In Situ Wire Damage Detection and Rerouting System

Electrical and Electronics
In Situ Wire Damage Detection and Rerouting System (KSC-TOPS-6)
A miniaturized and highly efficient wire damage detection system
Overview
NASA Kennedy Space Center seeks partners interested in the commercial application of the In Situ Wire Damage Detection and Rerouting System. NASA is soliciting licensees for this innovative technology. The In Situ Wire Damage Detection and Rerouting System consists of a miniaturized inline connector containing self-monitoring electronics that use time domain reflectometry (TDR) to detect wire faults and determine fault type and fault location on powered electrical wiring. When a damaged or defective wire is identified, the system is capable of autonomously transferring electrical power and data connectivity to an alternate wire path. When used in conjunction with NASAs wire constructions that use a conductive detection layer, the system is capable of detecting and limiting damage not only to the core conductor, but also to the insulation layer before the core conductor becomes compromised.

The Technology
The tester was designed to monitor electrical faults in either online or offline modes of operation. In the online mode, wires are monitored without disturbing their normal operation. A cable can be monitored several times per second in the offline mode, and once per second in the online mode. The online cable fault locator not only detects the occurrence of a fault, but also determines the type of fault (short/open/intermittent) and the location of the fault. This enables the detection of intermittent faults that can be repaired before they become serious problems. Since intermittent faults occur mainly during operations, a built-in memory device stores all relevant fault data. This data can be displayed in real time or retrieved later so maintenance and repairs can be completed without spending countless hours attempting to pinpoint the source of the problem. Hardware and algorithms have also been developed to safely, efficiently, and autonomously transfer electrical power and data connectivity from an identified damaged/defective wire in a cable to an alternate wire path. This portion of the system consists of master and slave units that provide the diagnostic and rerouting capabilities. A test pulse generated by the master unit is sent down an active wire being monitored by the slave unit. When the slave unit detects the test pulse, it routes the pulse back to the master unit through a communication wire. When the master unit determines that a test pulse is not being returned, it designates that wire as faulty and reroutes the circuit to a spare wire.
In Situ Wire Damage Detection and Rerouting System Exterior view of the ISWDDRS prototype module casing
Benefits
  • Simultaneously in online or offline mode
  • Online operation - system can be used while wires are powered and operational, making it possible to locate intermittent faults that occur only while wires are in use
  • Nonintrusive - faults are monitored in the background, using very low power signals that do not disrupt normal circuit operation
  • Intelligent - pattern recognition algorithms autonomously identify the type and location of a fault without operator intervention
  • Intuitive - an easy-to-understand graphical user interface displays the reflected waveforms and provides information on the type of fault and its distance fromthe test signal injection point
  • Flexible - system is capable of monitoring up to 64 individual wires on a cable

Applications
  • Aerospace wiring
  • Marine wiring
  • Automotive wiring
  • Industrial wiring
  • Smart grid wiring
Technology Details

Electrical and Electronics
KSC-TOPS-6
KSC-12866 KSC-13285
8,810,255 8,593,153
NASA Tech Brief, November 2012: https://ntrs.nasa.gov/api/citations/20130008790/downloads/20130008790.pdf
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Astronauts on Planet Surface
Dust Tolerant Quick Disconnect With Self-Sealing Barrier
Dusty, dirty environments can be very tough on connectors. The abrasive nature of dust and dirt particles can rub and wear down connector surfaces through friction, and have a negative effect on coatings used on gaskets to seal equipment. Dust on umbilical connections can also make mating and de-mating electrical and fluid connections difficult, hazardous, and unreliable. NASA's Quick Disconnect (QD) design consists of columnar arrays of parallel filaments. All the pins of the electrical connector easily penetrate the barriers when the umbilicals are brought together. They are wiped clean of dust when they penetrate the barrier and mate cleanly and reliably. Likewise, the male end of a fluid connector penetrates the filament arrays of both connector ends. Since the filament arrays are oriented perpendicular to each other, the entire circumference of the connector is contacted by the filaments that stretch around, conform to, and sweep off dust from the mating surface ensuring a clean and secure connection.
Cord Tension Measurement Device (C-Gauge)
The C-Gauge is made of a 3D-printed aluminum body with strain gauges attached to the inner and outer walls of the connecting beam. The legs of the gauge attach firmly to the cord. When the cord is stretched, the tension in the cord goes through the legs and into the beam, causing it to bend. This bending creates a tension and compression stress in the bottom and top surface of the beam, respectively. The strain gauges capture the tension and compression, which are then used to determine the tension in the cord. The use of multiple strain gauges mitigates any torsion loading of the gauge and provides a direct measurement of the axial tension load of the cord. The C-Gauge is a low-profile, non-invasive system that can be installed onto an existing cord in a system (e.g., the suspension, reefing, or riser lines in a parachute) without the need to remove or re-install the cord. It is small and lightweight and does not add stiffness or weight to the cord and thus does not affect the dynamics of the parachute or the structural response of the system. The C-Gauge can be scaled to larger and smaller sizes to measure larger and smaller load capabilities, dependent on the cord. The C-Gauge is at a TRL 4 (component and/or breadboard validation in a laboratory environment) and it is now available for your company to license and develop into a commercial product. Please note that NASA does not manufacture products itself for commercial sale.
Astronauts on Planet Surface
Quick Disconnect for High Pressure Mate/De-Mate
Dusty, dirty environments can be very tough on connectors. The abrasive nature of dust and dirt particles can rub and wear down connector surfaces through friction, and have a negative effect on coatings used on gaskets to seal equipment. Dust on umbilical connections can also make mating and de-mating electrical and fluid connections difficult, hazardous, and unreliable. NASA's Quick Disconnect (QD) design uses the gas supplied by the umbilical to spray the connector surfaces prior to mating to remove dust and debris. The QD uses a novel dual-poppet design and springs that balance forces on umbilical components. This allows a controlled release of gas to clear away dust from the end of the connector before it it inserted in the supply umbilical. The connector assembly is capable of mating and de-mating under 3500 psi fluid/gas. One poppet seals the QD while de-mated and automatically cleans the front surface of the QD during mating. A second poppet seals the QD while de-mated and automatically cleans the cylindrical surface of the QD during mating. The internal cavity of the QD is specifically designed such that the pressure in the line is reduced from 3500 psi to 450 psi while surface cleaning occurs. Finally, all exterior connector surfaces are designed to minimize the entrapment of dust while in the de-mated position.
Group of Four Assemblies
Feedthrough for Severe Environments and Temperatures
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