USH536H - Method of detecting and locating an electrostatic discharge event - Google Patents
Method of detecting and locating an electrostatic discharge event Download PDFInfo
- Publication number
- USH536H USH536H US06/886,995 US88699586A USH536H US H536 H USH536 H US H536H US 88699586 A US88699586 A US 88699586A US H536 H USH536 H US H536H
- Authority
- US
- United States
- Prior art keywords
- electrostatic discharge
- discharge event
- sensing
- event
- locating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000000034 method Methods 0.000 title claims abstract description 14
- 239000000463 material Substances 0.000 description 5
- 239000003380 propellant Substances 0.000 description 3
- 230000003750 conditioning effect Effects 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 101100386054 Saccharomyces cerevisiae (strain ATCC 204508 / S288c) CYS3 gene Proteins 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000135 prohibitive effect Effects 0.000 description 1
- 101150035983 str1 gene Proteins 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/22—Details, e.g. general constructional or apparatus details
- G01N29/24—Probes
- G01N29/2412—Probes using the magnetostrictive properties of the material to be examined, e.g. electromagnetic acoustic transducers [EMAT]
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
- G01N29/14—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object using acoustic emission techniques
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
- G01R31/12—Testing dielectric strength or breakdown voltage ; Testing or monitoring effectiveness or level of insulation, e.g. of a cable or of an apparatus, for example using partial discharge measurements; Electrostatic testing
- G01R31/1209—Testing dielectric strength or breakdown voltage ; Testing or monitoring effectiveness or level of insulation, e.g. of a cable or of an apparatus, for example using partial discharge measurements; Electrostatic testing using acoustic measurements
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2291/00—Indexing codes associated with group G01N29/00
- G01N2291/01—Indexing codes associated with the measuring variable
- G01N2291/011—Velocity or travel time
Definitions
- Sensitive electrostatic discharges that need to be identified involve systems that include missile systems that can be damaged by electrostatic discharges and propellants that can be inadvertently detonated by an electrostatic discharge event. These events are electrostatic arcs that are caused by charge separations. The charges may become separated by friction, propellant separation, or by induction fields in voids. These events generally occur subsurface and are not detectable optically.
- Another object of this invention is to utilize an electromagnetic method for detecting the event and an acoustic method for producing information from which the site of the electrostatic discharge can be located.
- Still another object of this invention is to provide a method that utilizes means that are readily available, relatively simple, relatively inexpensive and have the ability to provide sufficient information to accurately locate an electrostatic discharge event.
- a method of detecting and locating an electrostatic discharge event in which an electromagnetic detector on the structure of the device that has the electrostatic discharge event occuring there at is utilized for detecting that the event has occurred to start the counting of time, three acoustic detectors placed at different positions on the device in which the electrostatic discharge event occurs are utilized for detecting when the acoustic from the electrostatic discharge event reaches each of the acoustic detectors, and determining the time it takes the acoustics to travel to each of the acoustic detectors with the known positions of the acoustic detectors and utilizing this information to determine the location of the electrostatic discharge event within the device.
- FIG. 1 is a schematic illustration of an electrostatic discharge detector and locator system for carrying out the method
- FIG. 2 is a schematic circuit diagram for the system used in the method and illustrating the records caused to be produced by the detectors.
- the event desired to be detected is located in a device such as structure 10 that contains materials that are sensitive to electrostatic discharge. Structures of this type are propellants as well as other types of missile systems.
- An electromagnetic pickup device 12 is secured in a conventional manner to structure 10 and has an antenna 14 (see FIG. 2) such as a loop or stub antenna for picking up the electromagnetic waves of the event.
- Antenna 14 is connected by leads 16 through a high frequency audio amplifier means 18 greater than 100 Khz.
- Structure 10 also includes three acoustic detectors 24, 26, and 28 that are attached in a conventional manner to the structure of the system under test. These acoustic detectors 24, 26 and 28 are preferrably contact accelerometers such as high frequency microphones that have a frequency response of 2.5 KHz to 35 KHz with a rise time of 10 -5 seconds or less. Detectors 24, 26 and 28 are connected by leads 30, 32 and 34 to instrumentation control containers 36, 38 and 40. Each instrumentation control container includes an accelerometer drive for its respective detector and conditioning amplifier means.
- the output from the conditioning amplifier means is connected by leads 42, 44, and 46 to recording device 22 for recording the acoustics detected by detectors 24, 26 and 28 to establish times t 1 , t 2 , and t 3 .
- instrumentation control containers 36, 38 and 40 can contain fiber optic drives and fiber optic controls as are conventional in this type art for coupling the information. It is noted that detectors 24, 26, and 28 have been arbitrarily located as indicated, and the indicated locations work well. Since the location of the electrostatic discharge event relative to the acoustic detectors is to be determined, it is not desired to place the acoustic detectors close together or in a straight line.
- the first signal to reach each of detectors 24, 26 and 28 is the only useful signal that is used in determining the location of the electrostatic discharge event. There may be many standing waves set up in the material and the second, third, etc., wave may be detected until the signals are difficult to distinguish from background clutter. These signals may be useful in establishing the strength of the electrostatic discharge event; however, this particular feature is not of particular interest to this invention.
- an electrostatic discharge event occurs in structure 10
- the time required for the signal to travel from the location of the electrostatic discharge event to the location of the antenna of the electromagnetic pickup has been neglected. This time is of the order of a few nanoseconds.
- the electrostatic discharge event occurs somewhere on the surface of a sphere centered at the location of this particular detector with a radius of X 1 .
- This electrostatic discharge event is therefore also located on the surface of a sphere centered at the location of the second closest detector with a radius of X 2 .
- the electrostatic discharge event is located on a circle which is the innersection of these two spheres.
- the surface of this third sphere also intersects the above circles at only one point. This common point of the three spheres locates where the electrostatic discharge event took place.
- the location of the electrostatic discharge event is described mathematically below.
- the first detector assumes a right handed coordinate system X, Y, Z, and that t 1 ⁇ t 2 ⁇ t 3 . Let the first detector be located at (-h 1 , 0, 0), the second detector be located at (h 1 , 0, 0), the third detector be located at (0, h 2 , h 3 ).
- the X axis has been chosen so that both the first detector and the second detector are located on it.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Biochemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Acoustics & Sound (AREA)
- Electromagnetism (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Abstract
A method of locating an electrostatic discharge event in a predetermined ucture by sensing electromagnetically that an electrostatic discharge event has occurred and producing a trigger signal from the electromagnetic sensing to control a recording device for the starting of time, utilizing a plurality of acoustic detectors about the structure for sensing the acoustic of the electrostatic discharge event, determining the time elapsed between the starting of time by the electromagnetic sensing and the signals sensed by the acoustic detectors and utilizing the information gained from the times sensed and the predetermined locations of the sensors to determine the location of the electrostatic discharge event in the predetermined structure.
Description
The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to us of any royalties thereon.
In the past, it has not been possible to accurately locate electrostatic discharges even though it is important to accurately locate the site of electrostatic discharges that occur in systems or materials that are sensitive to electrostatic discharges. Sensitive electrostatic discharges that need to be identified involve systems that include missile systems that can be damaged by electrostatic discharges and propellants that can be inadvertently detonated by an electrostatic discharge event. These events are electrostatic arcs that are caused by charge separations. The charges may become separated by friction, propellant separation, or by induction fields in voids. These events generally occur subsurface and are not detectable optically. The fact that an event has occurred can be detected electrically, but to locate it electrically requires a very dense grid of sensors which is cost prohibitive, difficult to use and perturb the charge distribution to be monitored. Thus, it can be readily appreciated that a need exists for a relatively inexpensive, easy to use, and accurate way to detect and locate electrostatic discharge events.
Therefore, it is an object of this invention to supply a method by which an electrostatic discharge event can be detected and located.
Another object of this invention is to utilize an electromagnetic method for detecting the event and an acoustic method for producing information from which the site of the electrostatic discharge can be located.
Still another object of this invention is to provide a method that utilizes means that are readily available, relatively simple, relatively inexpensive and have the ability to provide sufficient information to accurately locate an electrostatic discharge event.
Other objects and advantages of this invention will be obvious to those skilled in this art.
In accordance with this invention, a method of detecting and locating an electrostatic discharge event is provided in which an electromagnetic detector on the structure of the device that has the electrostatic discharge event occuring there at is utilized for detecting that the event has occurred to start the counting of time, three acoustic detectors placed at different positions on the device in which the electrostatic discharge event occurs are utilized for detecting when the acoustic from the electrostatic discharge event reaches each of the acoustic detectors, and determining the time it takes the acoustics to travel to each of the acoustic detectors with the known positions of the acoustic detectors and utilizing this information to determine the location of the electrostatic discharge event within the device.
FIG. 1 is a schematic illustration of an electrostatic discharge detector and locator system for carrying out the method; and
FIG. 2 is a schematic circuit diagram for the system used in the method and illustrating the records caused to be produced by the detectors.
Referring now to the drawings, the event desired to be detected is located in a device such as structure 10 that contains materials that are sensitive to electrostatic discharge. Structures of this type are propellants as well as other types of missile systems. An electromagnetic pickup device 12 is secured in a conventional manner to structure 10 and has an antenna 14 (see FIG. 2) such as a loop or stub antenna for picking up the electromagnetic waves of the event. Antenna 14 is connected by leads 16 through a high frequency audio amplifier means 18 greater than 100 Khz. Amplifier 18 is connected by appropriate lead 20 to a recording device 22 such as an oscilloscope, oscillograph, or computer to provide a trigger input through lead 20 to recording device 22 to mark the starting of time at t=0 as indicated. Even though one electromagnetic pickup device has been illustrated, it may be desirable in some applications to provide more than one electromagnetic pickup on the structure in which the electromagnetic discharge event is to occur. Structure 10 also includes three acoustic detectors 24, 26, and 28 that are attached in a conventional manner to the structure of the system under test. These acoustic detectors 24, 26 and 28 are preferrably contact accelerometers such as high frequency microphones that have a frequency response of 2.5 KHz to 35 KHz with a rise time of 10-5 seconds or less. Detectors 24, 26 and 28 are connected by leads 30, 32 and 34 to instrumentation control containers 36, 38 and 40. Each instrumentation control container includes an accelerometer drive for its respective detector and conditioning amplifier means. The output from the conditioning amplifier means is connected by leads 42, 44, and 46 to recording device 22 for recording the acoustics detected by detectors 24, 26 and 28 to establish times t1, t2, and t3. If desired, instrumentation control containers 36, 38 and 40 can contain fiber optic drives and fiber optic controls as are conventional in this type art for coupling the information. It is noted that detectors 24, 26, and 28 have been arbitrarily located as indicated, and the indicated locations work well. Since the location of the electrostatic discharge event relative to the acoustic detectors is to be determined, it is not desired to place the acoustic detectors close together or in a straight line. The first signal to reach each of detectors 24, 26 and 28 is the only useful signal that is used in determining the location of the electrostatic discharge event. There may be many standing waves set up in the material and the second, third, etc., wave may be detected until the signals are difficult to distinguish from background clutter. These signals may be useful in establishing the strength of the electrostatic discharge event; however, this particular feature is not of particular interest to this invention.
In operation, when an electrostatic discharge event occurs in structure 10, the event is detected at antenna 14 of electromagnetic pickup 12 and the signal triggers recording device 22 to start the time at t=0 as illustrated. The time required for the signal to travel from the location of the electrostatic discharge event to the location of the antenna of the electromagnetic pickup has been neglected. This time is of the order of a few nanoseconds. Some time later, after time t=0, say t1, an acoustic signal from the electrostatic discharge event is detected by the closest detector of detectors 24, 26, and 28. If the velocity of sound is V, then the distance X from this detector to the electrostatic discharge event's location is given by X1 =Vt1. Therefore, the electrostatic discharge event occurs somewhere on the surface of a sphere centered at the location of this particular detector with a radius of X1. The next detector of detectors 24, 26 and 28 to receive the signal determines a time t2 as illustrated and is located distance X2 =Vt.sub. 2. This electrostatic discharge event is therefore also located on the surface of a sphere centered at the location of the second closest detector with a radius of X2. Thus, the electrostatic discharge event is located on a circle which is the innersection of these two spheres. The fartherest detector of detectors 24, 26 and 28 reoeives the signal at time t3 and likewise determines a sphere, of radius X3 =Vt3, on the surface of which the eleotrostatic discharge event also occurs. The surface of this third sphere also intersects the above circles at only one point. This common point of the three spheres locates where the electrostatic discharge event took place.
The location of the electrostatic discharge event is described mathematically below. The first detector assumes a right handed coordinate system X, Y, Z, and that t1 <t2 <t3. Let the first detector be located at (-h1, 0, 0), the second detector be located at (h1, 0, 0), the third detector be located at (0, h2, h3). Here the X axis has been chosen so that both the first detector and the second detector are located on it. Now if the event occurs at (X, Y, Z) then the three shares on which the event is located are given by ##STR1## Where X1 =Vt1, X2 =Vt2, and X3 =Vt3 and the solution of this system of equations gives the values of X, Y, and Z for the electrostatic discharge event. The above equations are quadratic, and therefore there are two possible solutions. This ambiguity can be removed by the use of an additional acoustic detector. However, for most applications the three acoustic detectors can be arranged so that one of these solutions falls outside the body being tested. In any event, in practice this data processing can be accomplished by allowing recording device 22 to be a small computer.
In some systems where several materials are used, there exist inhomogenuities and the velocity of sound may not be constant or isotropic. These anisotropic properties can be troublesome, but the systems of concern are known and a knowledge of the materials involved exist. Therefore, these uncertainties can be minimized by calibration techniques.
Claims (4)
1. A method of locating an electrostatic discharge event in a predetermined structure, said method comprising sensing electromagnetically that an electrostatic discharge event has occurred, producing a trigger signal from said sensed electromagnetic discharge event and utilizing said trigger signal to control a recording device and start the counting of time at t=0, sensing acoustics from said electrostatic discharge event at three spaced apart positions on said structure and communicating the sensed acoustics as inputs to said recording device to determine the time ellapsed from t=0 until the acoustics from the electrostatic discharge event reaches each of the three sensing acoustic and utilizing the information gained by the electromagnetic sensing and the acoustic sensing to determine the location of the electrostatic discharge event in said structure.
2. A method of locating an electrostatic discharge event as set forth in claim 1, wherein an antenna is used in the electromagnetic sensing of said electrostatic charge event, and wherein high frequency microphones with frequency response from 2.5 KHz to 35 KHz are used for said acoustic sensing.
3. A method of locating an electrostatic discharge event as set forth in claim 2, wherein said recording device utilized is an oscilloscope.
4. A method of locating an electrostatic discharge event as set forth in claim 3, wherein said acoustic sensing is sensed at random positions about said structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/886,995 USH536H (en) | 1986-07-18 | 1986-07-18 | Method of detecting and locating an electrostatic discharge event |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/886,995 USH536H (en) | 1986-07-18 | 1986-07-18 | Method of detecting and locating an electrostatic discharge event |
Publications (1)
Publication Number | Publication Date |
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USH536H true USH536H (en) | 1988-10-04 |
Family
ID=25390228
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US06/886,995 Abandoned USH536H (en) | 1986-07-18 | 1986-07-18 | Method of detecting and locating an electrostatic discharge event |
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US (1) | USH536H (en) |
Cited By (51)
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---|---|---|---|---|
US5107447A (en) * | 1988-05-16 | 1992-04-21 | Hitachi, Ltd. | Abnormality diagnosing system and method for a high voltage power apparatus |
US5185684A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Frequency selective arc detection |
US5185685A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Field sensing arc detection |
US5185687A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Chaos sensing arc detection |
US5185686A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Direction sensing arc detection |
US5208542A (en) * | 1991-03-28 | 1993-05-04 | Eaton Corporation | Timing window arc detection |
US5214595A (en) * | 1988-05-16 | 1993-05-25 | Hitachi, Ltd. | Abnormality diagnosing system and method for a high voltage power apparatus |
US5432455A (en) * | 1992-07-30 | 1995-07-11 | Blades; Frederick K. | Method and apparatus for detecting arcing in alternating current power systems by monitoring high-frequency noise |
US5434509A (en) * | 1992-07-30 | 1995-07-18 | Blades; Frederick K. | Method and apparatus for detecting arcing in alternating-current power systems by monitoring high-frequency noise |
US5452223A (en) * | 1993-08-20 | 1995-09-19 | Eaton Corporation | Arc detection using current variation |
US5590012A (en) * | 1995-03-30 | 1996-12-31 | Siemens Energy & Automation, Inc. | Electric arc detector sensor circuit |
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US5682101A (en) * | 1995-03-13 | 1997-10-28 | Square D Company | Arcing fault detection system |
US5729145A (en) * | 1992-07-30 | 1998-03-17 | Siemens Energy & Automation, Inc. | Method and apparatus for detecting arcing in AC power systems by monitoring high frequency noise |
US5825598A (en) * | 1997-02-11 | 1998-10-20 | Square D Company | Arcing fault detection system installed in a panelboard |
US5834940A (en) * | 1996-09-24 | 1998-11-10 | Brooks; Stanley J. | Arcing fault detector testing and demonstration system |
US5839092A (en) * | 1997-03-26 | 1998-11-17 | Square D Company | Arcing fault detection system using fluctuations in current peaks and waveforms |
US5847913A (en) * | 1997-02-21 | 1998-12-08 | Square D Company | Trip indicators for circuit protection devices |
US5923160A (en) * | 1997-04-19 | 1999-07-13 | Lucent Technologies, Inc. | Electrostatic discharge event locators |
US5946179A (en) * | 1997-03-25 | 1999-08-31 | Square D Company | Electronically controlled circuit breaker with integrated latch tripping |
US5986860A (en) * | 1998-02-19 | 1999-11-16 | Square D Company | Zone arc fault detection |
US6034611A (en) * | 1997-02-04 | 2000-03-07 | Square D Company | Electrical isolation device |
FR2786274A1 (en) * | 1998-11-25 | 2000-05-26 | Alstom Technology | METHOD AND DEVICE FOR DETECTION OF AN INTERNAL ARC IN AN ELECTRICAL LINK IN A METAL ENCLOSURE |
US6242993B1 (en) | 1995-03-13 | 2001-06-05 | Square D Company | Apparatus for use in arcing fault detection systems |
US6246556B1 (en) | 1995-03-13 | 2001-06-12 | Square D Company | Electrical fault detection system |
US6259996B1 (en) | 1998-02-19 | 2001-07-10 | Square D Company | Arc fault detection system |
US6313641B1 (en) | 1995-03-13 | 2001-11-06 | Square D Company | Method and system for detecting arcing faults and testing such system |
US6313642B1 (en) | 1995-03-13 | 2001-11-06 | Square D Company | Apparatus and method for testing an arcing fault detection system |
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-
1986
- 1986-07-18 US US06/886,995 patent/USH536H/en not_active Abandoned
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---|---|---|---|---|
US5214595A (en) * | 1988-05-16 | 1993-05-25 | Hitachi, Ltd. | Abnormality diagnosing system and method for a high voltage power apparatus |
US5107447A (en) * | 1988-05-16 | 1992-04-21 | Hitachi, Ltd. | Abnormality diagnosing system and method for a high voltage power apparatus |
US5185684A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Frequency selective arc detection |
US5185685A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Field sensing arc detection |
US5185687A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Chaos sensing arc detection |
US5185686A (en) * | 1991-03-28 | 1993-02-09 | Eaton Corporation | Direction sensing arc detection |
US5208542A (en) * | 1991-03-28 | 1993-05-04 | Eaton Corporation | Timing window arc detection |
US5729145A (en) * | 1992-07-30 | 1998-03-17 | Siemens Energy & Automation, Inc. | Method and apparatus for detecting arcing in AC power systems by monitoring high frequency noise |
US5432455A (en) * | 1992-07-30 | 1995-07-11 | Blades; Frederick K. | Method and apparatus for detecting arcing in alternating current power systems by monitoring high-frequency noise |
US5434509A (en) * | 1992-07-30 | 1995-07-18 | Blades; Frederick K. | Method and apparatus for detecting arcing in alternating-current power systems by monitoring high-frequency noise |
US5452223A (en) * | 1993-08-20 | 1995-09-19 | Eaton Corporation | Arc detection using current variation |
US5561605A (en) * | 1993-08-20 | 1996-10-01 | Eaton Corporation | Arc detection using current variation |
US6532424B1 (en) | 1995-03-13 | 2003-03-11 | Square D Company | Electrical fault detection circuit with dual-mode power supply |
US5682101A (en) * | 1995-03-13 | 1997-10-28 | Square D Company | Arcing fault detection system |
US6591482B1 (en) | 1995-03-13 | 2003-07-15 | Square D Company | Assembly methods for miniature circuit breakers with electronics |
US6195241B1 (en) | 1995-03-13 | 2001-02-27 | Squares D Company | Arcing fault detection system |
US6452767B1 (en) | 1995-03-13 | 2002-09-17 | Square D Company | Arcing fault detection system for a secondary line of a current transformer |
US6377427B1 (en) | 1995-03-13 | 2002-04-23 | Square D Company | Arc fault protected electrical receptacle |
US6313642B1 (en) | 1995-03-13 | 2001-11-06 | Square D Company | Apparatus and method for testing an arcing fault detection system |
US6313641B1 (en) | 1995-03-13 | 2001-11-06 | Square D Company | Method and system for detecting arcing faults and testing such system |
US6246556B1 (en) | 1995-03-13 | 2001-06-12 | Square D Company | Electrical fault detection system |
US6242993B1 (en) | 1995-03-13 | 2001-06-05 | Square D Company | Apparatus for use in arcing fault detection systems |
US5706159A (en) * | 1995-03-30 | 1998-01-06 | Siemens Energy & Automation, Inc. | Circuit interrupter including an electric arc monitoring circuit |
US5590012A (en) * | 1995-03-30 | 1996-12-31 | Siemens Energy & Automation, Inc. | Electric arc detector sensor circuit |
WO1997024742A1 (en) * | 1995-12-27 | 1997-07-10 | Quiet Power Systems, Inc | Method and apparatus for locating partial discharge in electrical transformers |
US5834940A (en) * | 1996-09-24 | 1998-11-10 | Brooks; Stanley J. | Arcing fault detector testing and demonstration system |
US6034611A (en) * | 1997-02-04 | 2000-03-07 | Square D Company | Electrical isolation device |
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