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Centrifugal compressors inducers

Klassen, H.A., Effect of Inducer Inlet and Diffuser Throat Areas on Performance of a Low-Pressure Ratio Sweptback Centrifugal Compressor, NASA TM X-3148, Lewis Research Center, January 1975. [Pg.273]

Centrifugal compressors can have problems at the inducer and blade tips. These parts of the blade can be excited by aerodynamic forces. Blade discs can have stresses at the rotor tips, which lead to cracks. To solve this problem, the offending part is removed and a scalloped disc results as seen in Figure 21-20. This type of disc experiences some efficiency loss (about 2 %). [Pg.772]

Equipment Protective System Shutdown Systems that are usually provided for the protection of centrifugal pumps, rotating and reciprocating gas compressors, gas expansion and combustion gas turbines (CGTs), electric motors, generators, and forced or induced draft air fans. [Pg.196]

See other pages where Centrifugal compressors inducers is mentioned: [Pg.926]    [Pg.2507]    [Pg.23]    [Pg.32]    [Pg.132]    [Pg.198]    [Pg.53]    [Pg.149]    [Pg.749]    [Pg.2262]    [Pg.1086]    [Pg.149]    [Pg.1089]    [Pg.930]    [Pg.2511]    [Pg.812]    [Pg.395]   


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Compressors centrifugal

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