Rotary compressor

US11835045B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11835045-B2
Application numberUS-202217719009-A
CountryUS
Kind codeB2
Filing dateApr 12, 2022
Priority dateOct 15, 2019
Publication dateDec 5, 2023
Grant dateDec 5, 2023

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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 rotary compressor includes a compression mechanism, a casing, a motor stator and a motor rotor. The motor stator includes stacked steel plates, teeth, and slots. The stacked steel plates are fixed to an inner surface of the casing. A number of the teeth and slots is nine. The motor rotor rotates a crankshaft to drive the compression mechanism. The stacked steel plates have first to ninth areas radially outside the nine teeth, first concave portions provided in five of the areas, and a second concave portion provided in at least one of four areas other than the five areas. The five first concave portions and an inner circumferential surface of a cylindrical portion form five first passages. The second concave portion and the inner circumferential surface of the cylindrical portion form at least one second passage.

First claim

Opening claim text (preview).

The invention claimed is: 1. A rotary compressor comprising: a compression mechanism; a casing having a cylindrical portion and covering the compression mechanism; a motor stator including stacked steel plates obtained by stacking a plurality of steel plates, the stacked steel plates fixed to an inner surface of the cylindrical portion, teeth, and slots, a number of the teeth and a number of the slots being nine; and a motor rotor configured to rotate a crankshaft that is configured to drive the compression mechanism, the stacked steel plates having first to ninth areas provided radially outside the nine teeth, first concave portions provided respectively in five of the first to ninth areas, and a second concave portion provided in at least one of four areas other than the five areas including the first concave portions, the five first concave portions and an inner circumferential surface of the cylindrical portion forming five first passages therebetween allowing communication between a first or upper side and a second or bottom side of the motor stator, the second concave portion and the inner circumferential surface of the cylindrical portion forming at least one second passage therebetween allowing communication between the first or upper side and the second or bottom side of the motor stator, each of the first passages having a sectional area that is larger than a sectional area of the second passage, no passage having a sectional area that is larger than the sectional area of the first passage being formed in the four areas other than the five areas where the first passages are located, three or more areas including the first concave portions being not continuous in the first area to the ninth area, and each of the first passages and each of the at least one second passages being circumferentially spaced from circumferentially adjacent the first or second passages. 2. The rotary compressor according to claim 1 , wherein the inner circumferential surface of the cylindrical portion has a radius R, the first sectional area of each of the first passages is 0.003 to 0.008 times πR 2 . 3. The rotary compressor according to claim 1 , wherein the sectional area of the second passage is 10% to 25% of the sectional area of each of the first passages. 4. The rotary compressor according to claim 1 , wherein the inner circumferential surface of the cylindrical portion has a radius R, each of the first passages has a first maximum depth D 1 as a maximum value of a radial length, and the first maximum depth D 1 is 0.05 to 0.11 times the radius R. 5. The rotary compressor according to claim 3 , wherein the inner circumferential surface of the cylindrical portion has a radius R, each of the first passages has a first maximum depth D 1 as a first maximum value of a radial length, and the second passage has a second maximum depth D 2 as a second maximum value of a radial length, the second maximum depth D 2 is 10% to 45% of the first maximum depth D 1 . 6. The rotary compressor according to claim 1 , wherein each of the first passages has a first end and a second end as circumferential ends along the inner circumferential surface of the cylindrical portion, and a first straight line connects a rotation center of the crankshaft and the first end, a second straight line connects the rotation center of the crankshaft and the second end, and the first and second straight lines form an angle of 15 to 35 degrees therebetween. 7. The rotary compressor according to claim 1 , wherein the first to ninth areas are aligned in order, and the stacked steel plates have the first concave portions provided respectively in the first area of the first to ninth areas, the third area of the first to ninth areas, the fourth area of the first to ninth areas, the sixth area of the first to ninth areas, and the eighth area of the first to ninth areas. 8. The rotary compressor according to claim 2 , wherein the sectional area of the second passage is 10% to 25% of the sectional area of each of the first passages. 9. The rotary compressor according to claim 2 , wherein the inner circumferential surface of the cylindrical portion has a radius R, each of the first passages has a first maximum depth D 1 as a maximum value of a radial length, and the first maximum depth D 1 is 0.05 to 0.11 times the radius R. 10. The rotary compressor according to claim 2 , wherein each of the first passages has a first end and a second end as circumferential ends along the inner circumferential surface of the cylindrical portion, and a first straight line connects a rotation center of the crankshaft and the first end, a second straight line connects the rotation center of the crankshaft and the second end, and the first and second straight lines form an angle of 15 to 35 degrees therebetween. 11. The rotary compressor according to claim 2 , wherein the first to ninth areas are aligned in order, and the stacked steel plates have the first concave portions provided respectively in the first area of the first to ninth areas, the third area of the first to ninth areas, the fourth area of the first to ninth areas, the sixth area of the first to ninth areas, and the eighth area of the first to ninth areas. 12. The rotary compressor according to claim 3 , wherein the inner circumferential surface of the cylindrical portion has a radius R, each of the first passages has a first maximum depth D 1 as a maximum value of a radial length, and the first maximum depth D 1 is 0.05 to 0.11 times the radius R. 13. The rotary compressor according to claim 3 , wherein each of the first passages has a first end and a second end as circumferential ends along the inner circumferential surface of the cylindrical portion, and a first straight line connects a rotation center of the crankshaft and the first end, a second straight line connects the rotation center of the crankshaft and the second end, and the first and second straight lines form an angle of 15 to 35 degrees therebetween. 14. The rotary compressor according to claim 3 , wherein the first to ninth areas are aligned in order, and the stacked steel plates have the first concave portions provided respectively in the first area of the first to ninth areas, the third area of the first to ninth areas, the fourth area of the first to ninth areas, the sixth area of the first to ninth areas, and the eighth area of the first to ninth areas. 15. The rotary compressor according to claim 4 , wherein each of the first passages has a first end and a second end as circumferential ends along the inner circumferential surface of the cylindrical portion, and a first straight line connects a rotation center of the crankshaft and the first end, a second straight line connects the rotation center of the crankshaft and the second end, and the first and second straight lines form an angle of 15 to 35 degrees therebetween. 16. The rotary compressor according to claim 4 , wherein the first to ninth areas are aligned in order, and the stacked steel plates have the first concave portions provided respectively in the first area of the first to ninth areas, the third area of the first to ninth areas, the fourth area of the first to ninth areas, the sixth area of the first to ninth areas, and the eighth area of the first to ninth areas. 17. The rotary compressor according to claim 6 , wherein the first to ninth areas are aligned in order, and the stacked steel plates have the first concave portions provided respectively in the fi

Assignees

Inventors

Classifications

  • F04C23/02Primary

    Pumps characterised by combination with, or adaptation to, specific driving engines or motors · CPC title

  • H02K1/165Primary

    Shape, form or location of the slots · CPC title

  • Structural association with mechanical loads, e.g. with hand-held machine tools or fans (with fan or impeller for cooling the machine H02K9/06) · CPC title

  • Electric motor · CPC title

  • Shafts · CPC title

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What does patent US11835045B2 cover?
A rotary compressor includes a compression mechanism, a casing, a motor stator and a motor rotor. The motor stator includes stacked steel plates, teeth, and slots. The stacked steel plates are fixed to an inner surface of the casing. A number of the teeth and slots is nine. The motor rotor rotates a crankshaft to drive the compression mechanism. The stacked steel plates have first to ninth area…
Who is the assignee on this patent?
Daikin Ind Ltd
What technology area does this patent fall under?
Primary CPC classification F04C23/02. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 05 2023 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 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).