2011
DOI: 10.1007/s12206-011-0419-7
|View full text |Cite
|
Sign up to set email alerts
|

Experimental identification of fluid-induced force in labyrinth seals

Abstract: The seal force is an important factor in turbomachineries. Therefore, the current paper puts forward an expanded seal force identification model. A seal test rig consisting of several sets of seals was prepared. Using the double-plane unbalance force identification theory in rotordynamics, the distributed seal force in the cylinder became equivalent to two selected planes. Considering the complex cylinder vibration with increasing rotating speed and inlet pressure, the cylinder was regarded as a vibration syst… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

0
4
0

Year Published

2013
2013
2019
2019

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(4 citation statements)
references
References 21 publications
0
4
0
Order By: Relevance
“…The first model is based on Hirano's compressor eye seal [21]. The second model is based on our previous experimental labyrinth seal [22].…”
Section: Numerical Modelmentioning
confidence: 99%
“…The first model is based on Hirano's compressor eye seal [21]. The second model is based on our previous experimental labyrinth seal [22].…”
Section: Numerical Modelmentioning
confidence: 99%
“…This is designed in terms of the condition of our previous test rig. 26 Figure 4 shows the boundary conditions defined for the conventional LS and the RAS. The calculation assumes the fluid to be an ideal gas at constant temperature and the entire flow to be turbulent.…”
Section: Numerical Modelmentioning
confidence: 99%
“…To validate the simulation approach and solver settings, validation was carried out against our previous experimental work reported in the literature. 26 The test rig and seal dimensions are shown in Figure 6. There are, in total, six sets of seals in the rig.…”
Section: Validation Of Cfd Model Against the Published Literature Resmentioning
confidence: 99%
“…Given the uncertainty surrounding both the expected leakage and rotordynamic performance of the floating bushing seals, a number of other seal technologies were also explored for their viable use with the GEL bearing test rig. These seals included lip seals [122,123], labyrinth seals [124][125][126][127][128][129][130][131][132][133][134], a variety of annular seals including bushing, ring, honeycomb, and hole pattern seals [135][136][137][138][139][140][141][142][143][144][145][146], centrifugal motion seals [47,147,148], and mechanical seals [149][150][151][152][153][154][155][156][157][158][159][160][161][162][163]. However, these sealing technologies also faced a number of technical hurdles to being implemented in GEL environments including Hence, after considering the uncertainty surrounding the cu...…”
Section: Bearing Sealsmentioning
confidence: 99%