Hermetic rotary compressor

US9828996B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9828996-B2
Application numberUS-201214653041-A
CountryUS
Kind codeB2
Filing dateDec 20, 2012
Priority dateDec 20, 2012
Publication dateNov 28, 2017
Grant dateNov 28, 2017

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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.

A rotor has at its two axis end portions an upper large-diameter inner circumferential portion and a lower large-diameter inner circumferential portion that have inner diameters larger than the inner diameter of the axially middle portion of the rotor and are offset in the radial direction. A crankshaft has a passageway, which is formed in the crankshaft and allows refrigerant to flow therethrough, and a gas venting hole, which provides communication between the passageway and at least one discharge opening formed in the outer circumferential surface of the crankshaft. The at least one discharge opening is formed at a position facing the inner circumferential surface of the lower large-diameter inner circumferential portion 5 b on the compression unit side.

First claim

Opening claim text (preview).

The invention claimed is: 1. A hermetic rotary compressor, comprising: an electric motor that drives a compression unit configured to compress refrigerant gas; a hermetic container that accommodates the compression unit and the electric motor and contains the refrigerant gas; and a crankshaft that extends from the compression unit to the electric motor and is provided on a rotor in the electric motor, wherein the rotor has two large-diameter inner circumferential portions formed at two axis end portions of the rotor, the large-diameter inner circumferential portions include an upper large-diameter inner circumferential portion and a lower large-diameter inner circumferential portion having inner diameters larger than an inner diameter of an axially middle portion of the rotor, the large-diameter inner circumferential portions have inner diameter centers offset with respect to a rotation axis line of the crankshaft in a radial direction, the crankshaft has a first passageway and a second passageway, the first passageway being formed in the crankshaft and allowing the refrigerant gas to flow through the first passageway, the second passageway providing communication between the first passageway and at least one discharge opening that is formed in an outer circumferential surface of the crankshaft, the at least one discharge opening jets out the refrigerant gas onto an inner circumferential surface of one of the two large-diameter inner circumferential portions and is formed at a position that faces the inner circumferential surface of the one of the two large-diameter inner circumferential portions, the one of the two large-diameter inner circumferential portions is the lower large-diameter inner circumferential portion provided on a side of the compression unit, the second passageway is in communication with the first passageway and penetrates through the crankshaft in the radial direction, and the at least one discharge opening comprises two openings that are provided in a direction in which the one large-diameter inner circumferential portion is offset and in a direction opposite to the direction in which the one large-diameter inner circumferential portion is offset. 2. A hermetic rotary compressor, comprising: an electric motor that drives a compression unit configured to compress refrigerant gas; a hermetic container that accommodates the compression unit and the electric motor and contains the refrigerant gas; and a crankshaft that extends from the compression unit to the electric motor and is provided on a rotor in the electric motor, wherein the rotor has two large-diameter inner circumferential portions formed at two axis end portions of the rotor, the large-diameter inner circumferential portions include an upper large-diameter inner circumferential portion and a lower large-diameter inner circumferential portion having inner diameters larger than an inner diameter of an axially middle portion of the rotor, the large-diameter inner circumferential portions have inner diameter centers offset with respect to a rotation axis line of the crankshaft in a radial direction, the crankshaft has a first passageway and a second passageway, the first passageway being formed in the crankshaft and allowing the refrigerant gas to flow through the first passageway, the second passageway providing communication between the first passageway and at least one discharge opening that is formed in an outer circumferential surface of the crankshaft, the at least one discharge opening jets out the refrigerant gas onto an inner circumferential surface of one of the two large-diameter inner circumferential portions and is formed at a position that faces the inner circumferential surface of the one of the two large-diameter inner circumferential portions, the one of the two large-diameter inner circumferential portions is the lower large-diameter inner circumferential portion provided on a side of the compression unit, and the at least one discharge opening comprises one opening that is provided in a direction opposite to a direction in which the one large-diameter inner circumferential portion is offset. 3. A hermetic rotary compressor, comprising: an electric motor that drives a compression unit configured to compress refrigerant gas; a hermetic container that accommodates the compression unit and the electric motor and contains the refrigerant gas; and a crankshaft that extends from the compression unit to the electric motor and is provided on a rotor in the electric motor, wherein the rotor has two large-diameter inner circumferential portions formed at two axis end portions of the rotor, the large-diameter inner circumferential portions include an upper large-diameter inner circumferential portion and a lower large-diameter inner circumferential portion having inner diameters larger than an inner diameter of an axially middle portion of the rotor, the large-diameter inner circumferential portions have inner diameter centers offset with respect to a rotation axis line of the crankshaft in a radial direction, the crankshaft has a first passageway and a second passageway, the first passageway being formed in the crankshaft and allowing the refrigerant gas to flow through the first passageway, the second passageway providing communication between the first passageway and at least one discharge opening that is formed in an outer circumferential surface of the crankshaft, the at least one discharge opening is formed above an upper end surface of the rotor on an opposite side of the rotor from the compression unit, and the at least one discharge opening is provided in a direction opposite to a direction in which one of the large-diameter inner circumferential portions as the lower large-diameter inner circumferential portion provided on a side of the compression unit is offset.

Assignees

Inventors

Classifications

  • Systems for the equilibration of forces acting on the pump (interstice adjustment other than by fluid pressure F01C21/102) · CPC title

  • F04B39/04Primary

    Measures to avoid lubricant contaminating the pumped fluid · CPC title

  • Hermetic pumps · CPC title

  • crankshaft · CPC title

  • Lubrication (of machines or engines in general F01M) · CPC title

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What does patent US9828996B2 cover?
A rotor has at its two axis end portions an upper large-diameter inner circumferential portion and a lower large-diameter inner circumferential portion that have inner diameters larger than the inner diameter of the axially middle portion of the rotor and are offset in the radial direction. A crankshaft has a passageway, which is formed in the crankshaft and allows refrigerant to flow therethro…
Who is the assignee on this patent?
Tsuchida Kazuchika, Kazama Osamu, Mitsubishi Electric Corp
What technology area does this patent fall under?
Primary CPC classification F04B39/04. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 28 2017 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).