SU150166A1 - Device for measuring angular accelerations - Google Patents

Device for measuring angular accelerations

Info

Publication number
SU150166A1
SU150166A1 SU746143A SU746143A SU150166A1 SU 150166 A1 SU150166 A1 SU 150166A1 SU 746143 A SU746143 A SU 746143A SU 746143 A SU746143 A SU 746143A SU 150166 A1 SU150166 A1 SU 150166A1
Authority
SU
USSR - Soviet Union
Prior art keywords
rotor
angular accelerations
measuring angular
winding
measuring
Prior art date
Application number
SU746143A
Other languages
Russian (ru)
Inventor
В.И. Долина
Original Assignee
В.И. Долина
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 В.И. Долина filed Critical В.И. Долина
Priority to SU746143A priority Critical patent/SU150166A1/en
Application granted granted Critical
Publication of SU150166A1 publication Critical patent/SU150166A1/en

Links

Description

Предлагаемое устройство дл  измерени  угловых ускорений относитс  к известному типу устройств того же целевого назначени , выполненных в виде электрической -машины с лолым ротором и со статором , имеющим обмотку возбуждени , питаемую посто нным током, или посто нные магниты, а также измерительную обмотку, э.д.с. в которой пропорциональна угловому ускорению.The proposed device for measuring angular accelerations refers to a known type of devices of the same purpose, made in the form of an electric machine with a light rotor and a stator having an excitation winding fed by direct current or permanent magnets, as well as a measuring winding, e. DS in which is proportional to angular acceleration.

Особенностью устройства, составл ющего предмет изобретени ,  вл етс  расположение указанной измерительной обмотки как вне, так и внутри ротора в плоскост х, параллельных его оси, причем части этой обмотки намотаны и соединены так, что э.д.с. от полезного магнитного потока в них складываютс , а от внешнего лотока взаимно уравновешиваютс , чем обеспечиваетс  исключение вли ни  внешних магнитмых полей.A feature of the device constituting the subject matter is the location of said measuring winding, both outside and inside the rotor, in planes parallel to its axis, with parts of this winding being wound and connected so that emf. from the useful magnetic flux in them are added up, and from the external tray are mutually balanced, thus eliminating the influence of external magnetic fields.

На чертеже, изображаюш,ем принципиальную схему предлагаемого устройства, выполненного IB видеМашины с посто нными магнитами, прин ты следующие обозначени : 1 - магнитопровод, 2-посто нные магниты, 3 - полюсные наконечники, 4 - полый ротор, 5 - часть измерительной обмотки, расположенна  внутри ротора, и 5- часть ее, расположенна  вне ротора, 7 - гальванометр осциллографа.In the drawing, a schematic diagram of the proposed device made in an IB type machine with permanent magnets, the following notation is adopted: 1 - magnetic circuit, 2-permanent magnets, 3 - pole tips, 4 - a hollow rotor, 5 - part of the measuring winding, located inside the rotor, and 5- part of it, located outside the rotor, 7 - oscilloscope galvanometer.

Посто нные магниты 2 создают поток Фр,  вл ющийс  результирующим потоком, действующим в воздушном зазоре.The permanent magnets 2 create a flow FR, which is the resultant flow acting in the air gap.

При вращении -полого ротора 4 с измерительной обмоткой, состо щей из двух частей, расположенных вне и внутри ротора, возникают от потока Фр токи, создающие потоки Фи и Фи-. Обе части 5 к 6 измерительной обмотки расположены в плоскост х, параллельных оси ротора, причем намотка и соединение этих обеих частей выполнены так, что э.д.с. от полезных потоков Фи и Фи складываютс , а от внешнего потока Фв взаимно уравновешиваютс .During the rotation of the ол-hollow rotor 4 with a measuring winding consisting of two parts, located inside and outside the rotor, arise from the flow of the Fcurrent, which creates the flows Фи and и. Both parts 5 to 6 of the measuring winding are located in planes parallel to the axis of the rotor, and the winding and connection of these two parts are made so that emf. from the useful flows, Phi and Phi add up, and from the external flow, the PVs are mutually balanced.

SU746143A 1961-09-29 1961-09-29 Device for measuring angular accelerations SU150166A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU746143A SU150166A1 (en) 1961-09-29 1961-09-29 Device for measuring angular accelerations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU746143A SU150166A1 (en) 1961-09-29 1961-09-29 Device for measuring angular accelerations

Publications (1)

Publication Number Publication Date
SU150166A1 true SU150166A1 (en) 1961-11-30

Family

ID=48305165

Family Applications (1)

Application Number Title Priority Date Filing Date
SU746143A SU150166A1 (en) 1961-09-29 1961-09-29 Device for measuring angular accelerations

Country Status (1)

Country Link
SU (1) SU150166A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4207769A (en) * 1978-07-24 1980-06-17 Hughes Aircraft Company Change of angular acceleration sensor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4207769A (en) * 1978-07-24 1980-06-17 Hughes Aircraft Company Change of angular acceleration sensor

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