Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection.
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| Title: | Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection. |
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| Authors: | Sui, Xiuming1,2 (AUTHOR), Zhao, Wei1,2,3 (AUTHOR) zhaowei@iet.cn, Xiang, Xiaorong1,2 (AUTHOR), Pi, Te1,2 (AUTHOR), Zhao, Qingjun1,2,3 (AUTHOR) |
| Source: | Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.). Dec2021, Vol. 235 Issue 8, p1864-1876. 13p. |
| Subject Terms: | *Coolants, Turbine efficiency, Turbines, Shock waves, Unsteady flow, Aerodynamic load |
| Abstract: | The sealing of the rotor-rotor gap and rotor disk cooling are vital to the safe operation of the vaneless counter-rotating turbine(VCRT). In order to quantifies the influence of the wheel-space cavity flow on the VCRT aerodynamic performance, and to improve turbine efficiency of the VCRT at certain rim seal ejection rates, numerical studies which considered the effects of rotor-rotor rim seal flow ejection are carried out in this paper. The three dimensional unsteady computational fluid dynamic analysis of a VCRT at the engine conditions are performed, and the seal flow ejected downstream of the high pressure rotor row at six sealing flow rate are modeled. The interaction among the high pressure rotor trailing shock wave, the downstream secondary flow and the seal flow has been studied and quantitatively characterized as a function of the purge ejection rate. Numerical results show that seal flow- mainstream flow interaction is entirely dominated by the high pressure rotor trailing edge shock at the hub, low pressure hub passage vortex and the mixing of the sealing flow from wheelspace and mainstream. When the mass flow rate of the coolant is smaller than some threshold value, the shock loss of the high pressure rotor and hub secondary flow loss of the low pressure rotor are decreased with the increasing of the coolant mass flow rate. It causes that the VCRT efficiency is gradually increased. On condition that the amount of the seal flows is beyond the threshold value, the key roles in modification of the VCRT performance are changed. The increment of the hub secondary flow loss and the mixing loss are gradually larger than the decrement of the shock loss. As a result, the turbine efficiency gradually decreases. [ABSTRACT FROM AUTHOR] |
| Copyright of Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.) is the property of Sage Publications, Ltd. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | GreenFILE |
| FullText | Text: Availability: 0 |
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| Header | DbId: 8gh DbLabel: GreenFILE An: 153686762 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Sui%2C+Xiuming%22">Sui, Xiuming</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Zhao%2C+Wei%22">Zhao, Wei</searchLink><relatesTo>1,2,3</relatesTo> (AUTHOR)<i> zhaowei@iet.cn</i><br /><searchLink fieldCode="AR" term="%22Xiang%2C+Xiaorong%22">Xiang, Xiaorong</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Pi%2C+Te%22">Pi, Te</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Zhao%2C+Qingjun%22">Zhao, Qingjun</searchLink><relatesTo>1,2,3</relatesTo> (AUTHOR) – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Proceedings+of+the+Institution+of+Mechanical+Engineers%2C+Part+A%3A+Journal+of+Power+%26+Energy+%28Sage+Publications%2C+Ltd%2E%29%22">Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.)</searchLink>. Dec2021, Vol. 235 Issue 8, p1864-1876. 13p. – Name: Subject Label: Subject Terms Group: Su Data: *<searchLink fieldCode="DE" term="%22Coolants%22">Coolants</searchLink><br /><searchLink fieldCode="DE" term="%22Turbine+efficiency%22">Turbine efficiency</searchLink><br /><searchLink fieldCode="DE" term="%22Turbines%22">Turbines</searchLink><br /><searchLink fieldCode="DE" term="%22Shock+waves%22">Shock waves</searchLink><br /><searchLink fieldCode="DE" term="%22Unsteady+flow%22">Unsteady flow</searchLink><br /><searchLink fieldCode="DE" term="%22Aerodynamic+load%22">Aerodynamic load</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: The sealing of the rotor-rotor gap and rotor disk cooling are vital to the safe operation of the vaneless counter-rotating turbine(VCRT). In order to quantifies the influence of the wheel-space cavity flow on the VCRT aerodynamic performance, and to improve turbine efficiency of the VCRT at certain rim seal ejection rates, numerical studies which considered the effects of rotor-rotor rim seal flow ejection are carried out in this paper. The three dimensional unsteady computational fluid dynamic analysis of a VCRT at the engine conditions are performed, and the seal flow ejected downstream of the high pressure rotor row at six sealing flow rate are modeled. The interaction among the high pressure rotor trailing shock wave, the downstream secondary flow and the seal flow has been studied and quantitatively characterized as a function of the purge ejection rate. Numerical results show that seal flow- mainstream flow interaction is entirely dominated by the high pressure rotor trailing edge shock at the hub, low pressure hub passage vortex and the mixing of the sealing flow from wheelspace and mainstream. When the mass flow rate of the coolant is smaller than some threshold value, the shock loss of the high pressure rotor and hub secondary flow loss of the low pressure rotor are decreased with the increasing of the coolant mass flow rate. It causes that the VCRT efficiency is gradually increased. On condition that the amount of the seal flows is beyond the threshold value, the key roles in modification of the VCRT performance are changed. The increment of the hub secondary flow loss and the mixing loss are gradually larger than the decrement of the shock loss. As a result, the turbine efficiency gradually decreases. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.) is the property of Sage Publications, Ltd. and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
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| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1177/09576509211018307 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 13 StartPage: 1864 Subjects: – SubjectFull: Coolants Type: general – SubjectFull: Turbine efficiency Type: general – SubjectFull: Turbines Type: general – SubjectFull: Shock waves Type: general – SubjectFull: Unsteady flow Type: general – SubjectFull: Aerodynamic load Type: general Titles: – TitleFull: Investigation of the flowfield on a vaneless counter-rotating turbine with seal cavity flow ejection. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Sui, Xiuming – PersonEntity: Name: NameFull: Zhao, Wei – PersonEntity: Name: NameFull: Xiang, Xiaorong – PersonEntity: Name: NameFull: Pi, Te – PersonEntity: Name: NameFull: Zhao, Qingjun IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 12 Text: Dec2021 Type: published Y: 2021 Identifiers: – Type: issn-print Value: 09576509 Numbering: – Type: volume Value: 235 – Type: issue Value: 8 Titles: – TitleFull: Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power & Energy (Sage Publications, Ltd.) Type: main |
| ResultId | 1 |