Supersonic compressor comprising radial flow path

Active Publication Date: 2010-12-30
NUOVO PIGNONE TECH SRL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007]In yet another embodiment, the present invention provides a supersonic compressor comprising (a) a gas conduit comprising (i) a low pressure gas inlet, and (ii) a high pressure gas outlet; (b) a first supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp; (c) a second supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compress

Problems solved by technology

Conventional compressor systems, while exceedingly useful, are limited in that the pressure ratio achievable by a single stage of a compress

Method used

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  • Supersonic compressor comprising radial flow path
  • Supersonic compressor comprising radial flow path
  • Supersonic compressor comprising radial flow path

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Embodiment Construction

[0020]In the following specification and the claims, which follow, reference will be made to a number of terms, which shall be defined to have the following meanings.

[0021]The singular forms “a”, “an”, and “the” include plural referents unless the context clearly dictates otherwise.

[0022]“Optional” or “optionally” means that the subsequently described event or circumstance may or may not occur, and that the description includes instances where the event occurs and instances where it does not.

[0023]Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about” and “substantially”, are not to be limited to the precise value specified. In at least some instances, the approximating language may correspond to the precision of an instrument for measuri

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Abstract

The present invention provides novel supersonic compressors comprising novel supersonic compressor rotors. The supersonic compressor rotors are designed to operate at very high rotational speed wherein the velocity of the gas entering the supersonic compressor rotor is greater than the local speed of sound in the gas, hence the descriptor “supersonic”. The new supersonic compressors comprise at least one supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp. The novel supersonic compressor rotors are expected to enhance the performance of supersonic compressors comprising them, and to provide for greater design versatility in systems comprising such novel supersonic compressors.

Description

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Claims

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Application Information

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Owner NUOVO PIGNONE TECH SRL
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