KR19990070985A - Turbo compressor - Google Patents

Abstract

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a turbocompressor, which has a disadvantage in that a volumetric compressor that compresses gas by reducing a conventional volume has a disadvantage in that the compression performance and the efficiency of compressing the gas are low, while the gas is compressed by using a conventional impeller. Turbo compressor has a disadvantage that it is not suitable when applied to household appliances, such as large size. The present invention reduces the size of the impeller that compresses the gas to not only make it possible to miniaturize, but also to install the three impellers in consideration of the losses generated by the high-speed rotation of the drive motor to obtain the required compression ratio due to the miniaturization of the impeller, By maintaining the center of gravity of the rotating drive shaft by receiving the driving force of the driving motor, the required compression ratio is achieved, while reducing the high speed rotation of the driving motor and smoothing the rotation of the driving shaft, thereby maintaining the necessary compression ratio. The efficiency can be increased by reducing the loss due to the high speed rotation of the drive motor, and the structure can be simplified as well as easy to handle when the product is applied due to the miniaturization of the overall size.

Description

Turbo compressor

The present invention relates to a turbo compressor, and in particular, to provide a turbo compressor that is compact and easy to manufacture and high efficiency.

Generally, a compressor is a machine that compresses gas such as air or refrigerant gas. The compressor is composed of a power generating unit for generating power and a compression mechanism unit for sucking and compressing gas by a driving force transmitted from the power generating unit. The compressor is divided into a hermetic compressor having a power generating portion and a compression mechanism portion installed together in a hermetically sealed container having a predetermined internal volume, and a compressor having a separation form in which the power generating portion and the compression mechanism portion are separated.

The hermetic compressor includes a rotary compressor (also called a rotary compressor), a reciprocating compressor, and a scroll compressor due to a structure for compressing gas. Such a compressor is a volumetric compression in which the way of compressing the gas reduces its volume. In the volumetric compressor, the rotary compressor is configured to pressurize the gas by reducing the volume of the inner space while the eccentric shaft rotates inside the cylinder in which the cylindrical space is formed, and the reciprocating compressor has a reciprocating piston in the cylinder. While pressurizing the gas by reducing the volume of the interior space, the scroll compressor is the upper and lower scrolls formed with the involute curve wrap inside the rotation by engaging with each other while reducing the volume of the gas by Pressurizing structure.

The rotary compressor and the reciprocating compressor not only generate periodic vibration noise in the process of periodically pressurizing the gas, but also have low efficiency and low manufacturing cost. On the other hand, while the scroll compressor generates a low vibration noise and high efficiency in the process of continuously pressurizing the gas, not only the number of parts used but also the high manufacturing cost. In addition, the scroll compressor has a relatively high volume by using a high-pressure refrigerant in a volumetric manner, and the weight of parts is relatively heavy, so that when applied to a home appliance such as a refrigerator or an air conditioner, the scale of the applied home appliance is not only large but also a weight. The heavy weight makes handling difficult.

Complementing this drawback, a turbo compressor has been developed that is compact, high compression efficiency and simple structure.

SUMMARY OF THE INVENTION An object of the present invention is to provide a turbo compressor having a compact design, easy to manufacture, and excellent in compression performance and high efficiency in compressing gas.

1 is a cross-sectional view showing a turbo compressor of the present invention;

2 is a cross-sectional view showing a drive shaft and a component coupled thereto of the turbo compressor.

(Explanation of symbols for the main parts of the drawing)

One ; Inducer section 2; Impeller room

3; Vane diffuser portion 4; Volute part

100; Airtight container 110; First compression chamber

120; Second compression chamber 130; 3rd compression chamber

131; Discharge port 140; Motor room

141; Inlet 150; First gas channel

160; Second gas flow path 170; 3rd gas flow path

200; Drive motor 300; driving axle

310; First impeller 320; 2nd impeller

330; Third impeller 340; Radial bearing

350; Thrust bearing

In order to achieve the object of the present invention as described above, a first compression chamber, a second compression chamber, and a third compression chamber having discharge ports are respectively formed at both sides, and a motor chamber having a suction port is formed at the center thereof. A first gas flow path is formed to communicate the compression chamber, and a second gas flow path is formed to guide the first compressed refrigerant gas from the first compression chamber to the second compression chamber, and the second compression flow is performed in the second compression chamber. A hermetically sealed container including a third gas passage formed to guide the refrigerant gas to the third compression chamber, a driving motor mounted to the motor chamber to generate a driving force, and one end of the first compression chamber and the second compression chamber. The other end is inserted into the third compression chamber is inserted into the drive shaft coupled to the drive motor for transmitting the driving force of the motor, and coupled to the end of the drive shaft to be rotatable in the first compression chamber A first impeller for allowing the gas introduced into the inlet to cool the motor chamber and first compressing the gas flowing through the first gas passage to flow through the second gas passage to the second compression chamber, and rotatable in the second compression chamber; A second impeller coupled to the drive shaft to be primarily compressed to flow the gas introduced into the second compression chamber into the third compression chamber through the third gas flow path, and to be rotatable in the third compression chamber. A third impeller coupled to the other end and thirdly compressing the refrigerant gas introduced into the third compression chamber and discharging the refrigerant gas to the discharge port, and radial bearings installed on both sides of the drive motor to support the drive shaft in a radial direction; Turbo compressor is characterized in that it comprises a thrust bearing coupled to the drive shaft so as to be located on the side coupled to the third impeller supporting the drive shaft in the axial direction. Ball.

The first compression chamber, the second compression chamber and the third compression chamber may include an inducer unit for inducing the introduction of refrigerant gas, an impeller chamber communicating with the inducer unit and increasing the kinetic energy of the gas into which the impeller is inserted, and the impeller Provided is a turbo compressor comprising a vane diffuser portion and a volute portion communicating a seal with a gas flow path and converting an increased kinetic energy of the gas into a static pressure.

The impeller chamber into which the first impeller, the second impeller and the third impeller are respectively inserted is formed in an inverted cone shape in which the inner diameter into which the gas is introduced is smaller than the outer diameter through which the gas is compressed, and each impeller rotating in the impeller chamber. The turbo compressor is provided in the form of an inverted cone whose outer diameter is larger than the inner diameter corresponding to the impeller chamber.

Hereinafter, the turbo compressor of the present invention will be described according to an embodiment shown in the accompanying drawings.

In the turbo compressor of the present invention, as shown in FIG. 1, a third compression chamber 130 having a first compression chamber 110, a second compression chamber 120, and a discharge port 131 is formed on both sides, respectively. A motor chamber 140 having a suction port 141 is formed in the center thereof, and a first gas passage 150 is formed to communicate the motor chamber 140 with the first compression chamber 110. A second gas flow path 160 for guiding the first compressed refrigerant gas at 110 is introduced into the second compression chamber 120, and a second compressed refrigerant gas is removed from the second compression chamber 120. An airtight container 100 including a third gas flow path 170 formed to guide the three compression chambers 130, a driving motor 200 mounted on the motor chamber 140 to generate a driving force, and one end portion. Is inserted into the first compression chamber (110) and the second compression chamber (120), and the other end is inserted into the third compression chamber (130) and coupled to the drive motor (200) to form a sphere of the drive motor (200). Drive shaft 300 for transmitting the force, and the gas is coupled to the end of the drive shaft 300 to be rotatable in the first compression chamber 110, the gas introduced into the inlet 141 to cool the motor chamber 140 and the first A first impeller 310 which first compresses the gas introduced through the gas flow path 150 and flows through the second gas flow path 160 to the first compression chamber 120, and the second compression chamber 120. Coupled to the drive shaft 300 so as to be rotatable in the first compression to the second gas is introduced into the second compression chamber 120 is second compressed to flow through the third gas passage 170 to the third compression chamber (130) It is coupled to the other impeller 320 and the other end of the drive shaft 300 so as to be rotatable in the third compression chamber 130, the refrigerant gas introduced into the third compression chamber 130 by the third compression outlet 131 It is configured to include a third impeller 330 to discharge to. A radial bearing 340 is installed inside the motor chamber 140 so as to be located at both sides of the driving motor 200 to support the driving shaft 300 in the radial direction, and the third impeller 330 is coupled thereto. The thrust bearing 350 is coupled to the drive shaft 300 so as to be positioned at the side of the drive shaft 300 to support the drive shaft 300 in the axial direction.

The motor chamber 140 formed in the hermetically sealed container 100 is formed in a cylindrical shape, and an inlet port 141 is formed at one side of the motor chamber 140, and the first gas flow path is opposite to the inlet port 141. Outflow hole 142 in communication with 150 is formed. The first compression chamber 110 is formed at one side of the motor chamber 140, and the second compression chamber 120 is formed at the side of the first compression chamber 110, and the first and second compression chambers 110 and 120 are formed. ) Is formed through the shaft insertion hole so that the drive shaft 300 can be inserted. The third compression chamber 130 is formed on the opposite side where the first and second compression chambers 110 and 120 are formed. A thrust bearing 350 is installed between the motor chamber 140 and the third compression chamber 130. As an example of the thrust bearing 350, a support space 351 forming a support surface is formed on one side wall constituting the motor chamber 140, and a support plate 352 having a predetermined area inserted into the support space 351. ) Is fixedly coupled to the drive shaft (300).

The first compression chamber 110, the second compression chamber 120, and the third compression chamber 130 communicate with the inducer unit 1, which induces the introduction of the refrigerant gas, and the inductor unit 1. Is inserted into the impeller chamber (2) to increase the kinetic energy of the suction, and the vane diffuser (Vane diffuser) for communicating the impeller chamber (2) and the gas flow path and converts the increased kinetic energy of the gas into a static pressure It consists of a part 3 and a volute part 4.

The impeller chamber 2 into which the first impeller 310, the second impeller 320, and the third impeller 330 are inserted, respectively, has an inverse cone whose inner diameter into which gas is introduced is smaller than the outer diameter through which gas is compressed. Each impeller rotating in the impeller chamber 2 is formed in the shape of an inverted cone whose outer diameter is larger than the inner diameter corresponding to the impeller chamber 2.

The first gas passage 150 is formed outside the motor chamber 140 and communicates with the outlet hole 142 of the motor chamber 140 and the inducer portion of the first compression chamber 110. The second gas passage 160 is formed to communicate with the volute portion of the first compression chamber 110 and the inducer portion of the second compression chamber 120, and the third gas passage 170 has a second compression. It is formed over the side of the motor chamber 140 to communicate with the volute of the chamber 120 and the inducer of the third compression chamber (130).

The drive motor 200 is a stator part composed of several fixed disks 210 coupled to the inside of the motor chamber 140 and several rotations which are alternately positioned on the fixed disks 210 and coupled to the drive shaft 300. It is composed of a rotor portion consisting of a disk (220).

The radial bearing 340 is installed in the motor chamber 140 to be located at both sides of the drive motor 200.

As shown in FIG. 2, a portion of the third impeller 330 and the thrust bearing 350 coupled to one side of the driving shaft 300 and the first impeller 310 coupled to the other side of the driving shaft 300 are illustrated. It is preferable that the weight balance between the portion and the second impeller 320 is coupled so that the center of gravity of the entire driving shaft 300 is located at the center of the driving shaft 300. In addition, as an example of the radial bearing 340 supporting the drive shaft 300 in the radial direction, a bush 341 having a predetermined width inserted into the drive shaft 300 and a support member 342 supporting the bush 341 are provided. It is configured to include, the specifications of the radial bearing 340 is preferably designed to the same size with each other.

Hereinafter, the operational effects of the turbo compressor of the present invention will be described.

In the turbo compressor of the present invention, when a current is applied to the driving motor 200, the driving motor 200 is operated, and the driving force of the driving motor 200 is transmitted to the driving shaft 300 so that the driving shaft 300 rotates. The first impeller 310, the second impeller 320, and the third impeller 330 coupled to both ends of the drive shaft 300 are rotated by the rotation of the drive shaft 300. Coolant gas in a low temperature low pressure state passing through an evaporator (not shown) is introduced into the motor chamber 140 through the suction port 141 by the rotational force of each impeller to cool the driving motor 200, and then It is introduced into the first gas passage 150 through the outlet hole 142 formed on one side. The refrigerant gas introduced into the first gas passage 150 is first compressed into the first compression chamber 110 and then compressed into the second compression chamber 120 through the second gas passage 160. The first compressed refrigerant gas introduced into the second compression chamber 120 is second compressed in the second compression chamber 120, and then flows into the third compression chamber 130 through the third gas passage 170, and the first compression refrigerant gas flows into the third compression chamber 130. The refrigerant gas introduced into the three compression chambers 130 is discharged through the discharge port 131 at a high pressure. The discharged high pressure refrigerant gas flows into a condenser (not shown).

The first and second compression chambers 110 and 120 compressing the refrigerant gas 1 and 2 as the first and second impellers 310 and 320 rotate, and the third and third compressors of the refrigerant gas as the third impeller 330 rotates. The axial force acting on the drive shaft 300 by the pressure difference of the three compression chambers 130 is supported by the thrust bearing 350, and is also driven by the weight of the components coupled thereto and the weight of the drive shaft 300. The load acting in the radial direction 300 is supported by the radial bearing 340 so that the drive shaft 300 is rotated in a stable state.

The present invention is equipped with three impeller to compress the refrigerant gas is excellent in compression performance, can be reduced in size by reducing the diameter of the impeller, the drive motor to obtain the required compression ratio when the size is reduced It is possible to reduce the high-speed rotation of the drive motor 200 by reducing the high speed rotation by reducing the high speed rotation of the drive motor 200 without rotating the high speed as well as to easily design the drive motor 200. do.

In addition, the present invention is not only easy to design the radial bearing 340 by positioning the center of gravity of the drive shaft 300 in the middle of the drive shaft 300, but also smoothly rotation of the drive shaft 300 to increase the compression performance. .

As described above, the turbo compressor according to the present invention can not only simplify the structure when the product is applied due to the miniaturization, but also facilitate the handling thereof, and the driving motor for maintaining the required compression ratio by installing three impellers By reducing the high speed rotation of the drive motor has the effect of increasing the efficiency by reducing the loss caused by the high speed rotation.

Claims (3)

A first compression chamber, a second compression chamber and a third compression chamber having discharge ports are formed at both sides, and a motor chamber having a suction port is formed at the center thereof, and a first gas flow path is formed so as to communicate the motor chamber with the first compression chamber. And a second gas passage configured to guide the first compressed refrigerant gas from the first compression chamber to the second compression chamber, and to guide the second compressed refrigerant gas from the second compression chamber to the third compression chamber. An airtight container including three gas passages, a driving motor mounted to the motor chamber to generate a driving force, one end is inserted into the first compression chamber and the second compression chamber, and the other end is inserted into the third compression chamber. A drive shaft inserted into and coupled to the drive motor to transmit a driving force of the drive motor, and a gas introduced to the end of the drive shaft so as to be rotatable in the first compression chamber and introduced into the suction port to cool the motor chamber, and A first impeller which first compresses the gas introduced through the gas flow path and flows it through the second gas flow path to the second compression chamber, and is coupled to the driving shaft to be rotatable in the second compression chamber to be first compressed and then second compressed. A second impeller which secondly compresses the gas introduced into the chamber to flow through the third gas passage to the third compression chamber, and a refrigerant gas which is coupled to the other end of the drive shaft to be rotatable in the third compression chamber and flows into the third compression chamber; The third impeller for the third compression to discharge to the discharge port, the radial bearing which is installed on both sides of the drive motor to support the drive shaft in the radial direction, and the drive shaft to be located on the side where the third impeller is coupled Turbo compressor characterized in that it comprises a thrust bearing coupled to support the drive shaft in the axial direction. The method of claim 1, wherein the first compression chamber, the second compression chamber and the third compression chamber, the inducer portion for inducing the introduction of the refrigerant gas, the inductor portion is in communication with the injector to increase the kinetic energy of the gas is sucked into The main compressor is characterized in that the impeller chamber, the vane diffuser and the volute unit for communicating the impeller chamber and the gas flow path and converts the increased kinetic energy of the gas into a constant pressure. The impeller chamber according to claim 1 or 2, wherein the impeller chamber into which the first impeller, the second impeller, and the third impeller are inserted is formed in an inverted cone shape such that an inner diameter into which gas is introduced is smaller than an outer diameter from which gas is compressed. And each impeller rotating in the impeller chamber is formed in the form of an inverted cone whose outer diameter is larger than the inner diameter corresponding to the impeller chamber.