A Vacuum Tube Amplifier for Feeble Pulses
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Alessandro Volta and the Discovery of the Battery
1 Primary Source 12.2 VOLTA AND THE DISCOVERY OF THE BATTERY1 Alessandro Volta (1745–1827) was born in the Duchy of Milan in a town called Como. He was raised as a Catholic and remained so throughout his life. Volta became a professor of physics in Como, and soon took a significant interest in electricity. First, he began to work with the chemistry of gases, during which he discovered methane gas. He then studied electrical capacitance, as well as derived new ways of studying both electrical potential and charge. Most famously, Volta discovered what he termed a Voltaic pile, which was the first electrical battery that could continuously provide electrical current to a circuit. Needless to say, Volta’s discovery had a major impact in science and technology. In light of his contribution to the study of electrical capacitance and discovery of the battery, the electrical potential difference, voltage, and the unit of electric potential, the volt, were named in honor of him. The following passage is excerpted from an essay, written in French, “On the Electricity Excited by the Mere Contact of Conducting Substances of Different Kinds,” which Volta sent in 1800 to the President of the Royal Society in London, Joseph Banks, in hope of its publication. The essay, described how to construct a battery, a source of steady electrical current, which paved the way toward the “electric age.” At this time, Volta was working as a professor at the University of Pavia. For the excerpt online, click here. The chief of these results, and which comprehends nearly all the others, is the construction of an apparatus which resembles in its effects viz. -
Parallel-Plate Capacitor
EXPERIMENT E4: Parallel-Plate Capacitor Objectives: • Scientific: Learn about parallel-plate capacitors • Scientific: Learn about multiple capacitors connected in parallel • Skill development: Use curve fitting to find parameters from experimental data Copyright © 2002, The University of Iowa Rev. jg 22 July 2002 Exp. E4: Parallel-Plate Capacitor Introductory Material Capacitance is a constant of proportionality. It relates the potential difference V between two conductors to their charge, Q. The charge Q is equal and opposite on the two conductors. The relationship can be written: Q = CV (4.1) The capacitance C of any two conductors depends on their size, shape, and separation. + schematic symbols capacitor battery One of the simplest configurations is a pair of flat conducting plates, which is called a “parallel-plate capacitor.” Theoretically, the capacitance of parallel-plate capacitors is CP = ε0 A/ d (4.2) where the subscript “P” denotes “parallel plate.” Here, A is the area of one of the plates, d is the distance between them, and ε0 is a constant called the “permittivity of free space,” which has a value of 8.85 × 10-12 C2 / N-m2, in SI units. Here is the basic idea of the experiment you will do. Suppose that you had a parallel-plate capacitor with the plates separated initially by a distance d0, and you applied a charge Q0 to the electrodes, so that they initially have a potential V0 = Q0 / Cp. Suppose that you then arranged for the two electrodes to be electrically insulated, so that the charge Q could not go anywhere. What would happen if you then increased the electrode separation d? The charge would remain constant, because it has nowhere to flow, whereas the capacitance would decrease, as shown in Eq. -
ECE 340 Lecture 22 : Space Charge at a Junction
ECE 340 Lecture 22 : Space Charge at a Junction Class Outline: •Space Charge Region Things you should know when you leave… Key Questions • What is the space charge region? • What are the important quantities? • How are the important quantities related to one another? • How would bias change my analysis? M.J. Gilbert ECE 340 – Lecture 22 10/12/11 Space Charge Region To gain a qualitative understanding of the solution for the electrostatic variables we need Poisson’s equation: Most times a simple closed form solution will not be possible, so we need an approximation from which we can derive other relations. Consider the following… Doping profile is known •To obtain the electric field and potential we need to integrate. •However, we don’t know the electron and hole concentrations as a function of x. •Electron and hole concentrations are a function of the potential which we do not know until we solve Poisson’s equation. Use the depletion approximation… M.J. Gilbert ECE 340 – Lecture 22 10/12/11 Space Charge Region What does the depletion approximation tell us… 1. The carrier concentrations are assumed to be negligible compared to the net doping concentrations in the junction region. 2. The charge density outside the depletion region is taken to be identically zero. Poisson equation becomes… Must xp = xn? M.J. Gilbert ECE 340 – Lecture 22 10/12/11 Space Charge Region We are already well aware of the formation of the space charge region… The space charge region is characterized by: Na < Nd •Electrons and holes moving across the junction. -
Varian Mw 3 % H
ORNL/Sub-75/49438/2 BP n ^TfFl varian mw 3 % h NOTICE PORTIONS OF TV'!? HFTL0'' SHE M.I.HGIB'.E. IF lT~~rvnrT;irri*"rr?.--p. tf.3 iwaito'jia 1 co1;;/ -o psrrnii the broadest possible avail- ability. FINAL REPORT MILLIMETER WAVE STUDY PROGRAM u by H.R. JORY, E.L. LIEN and R.S. SYMONS ft, 0 {I Order No. Y-12 11Y-49438V j November 1975 report prepared by Varian Associates Palo Alto Microwave Tube Division 611 Hansen Way o Palo Alto, California 94303 under subcontract number 11Y-49438V ; for ' ' r>4 OAK RIDGE NATIONAL LABORATORY * ° Oak Ridge, Tennessee 37830 operated by UNION CARBIDE CORPORATION for the nrsTKIUUTiON 01? 'ijl;.;?!---''--^-'.^-^''' UNLLMIT DEPARTMENTS ENERGY FINAL REPORT MILLIMETER WAVE STUDY PROGRAM by H. R. Jory, E. L Lien and R, S. Symons - NOTICE- Urn report Mas piepated as an account, of worl; sponsored by die Untied Stales Government. Neither Die United State* not the United States Pepastment of l.nergy, tiar any of1 their employees, nnr any of then contractors. subcontractor or their employees, makes any warranty, express or implied, or assumes any legal liability oi responsibility for tlie accuracy, completeness of usefulness of any information, apparatus, product or process disclovd. or represents that its use would not mUmfe pnvately owned npjits. Order No, Y-12UY-49438V November 1975 « 0 " report prepared by Varian Associates Palo Alto Microwave Tube Division 611 Hansen Way Palo Alto, California 94303 K< under subcontract number 11Y-49438V for OAK RIDGE NATIONAL LABORATORY Oak.RitJge-J'ennessee 37830 c.-..operatedjby U N 10N CARBiDE^G0RP0RATI0N, o <J>c l . -
High Resistance Measurements Introduction
1689 App Note 312 11/10/05 11:12 AM Page 1 Number 312 Application Note High Resistance Series Measurements Introduction R Resistance is most often measured with a digital multimeter, which can make measurements up to about 200MΩ. However, in some cases, resistances in the gigohm and higher ranges must be HI measured accurately. These cases include such applications as VA characterizing high megohm resistors, determining the resistivity of insulators and measuring the insulation resistance of printed LO circuit boards. These measurements are made by using an elec- trometer, which can measure both very low current and high Figure 1: The constant voltage method for measuring resistance impedance voltage. Using an electrometer, resistances up to constant current sources so that either the constant voltage or the 1018Ω can be measured depending on the method used. One method is to source voltage and measure current and the other constant current method can be used to measure high resistance. method is to source current and measure voltage. Besides using For accurate measurements, the high impedance terminal the proper method and instrumentation, special measurement of the ammeter is always connected to the high impedance point techniques such as shielding and guarding must be used to mini- of the circuit being measured. If not, erroneous measurements mize leakage current, noise and other undesirable effects that can may result. degrade the accuracy of the measurements. Some of the applications which use this method include: testing two-terminal high resistance devices, measuring insula- tion resistance, and determining the volume and surface resistivi- Measurement Methods ty of insulating materials. -
RESEARCH for DEVELOPMENT of THIN-FILM SPACE-CHARGE-LIMITED TRIODE DEVICES (U) by Kenneth G. Aubuchon, Peter Knoll and Rainer
RESEARCH FOR DEVELOPMENT OF THIN-FILM SPACE-CHARGE-LIMITED TRIODE DEVICES (U) BY Kenneth G. Aubuchon, Peter Knoll and Rainer Zuleeg May 1967 Distribution of this report is provided in the interest of information exchange and should not be construed as endorse- ment by NASA of the material presented. Responsibility for the contents resides in the organization that prepared it. Prepared under Contract No. NAS 12-144 by: Hughes Aircraft Company Applied Solid State Research Department Newport Beach, California Electronics Research Center National Aeronautics & Space Administration RESEARCH FOR DEVELOPMENT OF THIN-FILM SPACE-CHARGE-LIMITED TRIODE DEVICES (U) BY Kenneth G. Aubuchon, Peter Knoll and Rainer Zuleeg May 1967 Prepared under Contract No. NAS 12-144 by: Hughes Air craft Company Applied Solid State Research Department Newport Beach, California for Electronics Research Center National Aeronautics & Space Administration TABLE OF CONTENTS SECTION TITLE PAGE NO: ABSTRACT ii FORE WORD iii LIST OF ILLUSTRATIONS iv I MATERIAL PREPARATION AND ANALYSIS 1 A. Introduction 1 B. Literature Survey 1 C. Experimental 3 D. Results 6 E. Discussion 13 I1 DEVICE THEORY 18 I11 DEVICE DESIGN AND FABRICATION 20 A. Mask Design 20 B. Silicon Processing 24 C. Discussion of Processing Problems 25 D. Summary of Lots Fabricated 27 E. Discussion of Yield 29 IV DEVICE EVALUATION 32 A. Correlation Between Theory and Experiment 32 B. High Frequency Performance 42 C. Modes of Operation 49 D. High Temperature Stability 54 E. Radiation Effects 54 F. Noise 62 V CONCLUSION 64 LIST OF REFERENCES 66 ABSTRACT Silicon-on- sapphire space - charge-limited triodes were de signed and fabricated. -
A Simple Atmospheric Electrical Instrument for Educational Use
A simple atmospheric electrical instrument for educational use A.J. Bennett1 and R.G. Harrison Department of Meteorology, The University of Reading P.O. Box 243, Earley Gate, Reading RG6 6BB, UK Abstract Electricity in the atmosphere provides an ideal topic for educational outreach in environmental science. To support this objective, a simple instrument to measure real atmospheric electrical parameters has been developed and its performance evaluated. This project compliments educational activities undertaken by the Coupling of Atmospheric Layers (CAL) European research collaboration. The new instrument is inexpensive to construct and simple to operate, readily allowing it to be used in schools as well as at the undergraduate University level. It is suited to students at a variety of different educational levels, as the results can be analysed with different levels of sophistication. Students can make measurements of the fair weather electric field and current density, thereby gaining an understanding of the electrical nature of the atmosphere. This work was stimulated by the centenary of the 1906 paper in which C.T.R. Wilson described a new apparatus to measure the electric field and conduction current density. Measurements using instruments based on the same principles continued regularly in the UK until 1979. The instrument proposed is based on the same physical principles as C.T.R. Wilson's 1906 instrument. Keywords: electrostatics; potential gradient; air-earth current density; meteorology; Submitted to Advances in Geosciences 1 E-mail: [email protected] 1 1. Introduction The phenomena of atmospheric electricity provide an ideal topic for stimulating lectures, talks and laboratory demonstrations. -
Experiment 0 an Introduction to the Equipment
Experiment 0 An Introduction to the Equipment Objectives After completing Experiment 0, you should be able to: • Use basic electronic instruments • Determine the precision of a measurement • Select the scale that gives the most accurate reading • Give a qualitative description of electric potential (voltage), current, and resistance • Describe the uses of an electrometer, voltmeter, ammeter, ohmmeter, and multimeter • Use an electrometer and digital multimeter properly • Describe the precautions required to protect meters from damage. Introduction In Physics 116L, you will investigate the properties of electricity and magnetism with a variety of laboratory instruments. Unlike mechanics, for which the basic measurements of length, time, and mass are familiar, common quantities, electricity and magnetism involve unfamiliar quantities and require special instruments for their study. Some of the measurements are quite simple, for example the circuits of Experiments 5 and 6, but others are more subtle. Although you are certainly familiar with certain aspects of basic electricity -- shocks upon touching metal objects on dry days, the quantitative experiments are not trivial. You must understand a number of physical processes and phenomena to form a conceptual picture of what is happening in these experiments. We cannot explore electrostatics one step at a time as in the lectures; understanding even the simplest experiments requires the complete framework of electrostatics. These first three experiments, which introduce you to electrical instruments and the basic properties of electric charge, require considerable thought and care. If you are unfamiliar with these instruments, you may find them slightly intimidating at first. However, they are not really difficult to use. This first "experiment" is merely a set of exercises to enable you to experiment with the basic instruments and become comfortable with using them. -
Grid Pentode
512 RADIO -CRAFT April, 1930 The A. C. Screen -Grid Pentode The five- electrode tube which introduces revolutionary possibili- ties into radio circuit design, with data as to its characteristics, and suggestions as to circuits adapted for its employment THE progress of tube development, charge to accelerate the flow of electrons (5) A screen -grid which, as in previous which has been rapid during the past from the filament and break up the nega- tuhe types, is connected to the "G" prong three years, made another spurt re- tive "space charge" which surrounded it. of the tube base. Upon this is impressed cently with the appearance of a new This "space- charge" hook -up is preferred a high positive voltage, somewhat lower American "pentode," or "five -element" tube; for audio amplification. than that of the plate. It serves the pur- which was demonstrated in this city to In the new pentode (styled the "P-1" by pose of eliminating the capacitive effect be- radio engineers late in January, and will, its manufacturer, the CeCo Mfg. Co.) both tween plate and control -grid. it was then stated, be available on the (6) A plate, which is similar to that of market alwut the time of the appearance the '24, and connected to the "P" prong of of this issue of RADIO-CRAFT. the tube. This tube (unlike the British pentode, The tube itself, a view of whose elements which has been used as a power tube only, is given herewith, fits the standard UY tube for the past two years) is designed espe- socket; it is 1 13/16 inches in diameter, and cially as a radio- frequency amplifier, to 51/4 inches high. -
Frequency Characteristics of the Electron-Tube Oscillation Generator
FREQUENCY CHARACTERISTICS OF THE ELECTRON—TUBE OSCILLATION GENERATOR BY RAY STUART QUICK B. S. University of California, 1916 THESIS Submitted in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE IN ELECTRICAL ENGINEERING IN THE GRADUATE SCHOOL OF THE! UNIVERSITY OF ILLINOIS 1919 UNIVERSITY OF ILLINOIS THE GRADUATE SCHOOL I HEREBY RECOMMEND THAT THE THESIS PREPARED UNDER MY SUPERVISION BY Hay Stuart 4uick ENTITLED Jgraqstaney Character i st.i cs of the Electron-Tube Oscillation Generator BE ACCEPTED AS FULFILLING THIS PART OF THE REQUIREMENTS FOR THE DEGREE OF Master of Snionoe in Eleotri nol Engin eering . \Mm Head of Department Recommendation concurred in :! Committee on Final Examination* *Required for doctor's degree but not for master's 1 CONTENTS I INTRODUCTION Page 1. Scope of work 2 2. Historical review. 2 II THEORETICAL DISCUSSION OP PROBLEM 1. General principles of operation. 4 2. Circuits used. 6 3. Work of previous investigators. 6 4. Mathematical solution of circuits. 8 III APPARATUS AND METHODS 1. Electron- tubes used. 13 2. Circuit properties. 13 3. Frenuency determinations. 13 IV DATA AND EXPERIMENTAL RESULTS 1. Observed conditions necessary for constant eurrent and for oscillating eurrent. 36 2. Oscillograms. 36 3. Experimental results. 37 V CONCLUSIONS 1. Comparison of experimental ^nd theoretical results. 45 2. Suggestions as to future work 45 VI BIBLIOGRAPHY 47 2 I INTRODUCTIOU 1. Scope of Work. The development of the electron- tube ( also called three-electrode vacuum tube, vacuum- tube, thermionic amplifier, audion, etc. ) has brought to light many new and interest- ing problems. In using the tube as a source of continuous oscilla- tions it is desirable to be able to predetermine the frequency, wave-form and amplitude characteristics. -
High Accuracy Electrometers
www.keithley.com HighHigh accuracyaccuracy electrometerselectrometers forfor lowlow current/highcurrent/high resistanceresistance applicationsapplications A GREATER MEASURE OF CONFIDENCE KEITHLEY INSTRUMENTS ARE AT WORK AROUND THE WORLD KEITHLEY INSTRUMENTS ARE AT 1EΩ 1PΩ µ 1TΩ 1 C 1GΩ 1nC 1MΩ 1kΩ 1pC 1Ω 6430 6517 6514 1mΩ 1fC Resistance Measurement Ranges 6514 6517A Charge Measurement Ranges 1kV 1A 1mA 1V 1µA 1nA 1mV 1pA 1fA 1µV 1aA 6430 6517/6514 6430 6517/6514 Voltage Measurement Ranges Current Measurement Ranges High performance electrometers MEASUREMENTS FAR BEYOND THE RANGE OF CONVENTIONAL INSTRUMENTATION MEASUREMENTS FAR Keithley has more than a half-century of experience in designing and producing sensitive instrumentation. As new testing requirements have evolved, we’ve developed dozens of different models to address our customers’ needs for higher resolution, accuracy, and sensitivity, as well as support for specific applications. Keithley electrometers are at work around the world in production test applications, industrial R&D centers, and university and government laboratories—wherever people need to make high precision current, voltage, resistance, or charge measurements. What is an electrometer? Why is low voltage burden critical? Essentially, an electrometer is a highly refined digital multimeter Voltage burden is the voltage that appears across the ammeter (DMM). Electrometers can be used for virtually any measurement input terminals when measuring. As Figure 1 illustrates, a DMM task that a conventional DMM can and offer the advantages of uses a shunt ammeter that requires voltage (typically 200mV) to very high input resistance when used as voltmeters, and ultra-low be developed across a shunt resistor in order to measure current. -
Limits for Thermionic Emission from Leading Edges of Hypersonic Vehicles
10.2514/6.2016-0507 AIAA SciTech Forum 4-8 January 2016, San Diego, California, USA 54th AIAA Aerospace Sciences Meeting Limits for Thermionic Emission from Leading Edges of Hypersonic Vehicles Kyle M. Hanquist∗ and Iain D. Boydy Department of Aerospace Engineering, University of Michigan, Ann Arbor, MI Abstract Simulations of electron transpiration cooling (ETC) on the leading edge of a hypersonic vehicle using computational fluid dynamics (CFD) are presented. The thermionic emission boundary condition and electric field model including forced diffusion are discussed. Different analytical models are used to describe the plasma sheath physics in order to avoid resolving the sheath in the computational domain. The first analytical model does not account for emission in the sheath model, so the emission is only limited by the surface temperature. The second approach models the emissive surface as electronically floated, which greatly limits the emission. The last analytical approach biases the emissive surface, which makes it possible to overcome space-charge limits. Each approach is compared and a parametric study is performed to understand the effects that the material work function, freestream velocity, and leading edge geometry has on the ETC effect. The numerical results reveal that modeling the sheath as a floated surface results in the emission, and thus ETC benefits, being greatly limited. However, if the surface is negatively biased, the results show that the emission can overcome space-charge limits and achieve the ideal ETC benefits predicted by temperature limited emission. The study also shows that, along with negatively biasing the surface, emission is enhanced by increasing the number of electrons in the external flowfield by increasing the freestream velocity.