2021
DOI: 10.1007/s11630-021-1436-1
|View full text |Cite
|
Sign up to set email alerts
|

Using Tip Gaps on Tandem Diffuser to Broaden the Operation Range of a Centrifugal Compressor

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
1
1

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(2 citation statements)
references
References 9 publications
0
2
0
Order By: Relevance
“…Fang and Ji 131 found that with a 2.5% tip clearance ratio the compressor surge margin increased from 33.28% to 49.2%, the stability margin increased from 44% to 60.5%, the pressure ratio loss was 1.16%, and the efficiency loss was 1.14%. Li and Hu 132 found that an increase of 0.1 mm in the gap at the top of the leaf reduces the pressure ratio by about 3% and the efficiency by about 2%.…”
Section: Research Status Of Variable-altitude Turbocharging Systemsmentioning
confidence: 99%
“…Fang and Ji 131 found that with a 2.5% tip clearance ratio the compressor surge margin increased from 33.28% to 49.2%, the stability margin increased from 44% to 60.5%, the pressure ratio loss was 1.16%, and the efficiency loss was 1.14%. Li and Hu 132 found that an increase of 0.1 mm in the gap at the top of the leaf reduces the pressure ratio by about 3% and the efficiency by about 2%.…”
Section: Research Status Of Variable-altitude Turbocharging Systemsmentioning
confidence: 99%
“…However, due to manufacturability issues and assembly tolerances, it is known that the diffuser may have a clearance. This impacts the aerodynamic performance, even though industrial experience and literature show that small gaps can even be beneficial for the performance and stability of the diffuser [4]. Suppression of the suction side flow separation can be for example achieved using grove at low solidity blade leading tip [5].…”
Section: Introductionmentioning
confidence: 99%