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Turbo chiller, compressor therefor, and control method therefor
   
Document Number
US Patent 7412841
Issued Date
August 19, 2008
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Abstract
A compressor for a turbo chiller that can stably and efficiently operate in various operating states is provided. An aerodynamic feature map showing a rotating stall line at which rotating stall occurs is provided on a map represented by a flow parameter reflecting the volume flow based on the output thermal capacity of the chiller and by a pressure parameter reflecting the head based on the evaporator pressure and the condenser pressure. A minimum rotation speed obtaining unit obtains a minimum rotation speed from the pressure parameter and the rotating stall line on the aerodynamic feature map in the current operating state, and a rotation speed greater than or equal to the minimum rotation speed thus obtained is designated to the inverter.
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Number of Claims:
4
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Published
August 19, 2008
Application Number
11/010,385
Filed
December 14, 2004
US Classification
62/228.3   417/22 417/42 62/201 62/209
Int'l Classification
F25B   49/00   (20060101)  
Examiner
Assistant Examiner
Priority Data
Dec 18, 2003 [JP] 2003-420567
USPTO Field of Search
62/125   62/215   62/228.4   62/176.3   62/226   62/491   62/296   62/222  
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