Jason C. Wilkes, N. Smith, Karl D. Wygant, Abhay V. Patil, Chris D. Kulhanek
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In a recent test program for an sCO2 integrally geared compander (compressor/turbine), a balance piston was created on the opposite end of the turbine to provide an equalizing thrust; while this is not novel, the balance piston provided a test apparatus for measuring the leakage on a 20 tooth stepped labyrinth seal operating at pressures in excess of 250 bar (3600 psi).\n The stepped balance piston seal is a 20 tooth tooth-on-rotor balance piston seal. This type of seal was selected since it was predicted to have substantially less leakage than a comparably sized straight through labyrinth seal. Comparisons between the two designs will be made, showing that the leakage of the stepped balance piston seal is considerably lower. The tooth clearance on the seal was selected to be 30 mils radial. While this seems large, a stack-up tolerance assessment showed that this magnitude of clearance was appropriate to prevent rotor stator contact.\n During the testing campaign, data was recorded showing the leakage across this stepped balance piston seal at pressures in excess of 250 bar (3600 psi) with a pressure ratio of 2. This leakage data was measured, and will be compared to leakage data predicted with CFD. Two measurement methods are presented for the stepped balance piston seal: an orifice plate and valve.\n The predicted seal leakage from a straight through seal was four times that of the predicted stepped labyrinth seal. The measured flow from the stepped seal was on the same order as the CFD prediction and offered adequate rotordynamic performance.","PeriodicalId":105703,"journal":{"name":"Volume 9: Supercritical CO2","volume":"45 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-06-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Leakage Characteristics of a Stepped Balance Piston Labyrinth Seal in Supercritical CO2\",\"authors\":\"Jason C. Wilkes, N. Smith, Karl D. Wygant, Abhay V. Patil, Chris D. Kulhanek\",\"doi\":\"10.1115/gt2022-83262\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"\\n In an integrally geared compressor, there is a net thrust load on the pinion shaft from gear loads and aerodynamic forces. The net thrust on the pinion is resolved with either a thrust bearing or a thrust collar (rider ring). As the pressure increases, this increases the aerodynamic force proportionally. In high-pressure systems this can overwhelm the thrust bearing or thrust collar if thrust is mismanaged. In a recent test program for an sCO2 integrally geared compander (compressor/turbine), a balance piston was created on the opposite end of the turbine to provide an equalizing thrust; while this is not novel, the balance piston provided a test apparatus for measuring the leakage on a 20 tooth stepped labyrinth seal operating at pressures in excess of 250 bar (3600 psi).\\n The stepped balance piston seal is a 20 tooth tooth-on-rotor balance piston seal. This type of seal was selected since it was predicted to have substantially less leakage than a comparably sized straight through labyrinth seal. Comparisons between the two designs will be made, showing that the leakage of the stepped balance piston seal is considerably lower. The tooth clearance on the seal was selected to be 30 mils radial. While this seems large, a stack-up tolerance assessment showed that this magnitude of clearance was appropriate to prevent rotor stator contact.\\n During the testing campaign, data was recorded showing the leakage across this stepped balance piston seal at pressures in excess of 250 bar (3600 psi) with a pressure ratio of 2. This leakage data was measured, and will be compared to leakage data predicted with CFD. Two measurement methods are presented for the stepped balance piston seal: an orifice plate and valve.\\n The predicted seal leakage from a straight through seal was four times that of the predicted stepped labyrinth seal. 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引用次数: 0
摘要
在整体齿轮压缩机中,小齿轮轴上有来自齿轮负载和空气动力的净推力负载。小齿轮上的净推力通过推力轴承或推力环(骑环)来解决。随着压力的增加,空气动力也成比例地增加。在高压系统中,如果推力管理不当,这可能会压垮推力轴承或推力环。在最近的sCO2整体齿轮压缩机(压缩机/涡轮机)测试项目中,在涡轮机的另一端安装了一个平衡活塞,以提供平衡推力;虽然这并不新奇,但平衡活塞提供了一种测试装置,用于测量在超过250 bar (3600 psi)压力下工作的20齿阶梯迷宫密封上的泄漏。阶梯式平衡活塞密封是一个20齿齿转子平衡活塞密封。之所以选择这种类型的密封,是因为预计它比同等尺寸的直通式迷宫式密封具有更少的泄漏。将两种设计进行比较,表明阶梯式平衡活塞密封的泄漏要低得多。密封上的齿间隙选择为径向30密耳。虽然这看起来很大,但堆叠公差评估表明,这种大小的间隙是适当的,以防止转子定子接触。在测试过程中,记录的数据显示,在压力超过250 bar (3600 psi)、压力比为2的情况下,通过该阶梯平衡活塞密封的泄漏。该泄漏数据已被测量,并将与CFD预测的泄漏数据进行比较。介绍了两种测量阶梯平衡活塞密封的方法:孔板和阀。直通式密封的预测泄漏量是阶梯迷宫式密封的4倍。阶梯式密封的实测流量与CFD预测相同,且具有良好的转子动力学性能。
Leakage Characteristics of a Stepped Balance Piston Labyrinth Seal in Supercritical CO2
In an integrally geared compressor, there is a net thrust load on the pinion shaft from gear loads and aerodynamic forces. The net thrust on the pinion is resolved with either a thrust bearing or a thrust collar (rider ring). As the pressure increases, this increases the aerodynamic force proportionally. In high-pressure systems this can overwhelm the thrust bearing or thrust collar if thrust is mismanaged. In a recent test program for an sCO2 integrally geared compander (compressor/turbine), a balance piston was created on the opposite end of the turbine to provide an equalizing thrust; while this is not novel, the balance piston provided a test apparatus for measuring the leakage on a 20 tooth stepped labyrinth seal operating at pressures in excess of 250 bar (3600 psi).
The stepped balance piston seal is a 20 tooth tooth-on-rotor balance piston seal. This type of seal was selected since it was predicted to have substantially less leakage than a comparably sized straight through labyrinth seal. Comparisons between the two designs will be made, showing that the leakage of the stepped balance piston seal is considerably lower. The tooth clearance on the seal was selected to be 30 mils radial. While this seems large, a stack-up tolerance assessment showed that this magnitude of clearance was appropriate to prevent rotor stator contact.
During the testing campaign, data was recorded showing the leakage across this stepped balance piston seal at pressures in excess of 250 bar (3600 psi) with a pressure ratio of 2. This leakage data was measured, and will be compared to leakage data predicted with CFD. Two measurement methods are presented for the stepped balance piston seal: an orifice plate and valve.
The predicted seal leakage from a straight through seal was four times that of the predicted stepped labyrinth seal. The measured flow from the stepped seal was on the same order as the CFD prediction and offered adequate rotordynamic performance.