Direct drive refrigerant screw compressor with refrigerant lubricated rotors

US11898561B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11898561-B2
Application numberUS-202016973724-A
CountryUS
Kind codeB2
Filing dateMay 19, 2020
Priority dateMay 20, 2019
Publication dateFeb 13, 2024
Grant dateFeb 13, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

Disclosed is a direct-drive refrigerant screw compressor, having: a housing; a compression chamber in the housing; a pair of rotors, each rotor of the pair of rotors being rotationally disposed in the compression chamber and including an outer surface with a screw-geared profile; a fluid being disposed in the compression chamber, the fluid consisting of a working fluid for providing lubrication to each rotor; a first port extending through the housing and configured for directing the fluid toward the compression chamber; and when the compressor is activated, each rotor rotates and the fluid is distributed about each rotor to lubricate each rotor.

First claim

Opening claim text (preview).

We claim: 1. A direct-drive refrigerant screw compressor, comprising: a housing; a compression chamber in the housing; a motor in the housing; a pair of rotors disposed in the compression chamber, the pair of rotors including a first rotor and a second rotor, the second rotor having respective first and second axial shaft portions, the first axial shaft portion being driven by the motor, each rotor of the pair of rotors being rotationally disposed in the compression chamber and including an outer surface with a screw-geared profile to define alternating peaks and troughs axially along the outer surface; a working fluid being disposed in the compression chamber for providing lubrication to each rotor, wherein the working fluid is refrigerant; a first port extending through the housing and configured for directing the working fluid toward the compression chamber; wherein: for each rotor, the compressor includes a plurality of bearing packs disposed within a respective plurality of bearing chambers; the first port is fluidly connected to a passage only in the second shaft portion and in the second rotor of the pair of rotors that directs the working fluid to the compression chamber; the passage extends between an axial aft port of the second rotor passing through the second axial shaft portion and into the second rotor to end at the outer surface of the second rotor; the axial aft port extends through one of the plurality of bearing chambers; and the passage includes an axial segment forming a blind hole and a plurality of radial segments that are axially spaced apart from each other and fluidly connected between the axial segment and a respective plurality of surface ports that are axially spaced apart from each other on the outer surface of the second rotor, and the passage includes a flow control orifice located aft of the plurality of radial segments, wherein the plurality of surface ports are axially spaced apart at regular intervals along the outer surface of only the second rotor of the pair of rotors, wherein at least one first surface port of the plurality of surface ports is positioned at or proximate a peak of the alternating peaks and troughs and at least one second surface port of the plurality of surface ports is disposed at or proximate a trough of the alternating peaks and troughs; wherein the plurality of surface ports are configured to distribute the working fluid provided through the passage along the outer surface of the second rotor, so that when the motor operates to rotate the second rotor, the second rotor rotates the first rotor and disperses the distributed working fluid on the outer surface of the second rotor to provide the lubrication to the first rotor and the second rotor. 2. The compressor of claim 1 , wherein: the plurality of the radial segments each include opposing radial portions extending to respective surface ports of the plurality of the surface ports on the outer surface of the second rotor. 3. A refrigerant system including: a condenser; the compressor of claim 1 ; and a conduit fluidly connecting the condenser and the first port of the compressor, and configured to transport fluid to the first port of the compressor. 4. A method of directing fluid in a direct drive screw compressor, comprising: receiving fluid at a first port of a housing of the compressor, wherein the fluid consists of a working fluid for providing lubrication to each rotor of a pair of rotors disposed in a compression chamber defined in the housing, the pair of rotors including a first rotor and a second rotor, each rotor including an outer surface with a screw-geared profile to define alternating peaks and troughs axially along the outer surface, wherein the working fluid is refrigerant, the second rotor having respective first and second axial shaft portions, the first axial shaft portion being driven by a motor disposed in the housing; and directing the working fluid from the first port through the second axial shaft portion and the second rotor to the compression chamber, wherein: when the compressor is activated, each rotor rotates and the working fluid is distributed about each rotor to lubricate each rotor; and for each rotor, a plurality of bearing packs is disposed within a respective plurality of bearing chambers in the housing, and wherein the method further includes: the directing the working fluid from the first port to the compression chamber further includes injecting the working fluid from the first port through a passage only formed in the second rotor of the pair of rotors so that working fluid is injected into the compression chamber from the second rotor; the injecting the working fluid through the passage further includes directing the working fluid from the first port into an axial aft port of the passage and out a plurality of surface ports an outer surface of only the second rotor, wherein the axial aft port extends through one of the plurality of bearing chambers; and the directing the working fluid through the passage further includes directing the working fluid through an axial segment forming a blind hole in the second rotor and a plurality of radial segments that are axially spaced apart from each other and fluidly connected between the axial segment and the respective plurality of surface ports that are axially spaced apart from each other on the outer surface of the second rotor, to distribute the working fluid about the pair of rotors, wherein the plurality of surface ports are axially spaced apart at regular intervals along the outer surface of only the second rotor of the pair of rotors, the outer surface of the second rotor that includes the alternating peaks and troughs defined axially along the outer surface of the second rotor so that at least one first surface port of the plurality of surface ports is positioned at or proximate a peak of the alternating peaks and troughs and at least one second surface port of the plurality of surface ports is disposed at or proximate a trough of the alternating peaks and troughs; and controlling flow of the working fluid through the passage with a flow control orifice located in the passage at a position aft of the plurality of radial segments. 5. The method of claim 4 , wherein: the directing the working fluid through the passage further includes: directing the working fluid through opposing radial portions of each of the plurality of the radial segments, the opposing radial portions extending to respective surface ports of the plurality of the surface ports on the outer surface of the second rotor. 6. The method of claim 4 , comprising: receiving the fluid at the first port from a condenser in a refrigerant system in which the compressor is integrated.

Assignees

Inventors

Classifications

  • F04C29/02Primary

    Lubrication (of machines or engines in general F01M); Lubricant separation (separation in general B01D) · CPC title

  • F04C18/16Primary

    with helical teeth, e.g. chevron-shaped, screw type {(for non-parallel axes of movement F04C18/48)} · CPC title

  • Lubricant distribution through a hollow driving shaft (F04C29/025 takes precedence) · CPC title

  • Means for improving or restricting lubricant flow · CPC title

  • F04C29/026Primary

    Lubricant separation · CPC title

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What does patent US11898561B2 cover?
Disclosed is a direct-drive refrigerant screw compressor, having: a housing; a compression chamber in the housing; a pair of rotors, each rotor of the pair of rotors being rotationally disposed in the compression chamber and including an outer surface with a screw-geared profile; a fluid being disposed in the compression chamber, the fluid consisting of a working fluid for providing lubrication…
Who is the assignee on this patent?
Carrier Corp
What technology area does this patent fall under?
Primary CPC classification F04C29/02. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 13 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 6 related publications on this page (citations in our corpus or others sharing the same primary CPC).