Skip Nav Destination
Design and Analysis of Centrifugal Compressors
ISBN:
9781119424093
No. of Pages:
408
Publisher:
ASME Press
Publication date:
2020
The fastest way to obtain a large operating range is with a good design, with a correct blade loading distribution providing a negative slope of the pressure rise curve. The outcome of different optimizations is illustrated in Figure 9.1 and shows that maximizing the operating range may be at the expense of a lower efficiency.
9.1
Active Surge Control
9.2Bypass Valves
9.3Increased Impeller Stability
9.4Enhanced Vaned Diffuser Stability
9.5Impeller–diffuser Matching
9.6Enhanced Vaneless Diffuser Stability
This content is only available via PDF.
You do not currently have access to this chapter.
Email alerts
Related Chapters
Evaluation of the Analytical Bottom-Up SIL Proof by Statistical Top-Down Methods (PSAM-0242)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)
Boundary Layer Analysis
Centrifugal Compressors: A Strategy for Aerodynamic Design and Analysis
Identifying the Models, OF, DV, Convergence Criteria, and Constraints
Engineering Optimization: Applications, Methods, and Analysis
LARGE STANDOFF MAGNETOMETRY TECHNOLOGY ADVANCES TO ASSESS PIPELINE INTEGRITY UNDER GEOHAZARD CONDITIONS AND APPROACHES TO UTILISATION OF IT
Pipeline Integrity Management Under Geohazard Conditions (PIMG)
Related Articles
Analysis and Validation of a Unified Slip Factor Model for Impellers at Design and Off-Design Conditions
J. Turbomach (October,2011)
Rotordynamic Force Coefficients of Pocket Damper Seals
J. Turbomach (October,2006)
Exploring the Effect of V-Shaped Cut at Blade Exit of a Double Volute Centrifugal Pump
J. Pressure Vessel Technol (April,2012)
