<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>In aircraft construction, when creating samples of new equipment, shock tests are often performed, both on individual components and the entire product. It requires introducing non-destructive testing devices into production, it is one of the most important factors in accelerating scientific and technological progress, raising the quality and competitiveness of manufactured products. Applying modern means of non-destructive testing, there is the problem of their protection from external vibrations, which affect the sensitivity, accuracy and reliability of high-precision measurements. In such cases, the conversion of measuring information during powerful vibration and shock tests, as a rule, is carried out by piezoelectric acceleration sensors. Although to provide impact testing, there is a need to develop and use stand-alone recorders. The main requirements for these recorders are to ensure the autonomy and operability of the recorder onboard the test product and to ensure the synchronization of the registration of the shock load.</p>
</abstract>

In aircraft construction, when creating samples of new equipment, shock tests are often performed, both on individual components and the entire product. It requires introducing non-destructive testing devices into production, it is one of the most important factors in accelerating scientific and technological progress, raising the quality and competitiveness of manufactured products. Applying modern means of non-destructive testing, there is the problem of their protection from external vibrations, which affect the sensitivity, accuracy and reliability of high-precision measurements. In such cases, the conversion of measuring information during powerful vibration and shock tests, as a rule, is carried out by piezoelectric acceleration sensors. Although to provide impact testing, there is a need to develop and use stand-alone recorders. The main requirements for these recorders are to ensure the autonomy and operability of the recorder onboard the test product and to ensure the synchronization of the registration of the shock load.

Determination of Dynamic Range of Stand-alone Shock Recorders

Department of Computerized Electrical Systems and Technologies, Aerospace Faculty

Department of Automation and Non-Destructive Testing Systems, Faculty of Instrumentation Engineering

National Technical University of Ukraine “Igor Sikorsky Kyiv Polytechnic Institute”

Measurement Science Review

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

{"article-title":"Determination of Dynamic Range of Stand-alone Shock Recorders"}

In aircraft construction, when creating samples of new equipment, shock tests are often performed, both on individual components and the entire product. It...

Determination of Dynamic Range of Stand-alone Shock Recorders

Online veröffentlicht: 05. Aug. 2022

Seitenbereich: 208 - 213

Eingereicht: 03. Nov. 2021

Akzeptiert: 24. Mai 2022

DOI: https://doi.org/10.2478/msr-2022-0026

Schlüsselwörter
non-destructive testing, shock tests, measurements, sensitivity, accuracy, external vibrations

© 2022 Anzhelika Stakhova et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Determination of Dynamic Range of Stand-alone Shock Recorders

Online veröffentlicht: 05. Aug. 2022

Seitenbereich: 208 - 213

Eingereicht: 03. Nov. 2021

Akzeptiert: 24. Mai 2022

DOI: https://doi.org/10.2478/msr-2022-0026

Schlüsselwörternon-destructive testing, shock tests, measurements, sensitivity, accuracy, external vibrations

© 2022 Anzhelika Stakhova et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Schlüsselwörter
non-destructive testing, shock tests, measurements, sensitivity, accuracy, external vibrations