Numerical computation of the main gas-dynamic bearing static characteristics for the ball gyroscope; MATEC Web of Conferences; Vol. 48 : Space Engineering
| Parent link: | MATEC Web of Conferences Vol. 48 : Space Engineering.— 2016.— [01003, 5 p.] |
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| Shrnutí: | Title screen The numerical computation questions and analysis of the engineering calculation of the main gas-dynamic bearing static characteristics for the ball gyroscope experimental model are considered. The developed gyroscopic device construction is provided. These investigations for evaluation of the possibility to realize a sensitive element, which base on the developed device were provided. It is supposed, that this sensitive element can be used in information measuring systems of various applications. The main calculation data, such as load-bearing capacity and other characteristics of the hemispherical gas-dynamic bearing is carried out. According to the attained results, preliminary implications are stated. The basic problems for the further research are determined. |
| Jazyk: | angličtina |
| Vydáno: |
2016
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| Edice: | Spacecrafts and Devices |
| Témata: | |
| On-line přístup: | http://dx.doi.org/10.1051/matecconf/20164801003 http://earchive.tpu.ru/handle/11683/33710 |
| Médium: | Elektronický zdroj Kapitola |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648902 |
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| 330 | |a The numerical computation questions and analysis of the engineering calculation of the main gas-dynamic bearing static characteristics for the ball gyroscope experimental model are considered. The developed gyroscopic device construction is provided. These investigations for evaluation of the possibility to realize a sensitive element, which base on the developed device were provided. It is supposed, that this sensitive element can be used in information measuring systems of various applications. The main calculation data, such as load-bearing capacity and other characteristics of the hemispherical gas-dynamic bearing is carried out. According to the attained results, preliminary implications are stated. The basic problems for the further research are determined. | ||
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| 463 | 0 | |0 (RuTPU)RU\TPU\network\13956 |t Vol. 48 : Space Engineering |o IV Russian Forum for Young Scientists with International Participation, April 12-14, 2016, Tomsk, Russia |o [proceedings] |f National Research Tomsk Polytechnic University (TPU) ; eds. V. N. Borikov [et al.] |v [01003, 5 p.] |d 2016 | |
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