US2506298A - Fluid stream directing means - Google Patents

Fluid stream directing means Download PDF

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Publication number
US2506298A
US2506298A US767777A US76777747A US2506298A US 2506298 A US2506298 A US 2506298A US 767777 A US767777 A US 767777A US 76777747 A US76777747 A US 76777747A US 2506298 A US2506298 A US 2506298A
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conduit
gas
gas stream
vanes
motion
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US767777A
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Griffen Ralph
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AMERICAN BLOWER Corp
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AMERICAN BLOWER CORP
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B04CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
    • B04CAPPARATUS USING FREE VORTEX FLOW, e.g. CYCLONES
    • B04C3/00Apparatus in which the axial direction of the vortex flow following a screw-thread type line remains unchanged ; Devices in which one of the two discharge ducts returns centrally through the vortex chamber, a reverse-flow vortex being prevented by bulkheads in the central discharge duct
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B04CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
    • B04CAPPARATUS USING FREE VORTEX FLOW, e.g. CYCLONES
    • B04C3/00Apparatus in which the axial direction of the vortex flow following a screw-thread type line remains unchanged ; Devices in which one of the two discharge ducts returns centrally through the vortex chamber, a reverse-flow vortex being prevented by bulkheads in the central discharge duct
    • B04C2003/006Construction of elements by which the vortex flow is generated or degenerated

Definitions

  • This invention relates to new and useful im provements in means for changing the direction of rotary motion of a fluid stream.
  • An object of this invention'ls to provide a de vice for reducing the rotation of afluid stream having a spiral motion.
  • Another object of this invention is to provide a device for changing the direction of motion of arotating fluid stream from a spiral motion to a longitudinal motion.
  • Another object'ofthis'invention isto provide a' centrifugal separator unit for removing foreign particles from a gas stream and-to provide efii cient'reconversion of kinetic energy of the Totating cleaned'gas into potential energy thereby lowering the drop in static pressure across the unit.
  • drawing- Figure 1 is a'viewinlongitudinal'cross section of a centrifugal'type separator or dust collector having an inlet spinner and an outlet straightening member shown in full elevation;
  • Fig. 2 is an end elevation of the straightening member of Fig. I seen from the line-22 of Fig. 1.
  • centrifugal type'separator-or dust collector I having an inlet conduit s'and an inlet spinner member 3.
  • the inlet conduit 2 has an end portion 4 for attachment to'a gas or air supply.
  • the inlet conduit 2 is operable to receive a dust or particle laden air or gas which passes through the spinner member 3 andis given a rotary motion thereby throwing the particles toward the walls of the conduit 2.
  • An outlet conduit 5 is positioned in theoutlet end portion 6 of the conduit 2 and has an end portion 1 for attachment to' another conduit.
  • the annular space 8 between the conduit E'and the conduit end portion 6 isiclosedby an.-annular plate or cover member 9 having a plurality of apertures 9a therethrough for removal oftheparticles thrown toward the walls of the conduit-2.
  • Each of the aforementioned apertures has. a helical vane member I I3 leading to it for directing theparticles Y for removal with a minimum amount of turbulence.
  • the cover member 9 and apertures therethrough perform the additional function of re stricting the flow of gas through the annular space 8 so as to prevent diversion of clean gas iii thereto from theinlet portion of the conduit 5.
  • In theinlet'end portion I I of the conduit 5 there is :a vanedj-.member I2 for changing the spiral motion of thengas to 'a longitudinal motion.
  • - vaned member I2 has a streamlined body member I3 whichis rounded at the end facing gas flow and tapers toward its rear end portion I5. .
  • a plurality of curved vanes I4 are carried by the body member I3 and are affixed thereto attheir inner peripheries.
  • the -outer peripheries of the vanes-I4 lie substantially on the surface of a cylinder of approximately the same diameter as the inside diameter of the conduit end portion I I and fit tightly thereagainst when the member I2 is inserted therein.
  • the vanes I4 are helically curved toward the rounded end portion.
  • the 'va-ned member I2 is positioned in the inlet end It of-the conduit 5 with a substantial portion thereof extending out from the end portion II.
  • the ends of the vanes I lfacing gas flow terminate substantially in a plane transverse to and 'at -the point of maximum diameter of the body member I3 so' that the rounded end of the body member iB'extends beyond the ends of the vanes.
  • Theamount of curvature of the vanes I4 and the dis'tance'from their ends to the end portion I I of the conduit 5 will vary slightly with the contemplated conditions of operation. If the member I2 is intended to be used with a gas having a high spiral velocity the helical angle of the ends of the'vanes I i will'b'esharper to intercept the gas stream with-maximum efficiency and the distance from the ends- 0f the-vanesto the end portion II will be less. If the member I2 is to be used with a gas having a low spiral velocity, the angle'of the-vanes and distance to theend portion-I I will be greater.
  • vanes M in changing the'directi'on oimotionof the gas stream passing therethrough from a spiral-motion to a longitudinal motion perform the additional function of increasing the head pressureon the gas stream and simultaneously' reducing turbulence so that some ofthe power lost in forcing the gas stream throughtheinlet' spinner 3 is thereby regained.
  • a particle laden gas stream enters the conduit 2 through the spinner 3 which imparts a spiral or rotary motion thereto.
  • the spiral motion given the gas stream operates to throw the particles by centrifugal force towards M of the member l2 which extend out from the end portion H of the conduit '5 and is directed by the vanes I l into the conduit and straightened in its motion by the described change of curvature of the vanes hi.
  • a conduit for receiving a gas stream laden with foreign particles "'2; spinner member for imparting a rotary motion to said gas stream to throw said foreign particles towards the walls of said conduit to cause said particles to concentrate in the portion of said gas stream adjacent the walls of said conduit thereby dividing said gas stream into a central clean portion and a concentrated particle laden outer portion
  • a second conduit of smaller diameter having its inlet end extending concentrically into the outlet end of said first-named conduit and operable to receive said clean central portion of said gas stream
  • a vaned member positioned in the inlet end of said second conduit for reducing the rotation of said gas stream central portion
  • said varied member having a plurality of vanes for receiving and directing the movement of said gas stream central portion, said vanes being helically curved from their lines of initial contact with said gas stream and reducing in curvature toward the discharge end of said vaned member within said second conduit
  • a conduit for receiving a gas stream laden with foreign particles means for imparting a rotary motion to said gas stream to throw said foreign particles towards "the walls of said conduit to cause said particles to concentrate in the portion of said gas stream adjacent the walls of said conduit thereby divid ing said gas stream into a central clean portion and a concentrated particle laden outer portion
  • a second conduit of smaller diameter positioned into the outlet end of said first-named conduit and operable to receive said clean central portion of said gas stream
  • a vaned member positioned in the inlet end of said second conduit for reducing the rotation or" the gas stream passing therethrough, said member having a body portion of streamlined construction having a rounded frontal portion facing the gas stream and taper ing longitudinally in the direction of gas flow, a plurality of vanes for directing the movement of said gas stream central portion, said vanes being affixed to said body portion along their inner periphery and fitting tightly against the Walls of said second conduit at their outer periphery, said

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  • Separating Particles In Gases By Inertia (AREA)

Description

' y 17950 R. GRIFFEN 2,506,293
FLUID STREAM DIRECTING MEANS Filed Aug. 9, 1947 w 7 INV ENTOR.
7 11* BY I]? 4' 1 \m WMKM [I L ATTORNEY Patented May 2, 1950 UNITED STATES PATENT ()FFICE FLUID STREAM DIRECTING' MEANS Ralph Griiifen, Detroit, Mich., assignor to American Blower Corporation, Dearborn, Mich, a corporation of Delaware Application August-9, 1947, Serial No. 767.777
2 Claims. 1
This invention relates to new and useful im provements in means for changing the direction of rotary motion of a fluid stream.
An object of this invention'ls to provide a de vice for reducing the rotation of afluid stream having a spiral motion.
Another object of this invention is to provide a device for changing the direction of motion of arotating fluid stream from a spiral motion to a longitudinal motion.
Another object'ofthis'invention isto provide a' centrifugal separator unit for removing foreign particles from a gas stream and-to provide efii cient'reconversion of kinetic energy of the Totating cleaned'gas into potential energy thereby lowering the drop in static pressure across the unit.
Other objects of this invention will become a1 parent'from time to timethroughout the specificationand claims as hereinafter stated.
In the accompanying drawings, to be taken as a part of this specification there is clearlyand fully illustrated a-preferred embodiment of this invention, in which drawing- Figure 1 is a'viewinlongitudinal'cross section of a centrifugal'type separator or dust collector having an inlet spinner and an outlet straightening member shown in full elevation;
Fig. 2 is an end elevation of the straightening member of Fig. I seen from the line-22 of Fig. 1.
Referring to the drawings by characters of'reference there is a centrifugal type'separator-or dust collector I having an inlet conduit s'and an inlet spinner member 3. The inlet conduit 2 has an end portion 4 for attachment to'a gas or air supply. The inlet conduit 2 is operable to receive a dust or particle laden air or gas which passes through the spinner member 3 andis given a rotary motion thereby throwing the particles toward the walls of the conduit 2. An outlet conduit 5 is positioned in theoutlet end portion 6 of the conduit 2 and has an end portion 1 for attachment to' another conduit. The annular space 8 between the conduit E'and the conduit end portion 6 isiclosedby an.-annular plate or cover member 9 having a plurality of apertures 9a therethrough for removal oftheparticles thrown toward the walls of the conduit-2. Each of the aforementioned apertures has. a helical vane member I I3 leading to it for directing theparticles Y for removal with a minimum amount of turbulence. The cover member 9 and apertures therethrough perform the additional function of re stricting the flow of gas through the annular space 8 so as to prevent diversion of clean gas iii thereto from theinlet portion of the conduit 5. In theinlet'end portion I I of the conduit 5 there is :a vanedj-.member I2 for changing the spiral motion of thengas to 'a longitudinal motion. The
- vaned member I2 has a streamlined body member I3 whichis rounded at the end facing gas flow and tapers toward its rear end portion I5. .A plurality of curved vanes I4 are carried by the body member I3 and are affixed thereto attheir inner peripheries. The -outer peripheries of the vanes-I4 :lie substantially on the surface of a cylinder of approximately the same diameter as the inside diameter of the conduit end portion I I and fit tightly thereagainst when the member I2 is inserted therein. The vanes I4 are helically curved toward the rounded end portion. ofthe body member, I3 for intercepting the spirally moving :ga-s substantially tangential to the spiral path of motion of the gas and gradually reduce in curvature toward the rear end portion I5 so .they'terminatein plane-portions I6 running the planexof the axis of the conduit 5. The 'va-ned member I2 .is positioned in the inlet end It of-the conduit 5 with a substantial portion thereof extending out from the end portion II. The ends of the vanes I lfacing gas flow terminate substantially in a plane transverse to and 'at -the point of maximum diameter of the body member I3 so' that the rounded end of the body member iB'extends beyond the ends of the vanes. Theamount of curvature of the vanes I4 and the dis'tance'from their ends to the end portion I I of the conduit 5 will vary slightly with the contemplated conditions of operation. If the member I2 is intended to be used with a gas having a high spiral velocity the helical angle of the ends of the'vanes I i will'b'esharper to intercept the gas stream with-maximum efficiency and the distance from the ends- 0f the-vanesto the end portion II will be less. If the member I2 is to be used with a gas having a low spiral velocity, the angle'of the-vanes and distance to theend portion-I I will be greater. The vanes M in changing the'directi'on oimotionof the gas stream passing therethrough from a spiral-motion to a longitudinal motion perform the additional function of increasing the head pressureon the gas stream and simultaneously' reducing turbulence so that some ofthe power lost in forcing the gas stream throughtheinlet' spinner 3 is thereby regained.
In operation, a particle laden gas stream enters the conduit 2 through the spinner 3 which imparts a spiral or rotary motion thereto. The spiral motion given the gas stream operates to throw the particles by centrifugal force towards M of the member l2 which extend out from the end portion H of the conduit '5 and is directed by the vanes I l into the conduit and straightened in its motion by the described change of curvature of the vanes hi. Thus it is seen that a gas stream is given a spiral motion for separatlng foreign particles upon admission to this separator and by the use of the straightening member i2 is restored to its longitudinal movement upon emerging therefrom. It should be further noted that when the incoming gas passes through theinlet spinner 3 it is accelerated and the poten tial energy of the gas is transformed into kinetic energy of rotation resulting in a pressure drop across the spinner 3. The rotating gas upon intercepting the vaned member I2 is restored to a longitudinal motion with the result that the kinetic energy of rotation is transformed into potential energy of static pressure and a considerable amount of the pressure lost in passing the spinner 3 is regained, thereby decreasing the drop in static pressure across the unit as a Whole.
What is claimed and is desired to be secured by Letters Patent of the United States is: 1. In a' centrifugal separator, a conduit for receiving a gas stream laden with foreign particles, "'2; spinner member for imparting a rotary motion to said gas stream to throw said foreign particles towards the walls of said conduit to cause said particles to concentrate in the portion of said gas stream adjacent the walls of said conduit thereby dividing said gas stream into a central clean portion and a concentrated particle laden outer portion, a second conduit of smaller diameter having its inlet end extending concentrically into the outlet end of said first-named conduit and operable to receive said clean central portion of said gas stream, a vaned member positioned in the inlet end of said second conduit for reducing the rotation of said gas stream central portion, said varied member having a plurality of vanes for receiving and directing the movement of said gas stream central portion, said vanes being helically curved from their lines of initial contact with said gas stream and reducing in curvature toward the discharge end of said vaned member within said second conduit, the change of curvature of said vanes being such that said gas stream central portion will be substantially free from rotation and turbulence upon emerging from said varied member, a plate member fitting around said sec-- ond conduit and joined to said first-named conduit and having at least one aperture for the discharge oi particle laden gas from the annular space between said conduits, said plate member having a vane portion leading to said aperture, said vane portion being operable to intercept said particle laden gas portion substantially tangential to its direction'of motion so that said particle laden gas portion may be discharged with little 4 turbulence, and said plate member being operable to restrict the flow of gas through the annular space between said conduits thereby to prevent said clean central portion of gas from being deflected into said annular space by said vaned member.
2. In a centrifugal separator, a conduit for receiving a gas stream laden with foreign particles, means for imparting a rotary motion to said gas stream to throw said foreign particles towards "the walls of said conduit to cause said particles to concentrate in the portion of said gas stream adjacent the walls of said conduit thereby divid ing said gas stream into a central clean portion and a concentrated particle laden outer portion, a second conduit of smaller diameter positioned into the outlet end of said first-named conduit and operable to receive said clean central portion of said gas stream, a vaned member positioned in the inlet end of said second conduit for reducing the rotation or" the gas stream passing therethrough, said member having a body portion of streamlined construction having a rounded frontal portion facing the gas stream and taper ing longitudinally in the direction of gas flow, a plurality of vanes for directing the movement of said gas stream central portion, said vanes being affixed to said body portion along their inner periphery and fitting tightly against the Walls of said second conduit at their outer periphery, said vanes being helically curved at the end of said body portion facing gas flow and intercepting the gas stream central portion substantially tangential to the direction of motion of the same and decreasing in curvature longitudinally in the direction of gas flow terminating in straight portions running in the plane of the axis of said second conduit, and said body portion and the helically curved portion of said vanes extending outside the inlet end of said second conduit to receive and direct said gas stream central portion into said second conduit and to change its direction of movement from a spiral motion to a motion substantially parallel to the axis of said second conduit, a plate member surrounding said second conduit and extending across the annular space between the ends of said conduits and hav-- ing at least one aperture for the discharge of particle laden gas, said plate member having a heli cal vane portion leading to said aperture, said vane portion being operable to intercept said particle laden gas portion substantially tangential to its direction of motion so that said particle laden gas may be discharged with little turbulence, and said plate member being operable to restrict the iiow or" gas through the annular space between said conduits thereby to prevent said clean central portion of gas from being deflected into said annular space by said varied member.
RALPH GRIFFEN.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name A Date 1,146,218 Kamrath Feb. 4, 1930 1,876,092. Harper Sept. 6,1932
' 2,370,629 Appeldoorn Mar. 6, 1945 2,393,112 Lincoln Jan. 15, 1946
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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569909A (en) * 1948-01-26 1951-10-02 Power Jets Res & Dev Ltd Nonrotary centrifugal separator
US2659450A (en) * 1950-08-18 1953-11-17 Fluor Corp Pulsation eliminator and gas cleaner
US2659451A (en) * 1950-08-18 1953-11-17 Fluor Corp Centrifugal gas cleaner
US2712859A (en) * 1952-04-30 1955-07-12 Research Corp Centrifugal gas cleaning device
US2757581A (en) * 1952-09-24 1956-08-07 Nichols Engineering And Res Co Vortex separators
US2771157A (en) * 1952-07-11 1956-11-20 Hjorth & Co Ab Method of converting kinetic energy to pressure energy and a device for carrying out the method
US2802545A (en) * 1951-11-09 1957-08-13 Heinrich Richard Fritz Cyclone dust separators
DE1061601B (en) * 1953-05-22 1959-07-16 Licentia Gmbh Two-stage centrifugal dust separator with predominantly rotating flow moving in the axial direction
DE973021C (en) * 1950-09-07 1959-11-19 Waagner Biro Ag Centrifugal dust separator with a multi-stage centrifugal chamber that runs straight through from the rotational flow in the axial direction
US2936043A (en) * 1957-01-09 1960-05-10 Cottrell Res Inc Cyclonic dust collector
US3216182A (en) * 1964-10-06 1965-11-09 Gen Electric Axial flow vapor-liquid separator
US3613887A (en) * 1968-10-14 1971-10-19 Nils Anders Lennart Wikdahl Clyclone separator to be built in a casing or similar
FR2353738A1 (en) * 1976-06-05 1977-12-30 Messerschmitt Boelkow Blohm DEVICE FOR RETRANSFORMATION INTO POTENTIAL ENERGY OF THE GIRATORY KINETIC ENERGY OF A FLOWING FLUID
US4283206A (en) * 1978-05-12 1981-08-11 Stein Industrie Component for de-spinning a flow of dry vapor or gas and liquid and for separating the liquid from the vapor or gas
FR2681259A1 (en) * 1991-09-13 1993-03-19 Bertin & Cie Cyclone cell having an axial inlet and direct passage, and fluid purification apparatus using this cell
US6190438B1 (en) 1997-01-02 2001-02-20 Thermo Black Clawson Inc. Mist eliminator
US20030115843A1 (en) * 2000-12-22 2003-06-26 Trygve Haland Apparatus for separation of a liquid from a multiphase fluid flow
WO2003066195A1 (en) * 2002-02-08 2003-08-14 Norsk Hydro Asa Device for the transformation of gas/liquid flow to laminar or stratified flow
US6630014B1 (en) 1999-07-12 2003-10-07 Kadant Black Clawson Inc. Mist eliminator
EP1512453A1 (en) * 2003-08-30 2005-03-09 Mann+Hummel Gmbh Device for separation of particles from a media flow
US20090101013A1 (en) * 2007-10-23 2009-04-23 Moredock James G Powered air cleaning system and air cleaning method
US20120151886A1 (en) * 2010-12-20 2012-06-21 Microsoft Corporation Self cleaning fan assembly
US8657928B2 (en) 2011-07-29 2014-02-25 The Sy-Klone Company Versatile compact air precleaner, air cleaning method and disposable air filter cartridge for air precleaner
US20150047304A1 (en) * 2012-03-30 2015-02-19 Xu Bai Axial flow-type cyclone dust collection device
US20190009203A1 (en) * 2017-07-10 2019-01-10 Hamilton Sundstrand Corporation Vented dynamic pressure recovery module for aircraft ecs
IT201800004356A1 (en) * 2018-04-10 2019-10-10 AXIAL CYCLONIC APPARATUS FOR THE ABATEMENT OF PARTICULATES AND SPARKS FROM A GASEOUS FLOW AND FUME EXTRACTION SYSTEM OF A METALLURIGIC FURNACE EQUIPPED WITH THIS CYCLONIC APPARATUS

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1746218A (en) * 1927-04-08 1930-02-04 Ac Spark Plug Co Air cleaner
US1876002A (en) * 1930-06-06 1932-09-06 Bartlett Hayward Co Centrifugal dry-dust arrester
US2370629A (en) * 1943-06-02 1945-03-06 William R Appeldoorn Dust precipitator
US2393112A (en) * 1943-01-01 1946-01-15 B F Sturtevant Co Dust collector system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1746218A (en) * 1927-04-08 1930-02-04 Ac Spark Plug Co Air cleaner
US1876002A (en) * 1930-06-06 1932-09-06 Bartlett Hayward Co Centrifugal dry-dust arrester
US2393112A (en) * 1943-01-01 1946-01-15 B F Sturtevant Co Dust collector system
US2370629A (en) * 1943-06-02 1945-03-06 William R Appeldoorn Dust precipitator

Cited By (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2569909A (en) * 1948-01-26 1951-10-02 Power Jets Res & Dev Ltd Nonrotary centrifugal separator
US2659450A (en) * 1950-08-18 1953-11-17 Fluor Corp Pulsation eliminator and gas cleaner
US2659451A (en) * 1950-08-18 1953-11-17 Fluor Corp Centrifugal gas cleaner
DE973021C (en) * 1950-09-07 1959-11-19 Waagner Biro Ag Centrifugal dust separator with a multi-stage centrifugal chamber that runs straight through from the rotational flow in the axial direction
US2802545A (en) * 1951-11-09 1957-08-13 Heinrich Richard Fritz Cyclone dust separators
US2712859A (en) * 1952-04-30 1955-07-12 Research Corp Centrifugal gas cleaning device
US2771157A (en) * 1952-07-11 1956-11-20 Hjorth & Co Ab Method of converting kinetic energy to pressure energy and a device for carrying out the method
US2757581A (en) * 1952-09-24 1956-08-07 Nichols Engineering And Res Co Vortex separators
DE1061601B (en) * 1953-05-22 1959-07-16 Licentia Gmbh Two-stage centrifugal dust separator with predominantly rotating flow moving in the axial direction
US2936043A (en) * 1957-01-09 1960-05-10 Cottrell Res Inc Cyclonic dust collector
US3216182A (en) * 1964-10-06 1965-11-09 Gen Electric Axial flow vapor-liquid separator
US3613887A (en) * 1968-10-14 1971-10-19 Nils Anders Lennart Wikdahl Clyclone separator to be built in a casing or similar
FR2353738A1 (en) * 1976-06-05 1977-12-30 Messerschmitt Boelkow Blohm DEVICE FOR RETRANSFORMATION INTO POTENTIAL ENERGY OF THE GIRATORY KINETIC ENERGY OF A FLOWING FLUID
US4283206A (en) * 1978-05-12 1981-08-11 Stein Industrie Component for de-spinning a flow of dry vapor or gas and liquid and for separating the liquid from the vapor or gas
FR2681259A1 (en) * 1991-09-13 1993-03-19 Bertin & Cie Cyclone cell having an axial inlet and direct passage, and fluid purification apparatus using this cell
US6190438B1 (en) 1997-01-02 2001-02-20 Thermo Black Clawson Inc. Mist eliminator
US6630014B1 (en) 1999-07-12 2003-10-07 Kadant Black Clawson Inc. Mist eliminator
US20030115843A1 (en) * 2000-12-22 2003-06-26 Trygve Haland Apparatus for separation of a liquid from a multiphase fluid flow
US6752845B2 (en) * 2000-12-22 2004-06-22 Statoil Asa Apparatus for separation of a liquid from a multiphase fluid flow
WO2003066195A1 (en) * 2002-02-08 2003-08-14 Norsk Hydro Asa Device for the transformation of gas/liquid flow to laminar or stratified flow
AU2003206266B2 (en) * 2002-02-08 2008-07-17 Equinor Energy As Device for the transformation of gas/liquid flow to laminar or stratified flow
US20050066637A1 (en) * 2002-02-08 2005-03-31 Per Gramme Device for the transformation of gas/liquid flow to laminar or stratified flow
US7559975B2 (en) 2002-02-08 2009-07-14 Norsk Hydro Asa Process for transforming gas/liquid flow into laminar or stratified flow
CN1308056C (en) * 2002-02-08 2007-04-04 诺尔斯海德公司 Device for the transformation of gas/liquid flow to laminar or stratified flow
US20080216656A1 (en) * 2002-02-08 2008-09-11 Per Gramme Process for transforming gas/liquid flow into laminar or stratified flow
EP1512453A1 (en) * 2003-08-30 2005-03-09 Mann+Hummel Gmbh Device for separation of particles from a media flow
US20050086915A1 (en) * 2003-08-30 2005-04-28 Mann & Hummel Gmbh Apparatus for separating particles from a flowing medium
US7258727B2 (en) * 2003-08-30 2007-08-21 Mann & Hummel Gmbh Apparatus for separating particles from a flowing medium
US8216330B2 (en) 2007-10-23 2012-07-10 The Sy-Klone Company Powered air cleaning system and air cleaning method
US20090101013A1 (en) * 2007-10-23 2009-04-23 Moredock James G Powered air cleaning system and air cleaning method
EP2203237A1 (en) * 2007-10-23 2010-07-07 The Sy-Klone Company Powered air cleaning system and air cleaning method
EP2203237A4 (en) * 2007-10-23 2011-03-23 Sy Klone Company Powered air cleaning system and air cleaning method
US8007565B2 (en) 2007-10-23 2011-08-30 The Sy-Klone Company Powered air cleaning system and air cleaning method
US8480775B2 (en) * 2010-12-20 2013-07-09 Microsoft Corporation Self cleaning fan assembly
US20120151886A1 (en) * 2010-12-20 2012-06-21 Microsoft Corporation Self cleaning fan assembly
US8657928B2 (en) 2011-07-29 2014-02-25 The Sy-Klone Company Versatile compact air precleaner, air cleaning method and disposable air filter cartridge for air precleaner
US8945282B2 (en) 2011-07-29 2015-02-03 The Sy-Klone Company Versatile compact air precleaner, air cleaning method and disposable air filter cartridge for air precleaner
US9700828B2 (en) 2011-07-29 2017-07-11 The Sy-Klone Company Versatile compact air precleaner, air cleaning method and disposable air filter cartridge for air precleaner
US20150047304A1 (en) * 2012-03-30 2015-02-19 Xu Bai Axial flow-type cyclone dust collection device
US20190009203A1 (en) * 2017-07-10 2019-01-10 Hamilton Sundstrand Corporation Vented dynamic pressure recovery module for aircraft ecs
US10744437B2 (en) * 2017-07-10 2020-08-18 Hamilton Sunstrand Corporation Vented dynamic pressure recovery module for aircraft ECS
IT201800004356A1 (en) * 2018-04-10 2019-10-10 AXIAL CYCLONIC APPARATUS FOR THE ABATEMENT OF PARTICULATES AND SPARKS FROM A GASEOUS FLOW AND FUME EXTRACTION SYSTEM OF A METALLURIGIC FURNACE EQUIPPED WITH THIS CYCLONIC APPARATUS
WO2019197978A1 (en) * 2018-04-10 2019-10-17 Sms Group S.P.A. Axial cyclonic apparatus for the abatement of particulate matter and sparks from a gaseous flow and smoke suction system of a metallurgical furnace provided with such cyclonic apparatus

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