Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel
The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentall...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Liang, Yangyang [verfasserIn] Gao, Zhengming [verfasserIn] Shi, Dai'en [verfasserIn] Li, Haotian [verfasserIn] Bao, Yuyun [verfasserIn] Cai, Ziqi [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2018 |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Chinese journal of chemical engineering - [S.l.] : Elsevier Science, 1993, 27, Seite 781-793 |
|---|---|
| Übergeordnetes Werk: |
volume:27 ; pages:781-793 |
| DOI / URN: |
10.1016/j.cjche.2018.10.020 |
|---|
| Katalog-ID: |
ELV002314193 |
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| 245 | 1 | 0 | |a Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
| 264 | 1 | |c 2018 | |
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| 520 | |a The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. | ||
| 650 | 4 | |a Shaft bending moment | |
| 650 | 4 | |a Torque | |
| 650 | 4 | |a Disk turbines | |
| 650 | 4 | |a Gas–liquid flow | |
| 650 | 4 | |a Fluid structure interaction | |
| 700 | 1 | |a Gao, Zhengming |e verfasserin |4 aut | |
| 700 | 1 | |a Shi, Dai'en |e verfasserin |4 aut | |
| 700 | 1 | |a Li, Haotian |e verfasserin |4 aut | |
| 700 | 1 | |a Bao, Yuyun |e verfasserin |4 aut | |
| 700 | 1 | |a Cai, Ziqi |e verfasserin |4 aut | |
| 773 | 0 | 8 | |i Enthalten in |t Chinese journal of chemical engineering |d [S.l.] : Elsevier Science, 1993 |g 27, Seite 781-793 |h Online-Ressource |w (DE-627)271598441 |w (DE-600)1480835-3 |w (DE-576)284926248 |x 2210-321X |7 nnns |
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10.1016/j.cjche.2018.10.020 doi (DE-627)ELV002314193 (ELSEVIER)S1004-9541(18)30729-8 DE-627 ger DE-627 rda eng 660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Liang, Yangyang verfasserin aut Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel 2018 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction Gao, Zhengming verfasserin aut Shi, Dai'en verfasserin aut Li, Haotian verfasserin aut Bao, Yuyun verfasserin aut Cai, Ziqi verfasserin aut Enthalten in Chinese journal of chemical engineering [S.l.] : Elsevier Science, 1993 27, Seite 781-793 Online-Ressource (DE-627)271598441 (DE-600)1480835-3 (DE-576)284926248 2210-321X nnns volume:27 pages:781-793 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 58.10 Verfahrenstechnik: Allgemeines AR 27 781-793 |
| spelling |
10.1016/j.cjche.2018.10.020 doi (DE-627)ELV002314193 (ELSEVIER)S1004-9541(18)30729-8 DE-627 ger DE-627 rda eng 660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Liang, Yangyang verfasserin aut Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel 2018 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction Gao, Zhengming verfasserin aut Shi, Dai'en verfasserin aut Li, Haotian verfasserin aut Bao, Yuyun verfasserin aut Cai, Ziqi verfasserin aut Enthalten in Chinese journal of chemical engineering [S.l.] : Elsevier Science, 1993 27, Seite 781-793 Online-Ressource (DE-627)271598441 (DE-600)1480835-3 (DE-576)284926248 2210-321X nnns volume:27 pages:781-793 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 58.10 Verfahrenstechnik: Allgemeines AR 27 781-793 |
| allfields_unstemmed |
10.1016/j.cjche.2018.10.020 doi (DE-627)ELV002314193 (ELSEVIER)S1004-9541(18)30729-8 DE-627 ger DE-627 rda eng 660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Liang, Yangyang verfasserin aut Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel 2018 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction Gao, Zhengming verfasserin aut Shi, Dai'en verfasserin aut Li, Haotian verfasserin aut Bao, Yuyun verfasserin aut Cai, Ziqi verfasserin aut Enthalten in Chinese journal of chemical engineering [S.l.] : Elsevier Science, 1993 27, Seite 781-793 Online-Ressource (DE-627)271598441 (DE-600)1480835-3 (DE-576)284926248 2210-321X nnns volume:27 pages:781-793 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 58.10 Verfahrenstechnik: Allgemeines AR 27 781-793 |
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10.1016/j.cjche.2018.10.020 doi (DE-627)ELV002314193 (ELSEVIER)S1004-9541(18)30729-8 DE-627 ger DE-627 rda eng 660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Liang, Yangyang verfasserin aut Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel 2018 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction Gao, Zhengming verfasserin aut Shi, Dai'en verfasserin aut Li, Haotian verfasserin aut Bao, Yuyun verfasserin aut Cai, Ziqi verfasserin aut Enthalten in Chinese journal of chemical engineering [S.l.] : Elsevier Science, 1993 27, Seite 781-793 Online-Ressource (DE-627)271598441 (DE-600)1480835-3 (DE-576)284926248 2210-321X nnns volume:27 pages:781-793 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 58.10 Verfahrenstechnik: Allgemeines AR 27 781-793 |
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10.1016/j.cjche.2018.10.020 doi (DE-627)ELV002314193 (ELSEVIER)S1004-9541(18)30729-8 DE-627 ger DE-627 rda eng 660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Liang, Yangyang verfasserin aut Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel 2018 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction Gao, Zhengming verfasserin aut Shi, Dai'en verfasserin aut Li, Haotian verfasserin aut Bao, Yuyun verfasserin aut Cai, Ziqi verfasserin aut Enthalten in Chinese journal of chemical engineering [S.l.] : Elsevier Science, 1993 27, Seite 781-793 Online-Ressource (DE-627)271598441 (DE-600)1480835-3 (DE-576)284926248 2210-321X nnns volume:27 pages:781-793 GBV_USEFLAG_U SYSFLAG_U GBV_ELV FID-ASIEN SSG-OLC-PHA GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 58.10 Verfahrenstechnik: Allgemeines AR 27 781-793 |
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Enthalten in Chinese journal of chemical engineering 27, Seite 781-793 volume:27 pages:781-793 |
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Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction |
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Chinese journal of chemical engineering |
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Liang, Yangyang @@aut@@ Gao, Zhengming @@aut@@ Shi, Dai'en @@aut@@ Li, Haotian @@aut@@ Bao, Yuyun @@aut@@ Cai, Ziqi @@aut@@ |
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2018-01-01T00:00:00Z |
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Liang, Yangyang |
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Liang, Yangyang ddc 660 ssgn 6,25 fid ASIEN bkl 58.10 misc Shaft bending moment misc Torque misc Disk turbines misc Gas–liquid flow misc Fluid structure interaction Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
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660 DE-600 6,25 ssgn ASIEN DE-1a fid 58.10 bkl Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel Shaft bending moment Torque Disk turbines Gas–liquid flow Fluid structure interaction |
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Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
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Liang, Yangyang Gao, Zhengming Shi, Dai'en Li, Haotian Bao, Yuyun Cai, Ziqi |
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torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
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Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
| abstract |
The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. |
| abstractGer |
The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. |
| abstract_unstemmed |
The torque and bending moment acting on a flexible overhung shaft in a gas–liquid stirred vessel agitated by a Rushton turbine and three different curved-blade disk turbines (half circular blades disk turbine, half elliptical blades disk turbine, and parabolic blades disk turbine) were experimentally measured by a customized moment sensor. The results show that the amplitude distribution of torque can be fitted by a symmetric bimodal distribution for disk turbines, and generally the distribution is more dispersive as the blade curvature or the gas flow rate increases. The amplitude distribution of shaft bending moment can be fitted by an asymmetric Weibull distribution for disk turbines. The relative shaft bending moment manifests a “rising-falling-rising” trend over the gas flow number, which is a corporate contribution of the unstable gas–liquid flow around the impeller, the gas cavities behind the blades, and the direct impact of gas on the impeller. And the “falling” stage is greater and lasts wider over the gas flow number for Rushton turbine than for the curved-blade disk turbines. |
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Torque and bending moment acting on a flexible shaft agitated by disk turbines in a gas–liquid stirred vessel |
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| score |
7.402815 |