Science and the Instrument-Maker
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IT Legacy Article Compendium
An IT Legacy Booklet March 2016 IT Legacy Article Compendium 1 INTRODUCTION – LOWELL A. BENSON, EDITOR Write a Book? How about an autobiography? Shortly after the Information Technology (IT) Legacy Committee was formed, Dick Lundgren began to write Legacy articles for the VIP Club newsletter. During the committee’s decade of volunteering, several other committee members have also written Legacy associated newsletter items. This booklet1 is a collection of those VIP Club newsletter articles. The first several articles are the history of the Legacy Committee as we felt our way through the quagmire of gathering documents and hardware artifacts and then cataloging them. So, to some degree, this is both a book and the IT Legacy Committee’s autobiography. This book complements our December 2015 ‘Article for the Month’. That too was a booklet: Measuring Success = Volunteer Hours; recapping a decade with summaries of over 100 on-line IT Legacy articles. I dedicate this document to James 'Rapp' Rapinac who passed away 23 January 2016. Rapp was a steadfast supporter of our legacy initiatives and a good friend. LABenson If you are using Adobe reader; clicking on any section in the table of contents will get you there. 2 TABLE OF CONTENTS 1 Introduction – Lowell A. Benson, editor ......................................................................................... 1 3 2006, First Year Articles ................................................................................................................. 8 3.1 March 2006 – Richard Lundgren ........................................................................................... -
Aircraft Propellers
U.S. WORKS PROGRESS ADMINISTRATION BIBLIOGRAPHY OF A E R 0 N A U T I C S Part 27 - Aircraft Propellers Compiled from the INDEX OF AERONAUTICS of the INSTITUTE OF THE AERONAUTICAL SCIENCES 30 Rockefeller Plaza New York City The Index and Bibliographies have been prepared by workers under the supervision of the U.S. WORKS PROGRESS ADMINISTRATION Cecil A. Ross Senior Project Supervisor Project 465-97-S-S1 (Formerly 165-97-6055) 19 3 7 FOREWORD This bibliography is one of a series which aims to cover a large part of aeronautical literature. It is pub lished by the U. S. Works Progress Administration Project 465-97-3-21 (formerly 165-97-6055) under the sponsorship of the New York City Department of Docks with the cooperation of the Institute of the Aeronautical Sciences. Request for Additions The Institute of the Aeronautical Sciences which is directing the U. S. Works Progress Administration staff of workers will appreciate receiving additional references, corrections and criticism, so that the bibliographies will be.more helpful when issued in final form. Request for Copies The bibliographies have been prepared with funds allotted by the U. S. Works Progress Administration. They may not be sold. Persons and organizations wishing to procure copies may apply for them by letter, stating the use for which they are needed. When it is possible to prepare additional copies such requests will receive first consideration. Robert R. Dexter Aeronautical Engineer Address all correspondence to: John R. Palmer Managing Project Supervisor U- S. Works Progress Administration 5111 R.C.A. -
3D Rigid Body Dynamics: Tops and Gyroscopes
J. Peraire, S. Widnall 16.07 Dynamics Fall 2008 Version 2.0 Lecture L30 - 3D Rigid Body Dynamics: Tops and Gyroscopes 3D Rigid Body Dynamics: Euler Equations in Euler Angles In lecture 29, we introduced the Euler angles as a framework for formulating and solving the equations for conservation of angular momentum. We applied this framework to the free-body motion of a symmetrical body whose angular momentum vector was not aligned with a principal axis. The angular moment was however constant. We now apply Euler angles and Euler’s equations to a slightly more general case, a top or gyroscope in the presence of gravity. We consider a top rotating about a fixed point O on a flat plane in the presence of gravity. Unlike our previous example of free-body motion, the angular momentum vector is not aligned with the Z axis, but precesses about the Z axis due to the applied moment. Whether we take the origin at the center of mass G or the fixed point O, the applied moment about the x axis is Mx = MgzGsinθ, where zG is the distance to the center of mass.. Initially, we shall not assume steady motion, but will develop Euler’s equations in the Euler angle variables ψ (spin), φ (precession) and θ (nutation). 1 Referring to the figure showing the Euler angles, and referring to our study of free-body motion, we have the following relationships between the angular velocities along the x, y, z axes and the time rate of change of the Euler angles. The angular velocity vectors for θ˙, φ˙ and ψ˙ are shown in the figure. -
Chapter 7 – Autopilot Models for Course and Heading Control
Chapter 7 – Autopilot Models for Course and Heading Control 7.1 Autopilot Models for Course Control 7.2 Autopilot Models for Heading Control Automatic pilot, “also called autopilot, or autohelmsman, device for controlling an aircraft or other vehicle without constant human intervention.” Ref. Encyclopedia Britannica The first aircraft autopilot was developed by Sperry Corporation in 1912. It permitted the aircraft to fly straight and level on a compass course without a pilot's attention, greatly reducing the pilot's workload. Elmer Ambrose Sperry, Sr. (1860–1930) Lawrence Sperry (the son of famous inventor Elmer Sperry) demonstrated it in 1914 at an aviation safety contest held in Paris. Sperry demonstrated the credibility of the invention by flying the aircraft with his hands away from the controls. He was killed in 1923 when his aircraft crashed in the English channel. In the early 1920s, the Standard Oil tanker J.A. Moffet became the first ship to use an autopilot. Ref. Wikipedia Lawrence Burst Sperry (1892—1923) 1 Lecture Notes TTK 4190 Guidance, Navigation and Control of Vehicles (T. I. Fossen) Chapter Goals • Be able to explain the differences of course and heading controlled marine craft. In what applications are they used. • Understand what the crab angle is for a marine craft: • Understand why heading control is used instead of course control during stationkeeping. • Be able to compute the COG using two waypoints • Know what kind of sensors that give you a direct measurement of SOG and COG under water and on the surface. • Understand the well-celebrated Nomoto models for heading and course control, and it is extension to nonlinear theory (maneuvering characteristics) • Be able to explain what the pivot point is. -
Elmer Ambrose Sperry Papers 1893
Elmer Ambrose Sperry papers 1893 This finding aid was produced using ArchivesSpace on September 14, 2021. Description is written in: English. Describing Archives: A Content Standard Manuscripts and Archives PO Box 3630 Wilmington, Delaware 19807 [email protected] URL: http://www.hagley.org/library Elmer Ambrose Sperry papers 1893 Table of Contents Summary Information .................................................................................................................................... 3 Biographical Note .......................................................................................................................................... 3 Scope and Content ......................................................................................................................................... 4 Administrative Information ............................................................................................................................ 7 Related Materials ........................................................................................................................................... 7 Controlled Access Headings .......................................................................................................................... 8 Collection Inventory ....................................................................................................................................... 8 Personal ....................................................................................................................................................... -
Massachusetts Institute of Technology Bulletin
PRES IDENT'S REPO RT ISSUE Volume ninety, Number two a November, 1954 MASSACHUSETTS INSTITUTE OF TECHNOLOGY BULLETIN _ _I ___ I __ ~~~ Entered July 3, 1933, at the Post Ofice, Boston, Massachusetts, as second-class matter, under Act of Congress of August 24, 1912 Published by the MASSACHUSETTS INSTITUTE OF TECHNOLOGY, Cambridge Station, Boston, Massachusetts, in March, June, July, October and November. Issucs of the Bulletin include the REPORTS OF THE PRESIDENT and OF THE TREASURER, the SUMMER SESSION CATALOGUE, the GENERAL CATALOGUE, and THIS IS M. I. T. Published under the auspices of the M. I. T. Ofice of Publications __ Massachusetts Institute of Technology Bulletin PRESIDENT'S REPORT ISSUE Volume 90, Number 2 . November, 1954 _~1·_1__1_·_1 1--~111.1~^~-·~-····IIY·i The Corporation, 1954-1955 President: JAMES R. KILLIAN, JR. Vice-President and Provost: JULIUS A. STRATTON Vice-President and Treasurer:JosEPH J. SNYDER Vice-President for Industrial and Government Relations: EDWARD L. COCHRANE Secretary: WALTER HUMPHREYS LIFE MEMBERS WALTER HUMPHREYS RALPH E. FLANDERS DUNCAN R. LINSLEY JOHN R. MACOMBER JAMES M. BARKER THOMAS D. CABOT ALFRED L. LooMIS THOMAS C. DESMOND CRAWFORD H. GREENEWAL r HARLOW SHAPLEY J. WILLARD HAYDEN JAMES McGowAN, JR. ALFRED P. SLOAN, JR. MARSHALL B. DALTON HAROLD B. RICHMOND REDFIELD PROCTOR ROBERT E. WILSON LLOYD D. BRACE GODPREY L. CABOT DONALD F. CARPENTER THOMAS D'A. BROPHY BRADLEY DEWEY HORACE S. FORD WILLIAM A. COOLIDGE FRANCIS J. CHESTERMAN GEORGE A. SLOAN MERVIN J. KELLY VANNEVAR BUSH WALTER J. BEADLE ROBERT T. HASLAM WILLIAM EMERSON B. EDWIN HUTCHINSON RALPH LOWELL IRVING W. -
Basic Instruments Introduction Instruments Mechanically Measure Physical Quantities Or Properties with Varying Degrees of Accuracy
Chapter 3 Basic Instruments Introduction Instruments mechanically measure physical quantities or properties with varying degrees of accuracy. Much of a navigator’s work consists of applying corrections to the indications of various instruments and interpreting the results. Therefore, navigators must be familiar with the capabilities and limitations of the instruments available to them. A navigator obtains the following flight information from basic instruments: direction, altitude, temperature, airspeed, drift, and groundspeed (GS). Some of the basic instruments are discussed in this chapter. The more complex instruments that make accurate and long distance navigation possible are discussed in later chapters. 3-1 Direction The force of the magnetic field of the earth can be divided into two components: the vertical and the horizontal. The Basic Instruments relative intensity of these two components varies over the The navigator must have a fundamental background in earth so that, at the magnetic poles, the vertical component navigation to ensure accurate positioning of the aircraft. Dead is at maximum strength and the horizontal component is reckoning (DR) procedures aided by basic instruments give minimum strength. At approximately the midpoint between the navigator the tools to solve the three basic problems of the poles, the horizontal component is at maximum strength navigation: position of the aircraft, direction to destination, and the vertical component is at minimum strength. Only and time of arrival. Using only a basic instrument, such as the the horizontal component is used as a directive force for a compass and drift information, you can navigate directly to magnetic compass. Therefore, a magnetic compass loses its any place in the world. -
GYROCOMPASS CMZ 900 Series
GYROCOMPASS CMZ 900 series Bulletin 80B10M09E 2nd Edition CMZ 900 GYROCOMPASS is highly reliable and long life. CONTROL BOX (MKC 326/327) MASTER COMPASS (MKM 026) A gyrocompass detects the true north by means of a fast-spinning rotor, which is suspended with no friction and is influenced by gravity and rotation of the Earth. A gyrocompass consequently indicates a ship's heading. CMZ 900 series has been type approved in accordance with International Maritime Organization (IMO) standards, resolution A.424(XI) as well as JIS-F9602, class A standards. FEATURES -A modular design saves the space. MASTER COMPASS can be integrated in the autopilot steering stand. -Manual and automatic speed error correction -External heading sensor can back up the heading outputs. -Serial data output IEC 61162-2 (high-speed transmission) -An unique anti-vibration mechanism enhanced by the velocity damping effect of high viscous oil, provides superior damping of vibration and decoupling of shock at sea. -A small and lightweight container enhances the follow up speed. The gyrocompass reading changes smoothly and does not lag when a small ship rapidly changes course. -Easy maintenance and long maintenance periods Titanium capsule and electrodes are employed for GYROSPHERE. Purity is maintained inside of the container, and maintenance interval is then longer-dated. The container is divided into two pieces at bottom when overhauled. Ship's crew can replace GYROSPHERE in case of emergency. Easy maintenance Titanium capsule PERFORMANCE and electrodes SPECIFICATIONS (lower hemisphere) -Accuracy: Static:±0.25° x sec Lat. Dynamic:±0.75° x sec Lat. -Settling time:Within 5 hours -Follow up accuracy:0.1° or less -Max. -
Article, the Extravagantly Named German Scien- at Different Constant Velocities
PaRT I: gyRoScoPES aNd aLBERT EINSTEIN FRoM ThE IoN hISToRIaN, MaRvIN May Elmer A. Sperry and the Gyrocompass His company became Unisys, the giant computer and informa- tion technology company, and his gyroscope-guided autopilot became known as “metal Mike,” the mechanical helmsman. lmer Ambrose Sperry was born a year accepted at that time. Although unable to Ebefore the Civil War began, but the gyro- demonstrate an actual north-pointing gyro- compasses, inertial navigators and voyage compass using his string-propelled gyroscope managements systems that stem from his (electric motors being unavailable at the innovations still steer our ships and aircraft. time), Foucault did establish the theoretical Indeed, few pioneers of navigation have left basis for the gyrocompass. as enduring a legacy. By the late 19th century, iron ships had In 1880, the 20-year-old New Yorker largely replaced wooden ships, jeopardizing Elmer Sperry at age 27 formed his first company. By 1986, Sperry the integrity of the magnetic compass, which Corporation, a merger of all eight companies for 400 years had been the navigator’s most compass was an ingenious notion, several he founded to manufacture and market his reliable course indicator. problems presented themselves to Sperry and many inventions, had become Unisys, the The age of electrification began around others who were working on the same idea. giant information technology firm. the same time, when scientists such as Max- A 1912 publication of U.S. Naval Proceedings The brilliant inventor, engineer, and well, Faraday, Helmholz, Einstein, Steinmetz, outlines these challenges: entrepreneur held 135 patents and became and Edison advanced the theoretical and 1. -
PR-2000Series
DIMENSIONS ■ Rudder angle indicator(for JG ships) 150 106 130 4-φ8HOLES 90 142 Autopilot 70 10 70 10 106 134 160 140 4-φ4.5HOLES - Series 4-φ6.5HOLES PR 2000 250 134 13 134 124 110 ■ Repeat back unit(for 35~45゚) ■ Repeat back unit(for 60~70゚) 140° φ8.2HOLE φ 32 32 8.2HOLE 90° 4-φ12HOLES 4-φ12HOLES 100~400 100~400 114 80 80 171 171 45.5 20 284 20 20 284 45.5 324 80 324 13 32 80 13 5.6 240 5.6 256 240 15 35 15 Design and specifications are subject to change without prior notice, and without any obligation on the part of the manufacturer. Before operating this equipment, CAUTION you should first throughly read the operator's manual. www.tokyo-keiki.co.jp/marine/e/ Marine Systems Company Head Office 2-16-46, Minami-Kamata, Ohta-ku, Tokyo 144-8551 JAPAN Tel. +81-3-3737-8611 Fax. +81-3-3737-8663 TOKYO KEIKI (SHANGHAI) CO., LTD. C-1407, Orient International Plaza. No.85 Lou Shan Guan Rd., Shanghai 200336. CHINA Tel. +86-21-3223-1252 Fax. +86-21-6278-7667 TOKYO KEIKI U.S.A., INC. 625 Fair Oaks Ave, Suite190, South Pasadena, California 91030 U.S.A. Tel. +1-626-403-1500 Fax. +1-626-403-7400 Busan Liaison Office Shindonga bldg. Room 1003, 749-1 Gayadaero, Busanjin-gu, Busan 614-783, KOREA Tel. +82-51-802-2190 Fax. +82-51-802-2188 Singapore Branch No.2 Jalan Rajah #07-26/28, Golden Wall Flatted Factory, Singapore 329134 Tel. -
Zucchini Frittata
Please cite as: Spinzia, Raymond E., “The Involvement of Long Islanders in the Events Surrounding German Sabotage in the New York Metropolitan Area 1914-1917,” 2019. www.spinzialongislandestates.com The Involvement of Long Islanders in the Events Surrounding German Sabotage in the New York Metropolitan Area 1914-1917 by Raymond E. Spinzia In order to assist the reader in identifying the large number of unfamiliar names and the dizzying array of events, a photographic gallery with a thumbnail biography of the participants and a timeline pertaining to the pertinent events of those years have been included. In 1908 Washington was considered a backwater posting by the major powers in Europe. Washingtonians, at the beginning of the twentieth century, had to contend with excessively humid heat in the summer coupled with the fear of typhoid- and malaria-bearing mosquitos from the swamps of the nearby countryside. Additionally, the city’s social life lacked the sophistication and glitter associated with Manhattan and the capitals of the major countries of Western Europe. Despite this, Germany appointed the shrewd career diplomat Count Johann Heinrich von Bernstorff as its ambassador to the United States. Von Bernstorff, who was debonair and likeable, had close ties to Long Island and a grasp of America’s culture, politics, and economic potential, arrived in the United States on December 21, 1908.1 His South Shore country residence, Hickory Hall, that he rented from Mrs. Thomas F. White was at Central Avenue and White Lane in Long Island’s village -
Care and Feeding of Autopilots
BOATKEEPER Care and Feeding of Autopilots From Pacific Fishing, December 1998 By Terry Johnson, University of Alaska Sea Grant, Marine Advisory Program 4014 Lake Street, Suite 201B, Homer, AK 99603, (907) 235-5643, email: [email protected] ny device that simplifies matters for work on either a wet card or fluxgate com- cal, and the whole thing must be mounted Athe vessel operator must itself be com- pass, both of which respond to the earth’s where it is out of the weather and out of the plex; so it is with autopilots. magnetic field. Naturally, they also respond way but still has correct angle and rigidity In concept, the modern autopilot is to any other magnetic field in the boat, in- to impart full torque on the steering gear. If pretty simple. A compass indicates the cluding the engine block and electrical cir- the salesman doesn’t know exactly how to boat’s actual heading, a control unit accepts cuitry. Also, they are greatly affected by calculate sprocket size and other factors, get the heading the operator wants, a micropro- motion, including rolling, pitching, and an engineer to help you work it out. Big cessor calculates the difference between the pounding. To minimize motion the compass problems result from improper sizing. On desired and actual headings, and a power must be mounted low in the boat, prefer- hydraulic units, you need to know the ram unit acts on instructions from the control ably at the waterline and slightly forward size on your steering gear to select the cor- unit to move the rudder and turn the boat of amidships, close to the centerline.