COMPRESSOR

• US 20200132077A1
• Filed: 06/27/2019
• Published: 04/30/2020
• Est. Priority Date: 10/25/2018
• Status: Abandoned Application

• Current Assignee: Hyundai Motor Company (Hyundai Motor Group), Kia Motors Corporation (Kia Corp.)
• Original Assignee: Hyundai Motor Company (Hyundai Motor Group)
• Inventors: Ha, Kyoung Ku, Lee, Chang Ha
• Application Number:
  US16/455,305
• Publication Number:
  US 20200132077A1
• Time in Patent Office: Days
• CPC Class Codes: F04D 17/10 for compressing or evacuating
• CPC Class Codes: F04D 17/122 the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
• CPC Class Codes: F04D 25/06 the pump being electrically driven F04D25/08 takes precedence
• CPC Class Codes: F04D 29/0513 hydrostatic; hydrodynamic thrust bearings
• CPC Class Codes: F04D 29/056 Bearings
• CPC Class Codes: F04D 29/057 hydrostatic; hydrodynamic
• CPC Class Codes: F04D 29/284 for compressors
• CPC Class Codes: F05D 2250/292 tapered
• CPC Class Codes: F16C 17/024 with flexible leaves to create hydrodynamic wedge, e.g. radial foil bearings
• CPC Class Codes: F16C 17/042 with flexible leaves to create hydrodynamic wedge, e.g. axial foil bearings
• CPC Class Codes: F16C 17/10 for both radial and axial load
• CPC Class Codes: F16C 2360/24 Turbochargers in general F02C6/12
• CPC Class Codes: F16C 2360/43 Screw compressors in general F04C
• CPC Class Codes: F16C 32/0603 supported by a gas cushion, e.g. an air cushion
• CPC Class Codes: F16C 32/0696 for both radial and axial load
• CPC Class Codes: Y02E 60/50 Fuel cells

Abstract

A compressor includes a shaft extending in axial directions thereof, an impeller secured to one end of the shaft, a first bearing action member provided at the one end of the shaft, a second bearing action member provided at an opposite end of the shaft that is opposite to the one end of the shaft, a first bearing that acts on the first bearing action member and supports the first bearing action member in one axial direction of the axial directions and in a radially inward direction of the shaft, and a second bearing that acts on the second bearing action member and supports the second bearing action member in another axial direction, which is opposite to the one axial direction, and in the radially inward direction of the shaft.

Claims

1. A compressor comprising:

a shaft extending in axial directions thereof;

an impeller secured to one end of the shaft;

a first bearing action member provided at the one end of the shaft;

a second bearing action member provided at an opposite end of the shaft that is opposite to the one end of the shaft;

a first bearing configured to act on the first bearing action member and support the first bearing action member in one axial direction of the axial directions and in a radially inward direction of the shaft; and

a second bearing configured to act on the second bearing action member and support the second bearing action member in another axial direction of the axial directions, which is opposite to the one axial direction, and in the radially inward direction of the shaft.

2. The compressor of claim 1, wherein the first bearing action member has a rotating body shape with a gradually decreasing diameter from the one end of the shaft to a center of the shaft and includes a first action surface with a tapered shape on which the first bearing acts, and

wherein the second bearing action member has a rotating body shape with a gradually decreasing diameter from the opposite end of the shaft to the center of the shaft and includes a second action surface with a tapered shape on which the second bearing acts.

3. The compressor of claim 2, wherein the first bearing and the second bearing are tapered bearings configured to act on the first action surface and the second action surface, respectively.

4. The compressor of claim 1, wherein blades configured to compress fluid are provided at one end of the impeller with respect to the axial directions of the shaft, and

wherein the impeller is integrated with the first bearing action member at another end of the impeller that is opposite to the one end thereof.

5. The compressor of claim 4, wherein the impeller is referred to as a first impeller, and the blades provided on the first impeller are referred to as first blades,

wherein the compressor further comprises a second impeller secured to the opposite end of the shaft at which the second bearing action member is provided,

wherein second blades are provided at one end of the second impeller with respect to the axial directions of the shaft, and

wherein the second impeller is integrated with the second bearing action member at another end of the second impeller that is opposite to the one end thereof on which the second blades are provided.

6. The compressor of claim 1, wherein the first bearing and the second bearing are air-foil bearings.

7. A compressor comprising:

a shaft extending in axial directions thereof;

a first impeller secured to one end of the shaft and including, at one side thereof, first blades configured to guide a flow of fluid and, at an opposite side thereof, a first action surface with a tapered shape that becomes narrower toward a distal end;

a second impeller secured to an opposite end of the shaft that is opposite to the one end of the shaft to which the first impeller is secured, the second impeller including, at one side thereof, second blades configured to guide the flow of the fluid and, at an opposite side thereof, a second action surface with a tapered shape that becomes narrower toward a distal end; and

a first bearing and a second bearing configured to act on the first action surface and the second action surface, respectively,

wherein the first action surface and the second action surface face each other,

wherein the first bearing acts on the first action surface and supports the first impeller in one of the axial directions and in a radially inward direction of the shaft, and

wherein the second bearing acts on the second action surface and supports the second impeller in another axial direction, which is opposite to the one axial direction, and in the radially inward direction of the shaft.