Apparatus for the cleaning of crankcase gas

US9840951B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9840951-B2
Application numberUS-201314385429-A
CountryUS
Kind codeB2
Filing dateMar 11, 2013
Priority dateMar 13, 2012
Publication dateDec 12, 2017
Grant dateDec 12, 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.

An apparatus for the cleaning of crankcase gas from an internal combustion engine includes a housing and a separation chamber for the crankcase gas with a centrifugal rotor arranged for the cleaning of the crankcase gas in the separation chamber. The centrifugal rotor includes a drive shaft extending into a drive chamber of the apparatus. A turbine is connected to the drive shaft. A nozzle is arranged to receive pressurized liquid from the combustion engine and to direct the pressurized liquid in a jet from a nozzle opening against the turbine for rotation of the centrifugal rotor. An adapter element is configured such that the apparatus is mountable onto the combustion engine with a drive liquid passage in communication with the nozzle. The nozzle is integrally formed with the adapter element with a nozzle passage having a conical shape which converges in the flow direction towards the nozzle opening.

First claim

Opening claim text (preview).

The invention claimed is: 1. An apparatus for cleaning of crankcase gas from a combustion engine, the apparatus comprising: a centrifugal rotor, said centrifugal rotor being arranged to rotate about a rotational axis and adapted for the cleaning of the crankcase gas in a separation chamber, the centrifugal rotor comprising a drive shaft extending into a drive chamber of the apparatus; a turbine connected to the drive shaft; a nozzle arranged to receive pressurized liquid from the combustion engine and to direct the pressurized liquid in a jet from a nozzle opening thereof against the turbine for rotation of the centrifugal rotor; and an adapter element for mounting the apparatus onto the combustion engine, the adapter element comprising: an abutment surface arranged to abut against a corresponding abutment surface on the combustion engine, the abutment surface of the adapter element having a drive liquid opening arranged to receive the pressurized liquid from a supply opening in the abutment surface of the combustion engine; and a drive liquid passage connecting the drive liquid opening with the nozzle, wherein the nozzle is integrally formed with the adapter element with a nozzle passage having a conical shape which converges in a flow direction towards the nozzle opening, and wherein the conical shape of the nozzle passage converges to form an angle in a range of 5°-9° to a center line of the nozzle passage, wherein the turbine is arranged with buckets for receiving the jet of pressurized liquid, the buckets being configured such that a liquid jet direction is reversed along a height of the bucket, and wherein the height of the bucket is 2-2.5 times a diameter of the nozzle opening. 2. The apparatus according to claim 1 , wherein the conical shape of the nozzle passage converges to form an angle of 7° to the center line of the nozzle passage. 3. The apparatus according to claim 1 , wherein the buckets are configured with an inner curved part for reversing the liquid along the height of the bucket, which inner curved part transitions into outer straight parts diverging in a direction radially outwardly. 4. The apparatus according to claim 1 , wherein the bucket height is 2-2.5 times the diameter of the nozzle opening. 5. The apparatus according to claim 1 , wherein the bucket height is 2.3 times the diameter of the nozzle opening. 6. The apparatus according to claim 1 , wherein the drive liquid passage is configured with a longitudinal portion having a conical shape for converging pressurized liquid into the conical nozzle passage. 7. The apparatus according to claim 6 , wherein the nozzle passage and drive liquid passage form a continuous passage comprising several longitudinal portions of different conical shapes which gradually converge in the flow direction towards the nozzle opening. 8. The apparatus according to claim 1 , wherein the turbine is configured with a radius such that a ratio (V 1 /V 2 ) between a fluid jet speed (V 1 ) and a tangential speed (V 2 ) of the turbine at the radius where the fluid jet is arranged to hit the bucket is 2-3 during operation of the centrifugal rotor. 9. The apparatus according to claim 8 , wherein said ratio (V 1 /V 2 ) is 2.2-2.6. 10. The apparatus according to claim 8 , wherein said ratio (V 1 /V 2 ) is 2.4. 11. The apparatus according to claim 1 , wherein the conical shape of the nozzle passage converges at least along a major longitudinal portion of the nozzle passage. 12. The apparatus according to claim 11 , wherein the conical shape of the nozzle passage converges along an entire length of the nozzle passage up to the nozzle opening. 13. The apparatus according to claim 11 , wherein the nozzle passage comprises a minor longitudinal portion having a cylindrical shape at the nozzle opening, wherein the minor longitudinal portion is several times shorter than the major longitudinal portion having the conical shape. 14. The apparatus according to claim 13 , wherein the minor longitudinal portion having the cylindrical shape at the nozzle opening constitutes 0.1-1 mm of the nozzle passage. 15. An apparatus for cleaning of crankcase gas from a combustion engine, the apparatus comprising: a centrifugal rotor, said centrifugal rotor being arranged to rotate about a rotational axis and adapted for the cleaning of the crankcase gas in a separation chamber, the centrifugal rotor comprising a drive shaft extending into a drive chamber of the apparatus; a turbine connected to the drive shaft; a nozzle arranged to receive pressurized liquid from the combustion engine and to direct the pressurized liquid in a jet from a nozzle opening thereof against the turbine for rotation of the centrifugal rotor; and an adapter element for mounting the apparatus onto the combustion engine, the adapter element comprising: an abutment surface arranged to abut against a corresponding abutment surface on the combustion engine, the abutment surface of the adapter element having a drive liquid opening arranged to receive the pressurized liquid from a supply opening in the abutment surface of the combustion engine; and a drive liquid passage connecting the drive liquid opening with the nozzle, wherein the nozzle is integrally formed with the adapter element with a nozzle passage having a conical shape which converges in a flow direction towards the nozzle opening, wherein the nozzle opening is arranged at a distance of 0.5-5 mm from the turbine, and wherein the conical shape of the nozzle passage converges to form an angle in the range of 5°-9° to a center line of the nozzle passage, wherein the turbine is arranged with buckets for receiving the jet of pressurized liquid, the buckets being configured such that the liquid jet direction is reversed along a height of the bucket, and wherein the height of the bucket is 2-2.5 times the diameter of the nozzle opening. 16. An apparatus for cleaning of crankcase gas from a combustion engine, the apparatus comprising: a centrifugal rotor, said centrifugal rotor being arranged to rotate about a rotational axis and adapted for the cleaning of the crankcase gas in a separation chamber, the centrifugal rotor comprising a drive shaft extending into a drive chamber of the apparatus; a turbine connected to the drive shaft; a nozzle arranged to receive pressurized liquid from the combustion engine and to direct the pressurized liquid in a jet from a nozzle opening thereof against the turbine for rotation of the centrifugal rotor; and an adapter element for mounting the apparatus onto the combustion engine, the adapter element comprising: an abutment surface arranged to abut against a corresponding abutment surface on the combustion engine, the abutment surface of the adapter element having a drive liquid opening arranged to receive the pressurized liquid from a supply opening in the abutment surface of the combustion engine; and a drive liquid passage connecting the drive liquid opening with the nozzle, wherein the nozzle is integrally formed with the adapter element with a nozzle passage having a conical shape which converges in the flow direction towards the nozzle opening, and wherein the nozzle opening is arranged at a distance of 0.5-5 mm from the turbine, wherein the adapter element is configured to form a drive chamber casing and is releasably connected to a housing for the separation chamber, wherein a partition is arranged between the housing and the adapter element in such a manner that the drive chamber is delimited by the partition and the drive chamber casing, the drive shaft of the centrifugal rotor extend

Assignees

Inventors

Classifications

  • Centrifugal separators or filters for fluid circulation systems, e.g. for lubricant oil circulation systems · CPC title

  • Centrifuges in which rotors other than bowls generate centrifugal effects in stationary containers · CPC title

  • F01M13/04Primary

    having means for purifying air before leaving crankcase, e.g. removing oil · CPC title

  • generated by rotating vanes, discs, drums or brushes · CPC title

  • Separating oil and gas with a centrifuge device · CPC title

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What does patent US9840951B2 cover?
An apparatus for the cleaning of crankcase gas from an internal combustion engine includes a housing and a separation chamber for the crankcase gas with a centrifugal rotor arranged for the cleaning of the crankcase gas in the separation chamber. The centrifugal rotor includes a drive shaft extending into a drive chamber of the apparatus. A turbine is connected to the drive shaft. A nozzle is a…
Who is the assignee on this patent?
Alfa Laval Corp Ab
What technology area does this patent fall under?
Primary CPC classification F01M13/04. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 12 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).