercially available pin and jack assemblies that are configurable for a variety of application interfaces. It can be sized to work with small electric components or lab-on-a-chip devices and multiple pumps can be placed in line for pumping greater distances or used as a feeder system for smaller downstream pumps. All this is done as a one-piece construction consolidating an assembly of 21 components over previous iterations.
Benefits
  • Low malfunction rate due to no moving parts
  • Simple and robust system
  • Light weight and low energy consumption

Applications
  • Computer thermal control
  • Aerospace
  • Automotive
Technology Details

mechanical and fluid systems
GSC-TOPS-139
GSC-17220-1
10461621
Similar Results
Cell attached to the surface of a scaffold fiber (5 m)
Electroactive Scaffold
Current scaffold designs and materials do not provide all of the appropriate cues necessary to mimic in-vivo conditions for tissue engineering and stem cell engineering applications. It has been hypothesized that many biomaterials, such as bone, muscle, brain and heart tissue exhibit piezoelectric and ferroelectric properties. Typical cell seeding environments incorporate biochemical cues and more recently mechanical stimuli, however, electrical cues have just recently been incorporated in standard in-vitro examinations. In order to develop their potential further, novel scaffolds are required to provide adequate cues in the in-vitro environment to direct stem cells to differentiate down controlled pathways or develop novel tissue constructs. This invention is for a scaffold that provides for such cues by mimicking the native biological environment, including biochemical, topographical, mechanical and electrical cues.
Filtering Molecules with Nanotube Technology
Filtering Molecules with Nanotube Technology
This water filtration innovation is an acoustically driven molecular sieve embedded with small-diameter carbon nanotubes. First, water enters the device and contacts the filter matrix, which can be made of polymer, ceramic, or metallic compounds. Carbon nanotubes within the matrix allow only water molecules to pass through, leaving behind any larger molecules and contaminants. The unique aspect of the technology is its use of acoustics to help drive water through the filter. An oscillator circuit attached to the filter matrix propagates acoustic vibration, further causing water molecules to de-bond and move through the filter. This use of acoustics also eliminates dependence on gravity (and thus filter orientation) to move water through the device. When water exiting the system diminishes to a pre-determined set point, a cleaning cycle is triggered to clear the sediment from the inlet of the filter, reestablishing the standard system flow rate. Unlike other filtration systems, flushing of the filter system is not required. The combination of acoustics and small-diameter carbon nanotubes in this innovation make it an effective and efficient means of producing contaminant-free, clean water.
Cooperative Service Valve for on-orbit cooperative satellite fueling
Cooperative Service Valve for In-orbit Cooperative Satellite Fueling
The CSV replaces a standard spacecraft Fill and Drain Valve to facilitate cooperative servicing. The CSV offers various advantages over standard service valves: a robotic interface, three individually actuated seals, a self-contained anti-back drive system, and built-in thermal isolation. When mounted to a spacecraft as designed, the CSV transfers all operational and induced robotic loads to the mounting structure. An anti-back drive mechanism prevents the CSV seal mechanism from inadvertent actuation. Alignment marks, thermal isolation, and a mechanical coupling capable of reacting operational and robotic loads optimize the CSV for tele-robotic operations. Unique keying of the mating interface prevents mixing of media where more than one configuration of the CSV is used. Color-coding and labels are also used to prevent operator error. The CSV has four configurations for different working fluids, all with essentially unchanged geometry and mechanics.
https://pixabay.com/photos/architecture-station-city-to-travel-4112894/

Pixbay license: free for commercial use; no attribution required
In-Space Assembly of Structural Trusses and Shapes
The NASA innovation is based on a tessellation algorithm to break up a curved surface into identically sized equilateral surface polygons. Tessellation is a term used in mathematics that describes the process of deconstructing a surface into non-overlapping shapes with no gaps. Using this NASA innovation enables a curved-surface truss structure to be designed and built using all identical module and strut components. A key feature of this innovation is the use of a “multi-nut” connector, which enables curved surface truss structures to be assembled from identical truss modules. Uniform truss modules with customizable multi-nut connectors can be used to construct a curved-surface structure. The algorithm is a design approach for any size or surface shape. The NASA innovation represents a major breakthrough due to: • Versatility to a variety of planar and curved structure shapes (cylinder, sphere, etc.) • Ability to change the shape simply by updating the “multi-nut” connectors • Commonality of truss modules and components • Ease of assembly • Efficiency of construction and weight • Robotic assembly and servicing. In addition to a range of space related applications – mirrors, antennas, habitats, storage containers, etc. – the innovation is also directly applicable to general terrestrial assembly of systems with curvature, including for example sports stadiums, airports, aquariums, convention centers, or bridges.
Image from inventor slide deck shared on NTTS.
Universal Power Converter for a Lunar Power Grid
NASA’s Universal Modular Interface Converter (UMIC) is a bidirectional, modular power electronics converter that transfers power between a 120 V DC space power bus, and a medium-to-high-voltage, three-phase AC power grid. The UMIC system contains multiple parallel AC/DC UMIC modules that convert between 120 V DC and low voltage AC, as well as one or more transformers that convert power from the low voltage AC bus to the grid voltage. The UMIC module consists of multiple subsystems, including the power stage, gate driver, Field Programmable Gate Array (FPGA)-based controller, output filter, signal conditioning and sensing circuits, and thermal management subsystems. An FPGA-based controller is included within each AC/DC module and is used to regulate desired power system variables; synchronize power switching events and share load current between modules; synchronize the modules with existing service on the grid; receive commands; and share telemetry. The FPGA-based controller subsystem includes the FPGA Integrated Circuit, associated flash memory, and a controller area network (CAN) transceiver. It is envisioned that future UMIC designs can support lunar grid expansions, a Mars surface grid, or large space stations. These applications may necessitate different grid voltages or frequencies, or different control logic and communication systems. However, the core UMIC architecture and functionality will remain the same. The related patent is now available to license. Please note that NASA does not manufacture products itself for commercial sale.
Stay up to date, follow NASA's Technology Transfer Program on:
facebook twitter linkedin youtube
Facebook Logo X Logo Linkedin Logo Youtube Logo