SU1663504A1 - Method of testing materials for wear resistance - Google Patents

Method of testing materials for wear resistance Download PDF

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Publication number
SU1663504A1
SU1663504A1 SU884454765A SU4454765A SU1663504A1 SU 1663504 A1 SU1663504 A1 SU 1663504A1 SU 884454765 A SU884454765 A SU 884454765A SU 4454765 A SU4454765 A SU 4454765A SU 1663504 A1 SU1663504 A1 SU 1663504A1
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SU
USSR - Soviet Union
Prior art keywords
sample
wear
wear resistance
testing materials
conditions
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Application number
SU884454765A
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Russian (ru)
Inventor
Леонид Адамович Сосновский
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Белорусский Институт Инженеров Железнодорожного Транспорта
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Priority to SU884454765A priority Critical patent/SU1663504A1/en
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Publication of SU1663504A1 publication Critical patent/SU1663504A1/en

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Abstract

Изобретение относитс  к испытани м и оценке работоспособности, например, деталей летательных аппаратов, винтов и т. п. Цель изобретени  - приближение условий испытани  к реальным услови м изнашивани  деталей летательных аппаратов. Способ реализуетс  следующим образом. Вращают образец, прикладывают к нему изгибающий момент и одновременно изнашивают потоком газовой среды, который подают либо попутно, либо навстречу движению изнашиваемой поверхности. 2 ил.The invention relates to testing and evaluating the performance of, for example, aircraft parts, propellers, etc. The purpose of the invention is to approximate test conditions to actual wear conditions of aircraft parts. The method is implemented as follows. A sample is rotated, a bending moment is applied to it, and at the same time it is worn by a stream of gaseous medium, which is supplied either along the way or towards the movement of the wear surface. 2 Il.

Description

Фиг.11

Изобретение относитс  к испытани м и . оценке работоспособности, например деталей летательных аппаратов, винтов и т.п.The invention relates to tests and. performance assessment, such as parts of aircraft, screws, etc.

Цель изобретени  - приближение условий испытаний к реальным услови м изнашивани  деталей летательных аппаратов.The purpose of the invention is to bring the test conditions closer to actual wear conditions of aircraft parts.

На фиг. 1 показана принципиальна  схема взаимодействи  потока газовой среды с образцом; на фиг. 2 - сечение А-А на фиг. 1.FIG. 1 shows a schematic diagram of the interaction of the flow of a gaseous medium with a sample; in fig. 2 is a section A-A in FIG. one.

Устройство дл  реализации способа содержит приспособление (не показано) дл  подачи потока 1 газовой среды, длинномерный образец 2, установленный с возможностью вращени  в опорах 3, приспособление (не показано) дл  приложени  изгибающего момента за счет силы Q.A device for implementing the method comprises a device (not shown) for supplying a stream of 1 gaseous medium, a long sample 2 mounted rotatably in the supports 3, a device (not shown) for applying a bending moment due to the force Q.

Способ реализуетс  следующим образом .The method is implemented as follows.

Вращают длинномерный образец 2, прикладывают к нему изгибающий момент и одновременно изнашивают потоком газовой среды с абразивными и/или жидкими частицами, которые подают либо попутно, либо навстречу движению изнашиваемой поверхности по касательной к ней.Rotate the lengthy sample 2, apply a bending moment to it and at the same time wear it with a stream of gaseous medium with abrasive and / or liquid particles, which are served either along the way or against the movement of the wearing surface tangentially to it.

Пример. Изнашивали образец 2 диаметром 20, изнашиваема  поверхность была выполнена вогнутой (радиус кривиз0Example. Sample 2 with a diameter of 20 was worn, the wear surface was made concave (radius of curvature

ны R 40). При вращении образца 2 возникал циклически измен ющийс  момент (частота 100 Гц), а на поверхности образца напр жени  достигали 200-400 МПа. Одновременно на образец 2 подавали воздух, содержащий частицы пыли. Услови  подачи потока 1 по первому варианту навстречу (поток 2 или 2) движению поверхности образца 2, а по второму варианту попутно (поток 2) движению поверхности образца 2.R 40). When sample 2 was rotated, a cyclically varying moment (frequency of 100 Hz) appeared, and the voltage on the sample surface reached 200-400 MPa. At the same time, air containing dust particles was supplied to sample 2. The flow conditions of flow 1 in the first embodiment meet (flow 2 or 2) to the movement of the surface of sample 2, and according to the second option in passing (flow 2) to the movement of the surface of the sample 2.

Claims (1)

Формула изобретени Invention Formula Способ испытани  материалов на изнашивание , заключающийс  в том, что вращают длинномерный образец, прикладывают к нему изгибающий момент и одновременно изнашивают его поверхность и определ ют износостойкость образца, отличающийс  тем, что, с целью приближени  условий испытани  к реальным услови м изнашивани  деталей летательных аппаратов , изнашивание осуществл ют потоком газовой среды с абразивными и/или жидкими частицами, который направл ют либо навстречу, либо попутно движению изнашиваемой поверхности образца по касательной к ней.The method of testing materials for wear, which consists in rotating a long sample, applying a bending moment to it and simultaneously wearing its surface and determining the wear resistance of the sample, characterized in that, in order to bring the test conditions to the actual wear conditions of aircraft parts, wear is carried out by the flow of a gaseous medium with abrasive and / or liquid particles, which is directed either towards or in parallel with the movement of the wearing surface of the specimen along a tangent it. Фиг. 2FIG. 2 А-А - УвеличеноA-A - Increased ШЪSh /&/ &
SU884454765A 1988-07-04 1988-07-04 Method of testing materials for wear resistance SU1663504A1 (en)

Priority Applications (1)

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SU884454765A SU1663504A1 (en) 1988-07-04 1988-07-04 Method of testing materials for wear resistance

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Application Number Priority Date Filing Date Title
SU884454765A SU1663504A1 (en) 1988-07-04 1988-07-04 Method of testing materials for wear resistance

Publications (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6230544B1 (en) * 1998-04-08 2001-05-15 Maocho Co., Ltd. Frictional wear testing apparatus and frictional wear testing method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Авторское свидетельство СССР № 1341538. кл. G 01 N 3/56, 1977. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6230544B1 (en) * 1998-04-08 2001-05-15 Maocho Co., Ltd. Frictional wear testing apparatus and frictional wear testing method

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