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Corona Threshold Voltage
Team Tesla: Chris Rowan Anthony Thompson Brandon Sciortino Philip de la Vergne Aaron Wascom
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Presentation Purpose This Presentation describes the preliminary design for the electrical breakdown experiment by Team Tesla for the LaACES Program. It fulfills part of the LaACES Project requirements for the Preliminary Design Review (PDR) to be held February 5,2013
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Document Scope This Pre-PDR Presentation specifies the goal, objectives, background, and requirements for the electrical breakdown experiment and provides a guideline for the development of this payload under the LaACES Project. As such, these topics provide the basic for developing the PDR document and presentation.
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Mission Goal To study the effects of humidity and temperature on the electrical breakdown of the atmosphere to prevent sparking and ensure safety. We want to do this to further ensure the reliability of electronics operating at varying temperature and pressure and humidity conditions.
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Science Objectives To conduct an experiment of the breakdown voltage in air at varying altitudes To observe the effects that temperature and humidity have on our expected recreation of Paschen’s curve
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Technical Objectives Measure temperature, pressure, humidity, current, and discharge voltage for the duration of the flight
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Science Background: Electric Discharge
Results from the creation of a conducting path between two points of different electrical potential Three Types: 1. Corona Discharge 2. Spark Discharge 3. Brush Discharge Electric discharge happens when there is a conducting path between two electrodes of different electric potential. In other words, when the medium changes from an insulator to a conductor. We want to create a corona discharge while preventing a spark discharge so that we don’t endanger any payloads. In order to do this, we must understand each of the different kinds of discharges.
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Science Background: Corona Discharge
Occurs when the threshold voltage is breached Only requires a high field strength Current ranges around micro amps If the field strength in front of a sharp point of a conductor exceeds the breakdown field strength for the medium (in this case air), a corona discharge will take place. It may also happen if a grounded, sharp conductor (at zero voltage) is brought near a charged object, like a piece of plastic that has been rubbed. This event demonstrates that it does not take a high voltage to cause a discharge, only a high field strength, which is ideal for our payload experiment due to our weight restrictions. It may be maintained as long as the breakdown field strength is exceeded in some region—that is, as long as the voltage of the electrode or the charge density of the charged insulator is high enough. The current in a corona discharge can be as low as micro amps.
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Science Background: Spark Discharge
Occurs when the threshold voltage is breached Complete ionization between electrodes Maintained through a continuous high voltage source At the other extreme of the discharge range, we have the spark. Like corona discharge, the discharge starts at the point where the breakdown field strength is exceeded. However, unlike corona discharge, the ionization takes place all the way between the two electrodes. If the electrodes are connected to a voltage supply, the discharge may turn into a continuous arc, but in the normal case of a spark from an insulated conductor, the discharge is a very fast process. Typically, the process is extremely fast. However, a spark may be maintained if it is continuously powered.
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Science Background: Brush Discharge
In between the corona and spark discharge It may appear as irregular luminescent paths Occurs between corona and spark discharge and may look like irregular luminescent paths. Almost all discharges from insulators are brush discharges, like the crackle that you hear when you pick up a charged photocopy or that you feel when you pull a sweater over your head.
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Science Background: Corona Threshold Voltage
The potential at which corona is found to originate Ohm’s law regime Once the threshold is breached, current increase proportionality with voltage Past the threshold, current increases rapidly and leads to a complete breakdown and arcing or sparking at a point called the breakdown potential
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Science Background: Avalanche Effect
Ionization of neutral atoms becomes possible when the KE of free electrons increase Ionization of neutral atoms becomes possible when the KE of free electrons increase
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Science Background: Paschen’s Curve
V=f(pd) The minimum of this curve corresponds to the minimum Pxd product for which the ionization effect is maximal
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Science Background: Humidity
Partial breakdown threshold reverses from decreasing the threshold to increasing it once the pressure drops below a certain point 20,000-25,000 ft. Humidity can affect the magnitude of the current moving through the ionized air by up to 20% in a pulse corona Pulseless corona and negative corona is not affected by changes in humidity In cases where a pulse corona is created, humidity can affect the magnitude of the current moving through the ionized air by up to 20%
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Science Background: Atmospheric Conditions
This graph lays out the conditions of the atmosphere during flight For the duration of the flight we will be ranging from 0 to ft inside a temp window ranging from bla to bla with presures of bla to bla Flight profile of expected payload environmental conditions
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Science Background: Temperature
Temperature decrease ionization energy increase avalanche effect decrease breakdown voltage increase Temperature decrease ionization energy increase avalanche effect decrease breakdown voltage increase
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Technical Background: Electrodes
Electrode - an electrical conductor that is used to make contact with a nonmetallic part of a circuit An electrode can be classified as either a cad or an depends on its charge or polarity Cathode: negatively charged electrode that attracts cations Anode: positively charged electrode that attracts negatively charged electrons
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Technical Background: Positive vs. Negative Corona
More stable discharge Linearly sensitive to changes in humidity Produces less ozone than negative corona More self-sustaining discharge Humidity has little to no effect Can only be sustained in fluids that contain electronegative molecules
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Technical Background: Electrode Geometry
Point Small surface area Concentrated electric field Different geometries provide varying high-potential surface areas to ionize the gas flowing past them Electrode Geometry For a stable discharge, a point-plane geometry must be used. Since electrons flow from negative to positive, the anode needs to be as pointed as possible, like a needle. This will allow for the avalanche effect to begin. The cathode must then be a plate, to reduce the likelihood of a spark discharge. As the charge moves through the E field, its constructed as it moves back into the smaller surface, therefore causing a pulse corona.
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Technical Background: Electrode Geometry
Plane Evenly distributed electric field Larger surface area
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Technical Background: Electrode Configuration
Point-Plane Surface area ratio Ionization energy The extremely large ratio of surface area between the point and the plane and the concentration of ionization energy built up at the point allows for the lowest onset voltage for corona discharge.
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Technical Background: Electrode Composition
Surface Texture Impurities Surface Area Electrode Material Dielectric Strength Conductivity ough has increased numbers of weak points per unit area of electrode Smooth creates a more uniformed electric field In general, the rougher the surface finish, the lesser the breakdown voltage Impurities are examples of any substances located on the electrodes that would interfere with the conductivity within the medium Examples may be : Condensation and containments Increasing the area of the electrode makes it more difficult to maintain a given breakdown voltage The materials durability (dielectric strength) and conductivity have an effect on the voltage breakdown Steel Copper
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Technical Background: Previous Experiments
A mathematical model of the modified Paschen’s curve for breakdown in microscale gaps Influence of Axial Magnetic Field on the Electrical Breakdown and Secondary Electron Emission in Plane-Parallel Plasma Discharge Stainless steel electrodes Mean discharge current determined by voltage drop over R Breakdown voltage is mean value recorded from Oscil. Copper anode and SS cathode Voltage increased by increments and allowed to settle Current spikes from 1 nA to hundreds of mirco-amps Voltage quickly reduced to zero
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Technical Background: Measurements
Measurements during flight: Temperature Pressure Humidity Voltage Current
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Technical Background: Environmental Sensors
Temperature Sensor Small signal p-n junction diode Pressure Sensor Piezoelectric sensor Humidity Sensor Capacitive sensing element with on-chip integration Temp Sensor - Forward bias voltage of the diode varies linearly with temperature Pressure Sensor - difference in output voltages relates to pressure Humidity Sensor - Outputs a voltage varying linearly with RH
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Technical Background: DC to HVDC Converter
An electronic circuit which converts a source of direct current from one voltage to another Due to the payload size and weight restrictions, the required voltage for discharge is improbable with on-board batteries alone
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Technical Background: Current Sensor
Pico ammeter Voltage drop across resistor Radio Frequency Interference Band of frequencies produces upon discharge Use a circuit diagram for a pico ammeter as a basis and adjust it to measure microamps. Another method is to use measure radio frequency interference. When the corona starts and stops, it will produce radio wave disturbances. So we could have an AM radio wave antenna around the spark gap and identify when the disturbances happen by recording an AM radio frequency and looking at the data.
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Science Requirements: Spark Gap
The gap distance shall be 1mm The electrodes shall be composed of copper The electrodes shall be rough and clear of impurities The electrode configuration shall create a positive corona discharge -The gap distance needs to be 1mm because 1mm is the smallest gap distance that we can accurately measure and still get reliable results. -In order to ensure the accuracy of our results because a previous experiment we are basing our payload on also used copper for their material of choice -The electrode configuration sh-The electrodes shall be rough and cleaned to lower the required breakdown voltage needed to produce a corona discharge all facilitate corona discharge and inhibit sparking in order to ensure the safety of the payload -The discharge shall be stable
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Science Requirements: Power and Sensor
The spark gap shall be provided with a maximum of 4.5kV The payload shall record temperature, pressure, humidity, voltage, and current across the spark gap The payload shall be fully operational throughout the entire flight profile -The spark gap shall be provided with enough of a voltage difference to produce a discharge at ground level with a gap distance of 1mm, which is 4.5kV -The sensors must be operational throughout the flight and must measure temp., pressure, hum., volt., and current across spark gap so that the experiment is a success
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Technical Requirements
The ammeter shall have a minimum accuracy to the microamp range The HVDC shall operate in all environmental conditions The output voltage of the DC to DC converter shall be controlled through an on-board interface All data shall be time-stamped and real-time clock must be synced to the payload GPS - -Like our sensors, the HVDC will remain operational throughout the flight -The output voltage of the DC to DC converter needs to be controllable to ensure safety -All data must be time-stamped and real-time clock must be synced to the payload GPS to ensure accurate altitude data.
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Technical Requirements: LaACES
The payload shall not weigh more than 500 grams The payload shall not exceed 3 oz / in2 on the smallest face The payload equipment shall cost less than $500 The payload shall have two holes 17 cm apart running the length of the payload to comply with LaACES management requirements -The payload shall meet all geometry, mass, and budget requirements set forth by LaACES management
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Project Management: Team Contract
Team Meeting Disciplinary Action Communication Version Control Decision Making Team Roles
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Project Management: Organization
Task Member Project Management Anthony Thompson Science Requirements Chris Rowan Electronics Aaron Wascom Flight Software Mechanical Integration Philip de la Vergne System Testing Brandon Sciortino Calibrations Data Processing and Analysis Documentation
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Change Control & Update Procedures
Changes to this Pre-PDR document shall follow all regulations set by Team Tesla’s contract and only be made after approval by designated representatives from Team Tesla and the LaACES Institution Representative. Document change requests should be sent to Team members and the LaACES Institution Representative and the LaACES Project.
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Project Management: Master Schedule
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Reference Documents :8080/Medical/research/CoronaDischarge.doc - Switzerland
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