GB166317A - Electromagnetic induction micrometers - Google Patents

Electromagnetic induction micrometers

Info

Publication number
GB166317A
GB166317A GB938920A GB938920A GB166317A GB 166317 A GB166317 A GB 166317A GB 938920 A GB938920 A GB 938920A GB 938920 A GB938920 A GB 938920A GB 166317 A GB166317 A GB 166317A
Authority
GB
United Kingdom
Prior art keywords
transformers
armatures
instrument
relative motion
normally
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.)
Expired
Application number
GB938920A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JOSEPH MANNING FORD
Original Assignee
JOSEPH MANNING FORD
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by JOSEPH MANNING FORD filed Critical JOSEPH MANNING FORD
Priority to GB938920A priority Critical patent/GB166317A/en
Publication of GB166317A publication Critical patent/GB166317A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L3/00Measuring torque, work, mechanical power, or mechanical efficiency, in general
    • G01L3/02Rotary-transmission dynamometers
    • G01L3/04Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft
    • G01L3/10Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating
    • G01L3/101Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means
    • G01L3/102Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means involving magnetostrictive means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/16Measuring arrangements characterised by the use of electric or magnetic techniques for measuring the deformation in a solid, e.g. by resistance strain gauge
    • G01B7/24Measuring arrangements characterised by the use of electric or magnetic techniques for measuring the deformation in a solid, e.g. by resistance strain gauge using change in magnetic properties

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

166,317. Ford, J. M. March 31, 1920. Sounding-apparatus. - Small relative movements or changes of length are measured by causing them to vary the flux density or flux distribution in each of two normally balanced magnetic circuits. The application to a differential pyrometer or thermometer is shown in Fig. 1 in which the rods 2, 1 carry respectively iron cored transformers 4, 5, and armatures 7, 8 through which the magnetic circuits of the transformers are completed. The primary windings 11, 12 of the transformers are connected in series and are supplied with alternating or intermittent current. The secondary windings 14, 15 are connected in opposition to one another and in series with an alternating-current measuring-instrument 16. Normally, the air-gaps in the transformers 4, 5 are equal, consequently the secondary electromotive forces neutralize one another. Any relative motion between the rods 1, 2 causes a decrease of one air-gap and an increase in the other, thereby upsetting the balance of the secondary electromotive forces and causing an indication on the instrument 16, the magnitude of which is a measure of the relative motion. The transformers may be auto-connected. In order to distinguish displacements in one direction from those in the other, the secondary current may be rectified. The secondary windings may be wound on the armatures 7, 8 which two armatures may be replaced by one armature, in the form of a cross, between two inwardly facing E- shaped electromagnets. ln a modification, Fig. 2, the armatures 7, 8 are dispensed with and the secondary winding is a coil 19, normally symmetrically disposed in the fields of two electromagnets 17, 18. Relative motion between the coil 19 and the magnets 17, 18 is thereby indicated. A recording-instrument or oscillograph may replace the instrument 16.
GB938920A 1920-03-31 1920-03-31 Electromagnetic induction micrometers Expired GB166317A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB938920A GB166317A (en) 1920-03-31 1920-03-31 Electromagnetic induction micrometers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB938920A GB166317A (en) 1920-03-31 1920-03-31 Electromagnetic induction micrometers

Publications (1)

Publication Number Publication Date
GB166317A true GB166317A (en) 1921-06-30

Family

ID=9871022

Family Applications (1)

Application Number Title Priority Date Filing Date
GB938920A Expired GB166317A (en) 1920-03-31 1920-03-31 Electromagnetic induction micrometers

Country Status (1)

Country Link
GB (1) GB166317A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE744902C (en) * 1937-06-19 1944-01-29 Versuchsanstalt Fuer Luftfahrt Device for measuring changes in length on statically and dynamically loaded components

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE744902C (en) * 1937-06-19 1944-01-29 Versuchsanstalt Fuer Luftfahrt Device for measuring changes in length on statically and dynamically loaded components

Similar Documents

Publication Publication Date Title
US2390051A (en) Means for measuring magnetic fields
US2459210A (en) Variable differential transformer
US1952072A (en) Electrical instrument
US2033654A (en) Magnetic measurement
US2788486A (en) Electrical testing apparatus
US3173119A (en) Method of making and adjusting transducer
GB166317A (en) Electromagnetic induction micrometers
US2434547A (en) Electrical gauge circuits
US2058302A (en) Transformer
US1945378A (en) Temperature indicating device
US2405049A (en) Apparatus for detecting small direct currents
US1732715A (en) Electromagnetic induction apparatus
US1806331A (en) Induction meter
US2400308A (en) Electric ratiometer
US2731624A (en) Electromagnetic rod-position indicator
US2307649A (en) Measurement or indication of the thickness of thin sheets, coatings, and the like
US1982344A (en) Electromagnetic apparatus
US3500199A (en) Induction meter having saturable path for working voltage magnetic flux
US2858484A (en) Induction-type alternating-current relays
US3212005A (en) Phase adjusting means for induction meter including voltage flux shunt path having a shorted turn thereon
GB305166A (en) Improvements in or relating to electric signalling systems
US1835969A (en) Transformer
US2137177A (en) Magnetic tester
US1549664A (en) Method and means for measuring frequency
GB377458A (en) Improvements in and relating to electric speed and frequency indicators