Approach to High Performance Transonic Centrifugal Compressor

Oana, Mineyasu; Kawamoto, Osamu; Ohtani, Hideo; Yamamoto, Yuko

doi:10.2514/6.2002-3536

Cited by 9 publications

(6 citation statements)

References 2 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Therefore, adjusting and controlling the thickness distribution of the suction surface is the key point to improve the flow in the blade passage. Oana [8] studied the influence of the thickness distribution of rotary profile for the centrifugal compressor performance. The thickness distribution of pressure surface and suction surface has been given respectively.…”

Section: Impellermentioning

confidence: 99%

The Recent Progresses in Industrial Centrifugal Compressor Designs

Liang¹,

Yang²,

Xu³

et al. 2020

IJFMTS

View full text Add to dashboard Cite

The centrifugal compressor has been widely used in low power gas turbine, supercharger and industrial turbine compressors. Due to its outstanding advantages of simple process, compact structure and wide working range, it is more advantageous in some aspects such as small flow range than counterparts. However, the design of important components of centrifugal compressor requires lots of design experience and consideration. Because of the deepening research of the industrial centrifugal compressor, some excellent design optimization methods and experiences are obtained from researchers. In order to enable designers to get the preliminary design parameters and to develop a compressor with better performance better and faster, this paper addresses the main design optimization methods and design experiences of the components of the industrial centrifugal compressor. The detailed design considerations and design process for centrifugal compressor can reduce the design cycle time without scarifying performance for the new design. The purpose of this paper is to provide some design considerations and experiences of the centrifugal compressor for researchers. According to the centrifugal compressor design optimization process, purposed considerations in this paper are useful for compressor preliminary parameters selections. The optimizations and design considerations in this paper provide a detailed reference document for future centrifugal compressor developments.

show abstract

Section: Impellermentioning

confidence: 99%

The Recent Progresses in Industrial Centrifugal Compressor Designs

Liang¹,

Yang²,

Xu³

et al. 2020

IJFMTS

View full text Add to dashboard Cite

show abstract

“…The results showed that the size and location of the splitter blades were influenced on the overall performance of the centrifugal impeller. Oana et al [4] suggested that splitter incidence angle affects positively the overall efficiency of an impeller.…”

Section: Introductionmentioning

confidence: 99%

Effects of stator splitter blades on aerodynamic performance of a single-stage transonic axial compressor

Quang¹,

Le²,

Dinh³

2020

JMES

View full text Add to dashboard Cite

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations using the k-e turbulence model with a scalable wall function. The numerical results for the typical performance parameters without stator splitter blades were validated in comparison with experimental data. The numerical results of a parametric study using four geometric parameters (chord length, coverage angle, height and position) of the stator splitter blades showed that the operational stability of the single-stage axial compressor enhances remarkably using the stator splitter blades. The splitters were effective in suppressing flow separation in the stator domain of the compressor at near-stall condition which affects considerably the aerodynamic performance of the compressor.

show abstract

“…He achieved enhanced blade loading distribution and efficiency. By changing blade thickness and shape, Ona et al [19] retrofitted the compressor and succeeded in reducing rapid fluid flow acceleration/deceleration at leading edge and separation phenomena at hub.…”

Section: Introductionmentioning

confidence: 99%

Centrifugal Compressor Performance Improvement through Multi Splitter Impeller

Malik

Zheng

Qureshi

et al. 2019

Polish Maritime Research

View full text Add to dashboard Cite

In the paper, a back swept impeller of centrifugal compressor is experimentally studied and numerically validated and modified to increase its pressure ratio and improve efficiency, as well as to analyse the effect of splitter blade location between two main blades. The back swept multi splitter blade impeller was designed with a big splitter positioned close to the main blade suction surface and a smaller splitter close to the pressure surface. Adding this multi splitter improves the overall performance of the modified impeller due to less intensive flow separation and smaller pressure loss. In particular, the total pressure ratio was observed to increase from 4.1 to 4.4, with one percent increase in efficiency.

show abstract

Approach to High Performance Transonic Centrifugal Compressor

Cited by 9 publications

References 2 publications

The Recent Progresses in Industrial Centrifugal Compressor Designs

The Recent Progresses in Industrial Centrifugal Compressor Designs

Effects of stator splitter blades on aerodynamic performance of a single-stage transonic axial compressor

Centrifugal Compressor Performance Improvement through Multi Splitter Impeller

Contact Info

Product

Resources

About