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A turbo compressor has a plurality of stages of compression means, each including an impeller and a diffuser, arranged in tandem with the flow of a fluid, and is capable of compressing the fluid sequentially in a plurality of the compression means and supplying the fluid compressed in the compressio

A turbo compressor has a plurality of stages of compression means, each including an impeller and a diffuser, arranged in tandem with the flow of a fluid, and is capable of compressing the fluid sequentially in a plurality of the compression means and supplying the fluid compressed in the compression means in a final stage to a condenser. The diffuser of at least the compression means in the final stage is a vaneless diffuser which does not include diffuser vanes which reduce the turning speed of the fluid in the diffuser. As such, according to this turbo compressor, it is possible to reduce generation of noise resulting from the transmission of turbulence of the fluid to the condenser, which occurs as the refrigerant collides against the diffuser vane.

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1. A turbo compressor comprising: a plurality of compression modules including a final stage compression module positioned and configured to supply fluid compressed to a condenser and a non-final stage compression module positioned and configured to supply the fluid compressed to the final stage com

1. A turbo compressor comprising: a plurality of compression modules including a final stage compression module positioned and configured to supply fluid compressed to a condenser and a non-final stage compression module positioned and configured to supply the fluid compressed to the final stage compression module, each compression module including an impeller and a diffuser, arranged in tandem with a flow of the fluid, and configured to compress the fluid sequentially in the plurality of compression modules,wherein the diffuser of the non-final stage compression module is positioned and configured to supply no fluid directly to the condenser and comprises vanes including diffuser vanes positioned and configured to reduce a turning speed of the fluid in the diffuser, andthe diffuser of the final stage compression module is a vaneless diffuser no diffuser vanes reducing the turning speed of the fluid in the diffuser. 2. The turbo compressor according to claim 1, further comprising a second non-final stage compression module positioned and configured to compress the fluid received from the non-final stage compression module and to supply the fluid compressed directly to the final compression module, wherein the second non-final stage compression module includes an impeller, a vaneless diffuser and a bypass flow path and is positioned and configured to supply the fluid directly to the condenser through the bypass flow path. 3. A refrigerator comprising: a condenser configured to cool and to liquify a compressed refrigerant;an evaporator positioned and configured to evaporate the liquefied refrigerant and to deprive vaporization heat from an object to be cooled, thereby cooling the object to be cooled; anda compressor configured to compress the refrigerant evaporated in the evaporator and to supply the refrigerant to the condenser,wherein the compressor comprises the turbo compressor according to claim 2. 4. A refrigerator comprising: a condenser configured to cool and to liquify a compressed refrigerant;an evaporator positioned and configured to evaporate the liquefied refrigerant and to deprive vaporization heat from an object to be cooled, thereby cooling the object to be cooled; anda compressor configured to compress the refrigerant evaporated in the evaporator and to supply the refrigerant to the condenser,wherein the compressor comprises the turbo compressor according to claim 1. 5. A turbo refrigeration system comprising a turbo compressor according to claim 1. 6. A turbo compressor comprising: a plurality of compression modules including a final stage compression module positioned and configured to supply fluid compressed to a condenser and at least one non-final stage compression module positioned and configured to supply the fluid compressed to the final stage compression module and to supply no fluid directly to the condenser, each compression module including an impeller and a diffuser, arranged in tandem with a flow of the fluid, and configured to compress the fluid sequentially in the plurality of compression modules,wherein the diffuser of the final stage compression module is a vaneless diffuser including no diffuser vanes reducing the turning speed of the fluid in the diffuser;each module of the at least one non-final stage compression module comprising vanes including diffuser vanes positioned and configured to reduce a turning speed of the fluid in the diffuser; andan additional compression module position and configured to receive the fluid from the at least one non-final stage compression module and to supply the fluid directly to the final stage compression module and including a bypass flow path positioned and configured to supply the fluid directly to the condenser through the bypass flow path, and the additional compression module comprising a vaneless diffuser.