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Multistage compressor unit and method for regulating such multistage compressor unit
   
Document Number
US Patent 6802696
Issued Date
October 12, 2004
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Abstract
The invention relates to a multistage compressor unit which comprises at least two different compressor elements (1 and 2) driven by means of separate electric motors (3, 4) with an adjustable speed, whereby the outlet (8) of a compressor element (1) of one stage connected to the inlet (10) of a successive compressor element (2) of a successive stage, characterized in that the electric motors (2, 4) are identical and therefore have approximately one and the same nominal capacity, whereas between each motor (3, 4) and the compressor element (1, 2) driven thereby, a gear transmission (13, 14) is provided.
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Multistage compressor unit and method for regulating such multistage compressor unit - US Patent 6802696 Drawing
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Number of Claims:
16
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Published
October 12, 2004
Application Number
10/110,770
Filed
August 13, 2002
US Classification
417/2  
Int'l Classification
F04C   23/00   (20060101)  
Examiner
Attorney/Law Firm
Priority Data
Oct 26, 1999 [BE] 09900699
USPTO Field of Search
417/2   417/243   417/426  
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7044716 - High-pressure multi-stage centrifugal compressor - Owned by Atlas Copco Airpower, naamloze vennootschap (BE)

A high-pressure multi-stage centrifugal compressor is provided containing at least three compressor elements which are arranged in series as compressor stages, and at least two electric motors to drive these compressor elements. At least one compressor element forms a low-pressure stage which is driven by an electric motor. At least two compressor elements form high-pressure stages, and are arranged in series and driven by one and the same second electric motor.

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Description
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