US1974110A - Curved conduit - Google Patents

Curved conduit Download PDF

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Publication number
US1974110A
US1974110A US648263A US64826332A US1974110A US 1974110 A US1974110 A US 1974110A US 648263 A US648263 A US 648263A US 64826332 A US64826332 A US 64826332A US 1974110 A US1974110 A US 1974110A
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way
pipe
fins
stream
conduit
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US648263A
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Frank R Higley
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15DFLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00Influencing flow of fluids
    • F15D1/02Influencing flow of fluids in pipes or conduits
    • F15D1/04Arrangements of guide vanes in pipe elbows or duct bends; Construction of pipe conduit elements or elbows with respect to flow, specially for reducing losses in flow

Definitions

  • This invention relates to improvements in the type of conduit having a curved way, that is, to a pipe device having a through passageway, the entrance to which is adapted to receive the flow from one direction and theconduit being adapted to change the direction of this fiow so that the conduit discharge opening, at the opposite end of the way, will discharge the flow in another direction.
  • An example is the ordinary elbow pipe fitting adapted to interconnect a pair of straight pipe lengths angularly related but in a common plane.
  • Methods of pipe fitting such as employing threaded and flanged joints, are rapidly being supplanted by weldedjoints wherein the inner pipe surface is substantially uninterrupted at its joints, and turbulence caused by joints is practically negligible, so that loss of head about the curve may be considered as only'that produced bythe bend orcurve itself. This would be obviously true in a passageway having an integral wallsuchas is found, for example, in the cast intake manifold of an internal combustionenginea I My copending application, Serial No. 581,342,
  • Fig. 11 is a perspective view of the insert part of another modification. 7
  • 1 is a curved part and 2 a straight part of a conduit or pipe wherein flow is to be had from right to left, as indicated.- by the arrows.
  • 3 indicates-generally, means inserted within the straight part 2- of the pipe, just aheadof the bend 1 thereof, for the -purpose of imparting to a stream moving through said pipe, a twisting or angular motion.
  • the part 3 here shown comprises five fins orvanes 4, each radially disposed to divide the fiow into five equal passageways. As indicated, Fig. 1, each fin 4' at its upstream end is parallel to the general direction of 'flow through the straight pipe section.
  • Each fin is deformed to have increasing ang-ularity in -'a commonv direction from its upstream end, about the pipe center, so that each fin at its downstream end has maximum angularity.
  • the fins 4 may be of any suitable material considering that of the pipe and the nature of the liquid or gas to be passed therethrough.
  • the pipe may be of cast iron and the fins may be of sheet metal They may be welded, soldered or otherwise connected with each other and secured with the pipe.
  • a lining of vitreous enamel 5 providing a substantially frictionless surface may be employed and may serve to form the fillets indicated at 5, Fig. 2, whereby the fins are secured with the pipe sides.
  • the invention is particularly applicable to an inlet manifold, wherein extreme velocities of fiow are had with high frequency pulsations or alter- 7 nations. It willbe obvious that the pitch of the fins at their downstream end will cause'them to obstruct reverse flow, in the directionppposite that indicated by the arrows. fin arrangement shown in Figs. 1 and *2 is theoretically efficient, it is not as practical a one from the viewpoint of manufacture, as'are some of the modifications hereinafter referred to.
  • Fig. 3 shows'a pair of oppositely extending fins 6 formed as by a single piece of sheet metal diametrically disposed in the straight pipe section 2 and, of course, having pitch of increasing amount as in the form of Figs. 1 and 2.
  • Fillet members '7 of soft rubber or the like are here employed to position the diametrical partition member. 7
  • Fig. 4 shows an arrangement wherein three integral fins 8, disposed at 120", are provided from a single sheet of metal, the peripheral part 9 connecting two of the fins 8 and having spring characteristics tending to expand the parts against the pipe walls.
  • Fig. 5 shows a generally triangular arrangement wherein the fins 10 are non-radially disposed, and divide the passage into a central one of generally triangular section surrounded by three passages of lozenge-shaped section.
  • This form is preferably of spring metal so that it may be inserted in a position by fiexing the central parts of three fins inwardly toward each other, so that upon release, these parts will tend to straighten and thus expand the three points 11, at their extremities, against the pipe walls, the fins 10 having pitch, as before, to impart the desired twist to the stream.
  • Fig. 6 is similar to that of Fig. 5 except that only two fin members 12 are employed, of spring metal so that they will tend to open from each other and may thus be conveniently inserted into the pipe and when released, will secure themselves therein.
  • Fig. 7 is of S shape in section, and likewise of spring metal so that it will be selfsecuring, the metal tending to straighten.
  • Fig. 8 the section is cruciform, with opposed peripheral parts 13 adapted to grip the pipe walls.
  • Fig. 10 is shown a form dividing the pipe opening into six similar passages.
  • the insert comprising the fin parts will expand to grip the pipe sides.
  • Fig. 11 the form is that adapted to divide the pipe opening into five substantially equal passages, as was done in the form of Figs. 1 and 2, the insert of Fig. 11, however, being adapted to seat by expansion, as in the case of the insert of Fig. 10.
  • vane means located ahead of said way and constructed and arranged to impart, to a stream approaching said Way, such rotating motion that said stream will revolve substantially 180 during its progress along said Way.
  • vane means located in said approach and constructed and arranged to impart such rotating motion to a stream flowing therethrough, that said stream will have a half revolution of twist during its progress along said curved way.
  • vane means located ahead of said Way and constructed and arranged to gradually impart to'a stream approaching said way, such rotating motion that said stream will revolve substantially 180 during its progress along said way.
  • vane means located in said approach to impart rotating motion to a stream fiowing therethrough, said vane means being constructed and arranged to resiliently engage the sides of said approach for securement in the latter.
  • vane means located in said approach to impart rotating motion to a stream flowing therethrough, said vane means having peripherally located parts arranged to engage the side walls of said approach, and having resilient parts arranged to provide yieldable,

Description

Sept. 18, 1934. g, R, HI 'LEY 1,974,110
CURVED CONDUIT Filed Dec. 21, 1932 INVENTOR ATTORNEYS CURVED' CONDUIT, Frank R. Hig-ley, Cleveland Heights, Ohio Application December 21, 1932, Serial No. 648,263 1 9 clai (01. 137-112) This invention relates to improvements in the type of conduit having a curved way, that is, to a pipe device having a through passageway, the entrance to which is adapted to receive the flow from one direction and theconduit being adapted to change the direction of this fiow so that the conduit discharge opening, at the opposite end of the way, will discharge the flow in another direction.
An example is the ordinary elbow pipe fitting adapted to interconnect a pair of straight pipe lengths angularly related but in a common plane. Methods of pipe fitting, such as employing threaded and flanged joints, are rapidly being supplanted by weldedjoints wherein the inner pipe surface is substantially uninterrupted at its joints, and turbulence caused by joints is practically negligible, so that loss of head about the curve may be considered as only'that produced bythe bend orcurve itself. This would be obviously true in a passageway having an integral wallsuchas is found, for example, in the cast intake manifold of an internal combustionenginea I My copending application, Serial No. 581,342,
. filed December 16, 1931, illustrates and describes 'an arrangement for reducing the turbulence andv consequent loss of. head in'a curved conduit way,
wherein the absolute path of a unitofyclume in thestream along said wayis caused to be helical, with such angular advancement about the mean path of the way, as said mean path extends along the curve of said way, that the absolute paths of all units of volume are substantially The invention of this application comprises a modification of that of said copending applica-.
tion in that means are employed for the same purpose, but located in a straight pipe section ahead of the bend. The arrangement is thus one simpler and less expensive, as will appear, and one equally useful in many instances.
Generally, therefore, the objects of this invention are improvements over the disclosure of said copending application.
Further objects and advantages are in part obvious and in part will appear more in detail hereinafter and in the accompanying drawing in which Figs. 1 and 2 are side and end views,
respectively, of an embodiment of the invention,
practical -modific'ations; and Fig. 11 is a perspective view of the insert part of another modification. 7
With reference now to the drawing and particularly Figs. 1 and 2 thereof, 1 is a curved part and 2 a straight part of a conduit or pipe wherein flow is to be had from right to left, as indicated.- by the arrows. 3 indicates-generally, means inserted within the straight part 2- of the pipe, just aheadof the bend 1 thereof, for the -purpose of imparting to a stream moving through said pipe, a twisting or angular motion. The part 3 here shown comprises five fins orvanes 4, each radially disposed to divide the fiow into five equal passageways. As indicated, Fig. 1, each fin 4' at its upstream end is parallel to the general direction of 'flow through the straight pipe section. Each fin is deformed to have increasing ang-ularity in -'a commonv direction from its upstream end, about the pipe center, so that each fin at its downstream end has maximum angularity. Thus the mean path of fiow througheach of thefive passageways between fins'commences parallel with'the center line of the straight pipe section, but. moves thereabout as it advances, in a helical direction of increasing pitch until a maxi-' mum ratio of twist about-the center line, to advance therealong, is had, at the point of de-' parture from between thefins. The angle. of. departure is equal for all of the fins and consequently forall of the paths of flow therebetween, and is such that as the stream leaves the fins and progresses through the curve of the part 1 ofthe conduit, its rotational component of inertia will cause the stream as a whole to rotate about its center substantially 180 between entrance'into and departure from the con-.
dult curve.
This rotational amount will be desirable regardless of the amount of 'bendin the curved section, so that if thebend 1 were only 45 instead of as illustrated, the fins may be pitched'to have less angle of departure than that shown; whilezif the amount of bend in the elbow were greater than the 90 shown, the fins would have to be pitched to have a correspondingly greater angle of departure. In any case, the entrancev angle of the fins should ibe zero, or in other words, their upstream ends should lie in the general di-Z rection of the straight pipe part 2.
The fins 4 may be of any suitable material considering that of the pipe and the nature of the liquid or gas to be passed therethrough. Thus, as in an inlet manifold for an internal combustion engine, the pipe may be of cast iron and the fins may be of sheet metal They may be welded, soldered or otherwise connected with each other and secured with the pipe. In the case of an inlet manifold, a lining of vitreous enamel 5 providing a substantially frictionless surface may be employed and may serve to form the fillets indicated at 5, Fig. 2, whereby the fins are secured with the pipe sides.
The invention is particularly applicable to an inlet manifold, wherein extreme velocities of fiow are had with high frequency pulsations or alter- 7 nations. It willbe obvious that the pitch of the fins at their downstream end will cause'them to obstruct reverse flow, in the directionppposite that indicated by the arrows. fin arrangement shown in Figs. 1 and *2 is theoretically efficient, it is not as practical a one from the viewpoint of manufacture, as'are some of the modifications hereinafter referred to.
Fig. 3 shows'a pair of oppositely extending fins 6 formed as by a single piece of sheet metal diametrically disposed in the straight pipe section 2 and, of course, having pitch of increasing amount as in the form of Figs. 1 and 2. Fillet members '7 of soft rubber or the like are here employed to position the diametrical partition member. 7
Fig. 4 shows an arrangement wherein three integral fins 8, disposed at 120", are provided from a single sheet of metal, the peripheral part 9 connecting two of the fins 8 and having spring characteristics tending to expand the parts against the pipe walls.
Fig. 5 shows a generally triangular arrangement wherein the fins 10 are non-radially disposed, and divide the passage into a central one of generally triangular section surrounded by three passages of lozenge-shaped section. This form is preferably of spring metal so that it may be inserted in a position by fiexing the central parts of three fins inwardly toward each other, so that upon release, these parts will tend to straighten and thus expand the three points 11, at their extremities, against the pipe walls, the fins 10 having pitch, as before, to impart the desired twist to the stream.
The form of Fig. 6 is similar to that of Fig. 5 except that only two fin members 12 are employed, of spring metal so that they will tend to open from each other and may thus be conveniently inserted into the pipe and when released, will secure themselves therein.
The form of Fig. 7 is of S shape in section, and likewise of spring metal so that it will be selfsecuring, the metal tending to straighten.
In Fig. 8 the section is cruciform, with opposed peripheral parts 13 adapted to grip the pipe walls.
The form of Fig. 9 will be recognized as a modification of the form of Fig. 6.
In Fig. 10 is shown a form dividing the pipe opening into six similar passages. Here again the insert comprising the fin parts will expand to grip the pipe sides.
In Fig. 11, the form is that adapted to divide the pipe opening into five substantially equal passages, as was done in the form of Figs. 1 and 2, the insert of Fig. 11, however, being adapted to seat by expansion, as in the case of the insert of Fig. 10.
'located'ahead of said way, and constructed and arranged to impart, to a stream approaching said way, such rotating motion that said stream will revolve substantially 180 during its progress along said way.
2. In a, conduit having a curved way, vane means located ahead of said way and constructed and arranged to impart, to a stream approaching said Way, such rotating motion that said stream will revolve substantially 180 during its progress along said Way.
3.,In a conduit having a curved way and a straight approach thereto, means located in said approach and constructed and arranged to impart such rotating motion to a stream flowing therethrough, that said stream will have a half revolution of twist during its progress along said curved way.
4. In a conduit having a curved way and a straight approach thereto, vane means located in said approach and constructed and arranged to impart such rotating motion to a stream flowing therethrough, that said stream will have a half revolution of twist during its progress along said curved way.
5. In combination with a conduit having a curved way, vane means located ahead of said Way and constructed and arranged to gradually impart to'a stream approaching said way, such rotating motion that said stream will revolve substantially 180 during its progress along said way. W
'6. In combination with a conduit having a curved way, an approach thereto having vane means constructed and arranged to impart to a stream entering said way by said approach, such rotation about the center line of said way that said stream will revolve substantially 180 during its progress along said way.
7. In a conduit having a curved way and a straightapproach thereto, vane means located in said approach to impart rotating motion to a stream fiowing therethrough, said vane means being constructed and arranged to resiliently engage the sides of said approach for securement in the latter.
8. In a conduit having a curved Way and a' straight approach thereto, vane means located in said approach to impart rotating motion to a stream flowing therethrough, said vane means having peripherally located parts arranged to engage the side walls of said approach, and having resilient parts arranged to provide yieldable,
FRANK R. HIGLEY.
US648263A 1932-12-21 1932-12-21 Curved conduit Expired - Lifetime US1974110A (en)

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Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3266524A (en) * 1963-05-20 1966-08-16 William H Goettl Duct structure
US3273598A (en) * 1966-09-20 Goettl duct structure
DE2733943A1 (en) * 1976-08-02 1978-02-09 Quantor Corp FILM PROCESSING DEVICE
FR2474614A1 (en) * 1980-01-30 1981-07-31 Inst Francais Du Petrole METHOD AND DEVICE FOR REGULARIZING THE FLOW OF A DIPHASIC FLUID
EP0532697A1 (en) * 1990-06-06 1993-03-24 CHENG, Dah, Yu Laminar flow elbow system
WO1995025897A1 (en) * 1994-03-24 1995-09-28 Koch Engineering Company, Inc. Laminar flow elbow system
FR2767160A1 (en) * 1997-08-06 1999-02-12 Ksb Ag GUIDING DEVICE FOR PIPE ELBOWS
US5916134A (en) * 1997-09-10 1999-06-29 Industrial Technology Research Institute Catalytic converter provided with vortex generator
US5992465A (en) * 1996-08-02 1999-11-30 Jansen; Robert C. Flow system for pipes, pipe fittings, ducts and ducting elements
US20020179166A1 (en) * 2001-06-05 2002-12-05 Houston John Graeme Flow means
US20060124187A1 (en) * 2002-11-23 2006-06-15 Tayside Flow Technologies Limited Helical formation for a conduit
US20080308653A1 (en) * 2007-06-15 2008-12-18 Dah Yu Cheng Method and apparatus for balancing flow through fuel nozzles
US20100122531A1 (en) * 2008-11-19 2010-05-20 Ford Global Technologies, Llc Inlet system for an engine
US20100132937A1 (en) * 2008-11-06 2010-06-03 Tinker Donald W Laminar Flow Tool
US8272836B1 (en) 2008-01-25 2012-09-25 Lynx Product Group, LLC Pump suction assembly
DE102011100637A1 (en) * 2011-05-05 2012-11-08 Striko Verfahrenstechnik W. Strikfeldt & Koch Gmbh swirler
US20120304628A1 (en) * 2010-05-07 2012-12-06 Ford Global Technologies, Llc Exhaust system mixing device
US20130091830A1 (en) * 2011-10-18 2013-04-18 GM Global Technology Operations LLC Assembly for mixing liquid within gas flow
US20130192805A1 (en) * 2007-10-05 2013-08-01 The Boeing Company Twist Vane Counter-Parallel Flow Heat Exchanger Apparatus And Method
US20140116567A1 (en) * 2012-10-31 2014-05-01 Toyota Jidosha Kabushiki Kaisha Pipe with rib and method for manufacturing pipe with rib
US20150107563A1 (en) * 2012-07-11 2015-04-23 Kawasaki Jukogyo Kabushiki Kaisha Air intake duct of saddle-ridden vehicle
US20160032809A1 (en) * 2014-07-31 2016-02-04 Eberspächer Exhaust Technology GmbH & Co. KG Mixer and mixing device for an exhaust system
US9534525B2 (en) 2015-05-27 2017-01-03 Tenneco Automotive Operating Company Inc. Mixer assembly for exhaust aftertreatment system
US10188532B2 (en) 1998-12-29 2019-01-29 Vascular Flow Technologies Limited Blood-flow tubing
US10458446B1 (en) 2018-11-29 2019-10-29 Vortex Pipe Systems LLC Material flow amplifier
US11002301B1 (en) 2020-09-15 2021-05-11 Vortex Pipe Systems LLC Material flow modifier and apparatus comprising same
US11221028B1 (en) 2018-11-29 2022-01-11 Vortex Pipe Systems LLC Cyclonic flow-inducing pump
US11378110B1 (en) 2022-01-05 2022-07-05 Vortex Pipe Systems LLC Flexible fluid flow modifying device
LU102868B1 (en) * 2021-10-20 2023-04-20 Wilo Se double pump
US11739774B1 (en) 2023-01-30 2023-08-29 Vortex Pipe Systems LLC Flow modifying device with performance enhancing vane structure

Cited By (58)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273598A (en) * 1966-09-20 Goettl duct structure
US3266524A (en) * 1963-05-20 1966-08-16 William H Goettl Duct structure
DE2733943A1 (en) * 1976-08-02 1978-02-09 Quantor Corp FILM PROCESSING DEVICE
US4101919A (en) * 1976-08-02 1978-07-18 Quantor Corporation Film processing apparatus
FR2474614A1 (en) * 1980-01-30 1981-07-31 Inst Francais Du Petrole METHOD AND DEVICE FOR REGULARIZING THE FLOW OF A DIPHASIC FLUID
EP0034079B1 (en) * 1980-01-30 1983-07-06 Institut Français du Pétrole Method and device for stabilizing the flow of a two-phase fluid
EP0532697A1 (en) * 1990-06-06 1993-03-24 CHENG, Dah, Yu Laminar flow elbow system
US5197509A (en) * 1990-06-06 1993-03-30 Cheng Dah Y Laminar flow elbow system and method
EP0532697A4 (en) * 1990-06-06 1993-08-04 Dah Yu Cheng Laminar flow elbow system
US5323661A (en) * 1990-06-06 1994-06-28 Cheng Dah Y Laminar flow elbow system and method
WO1995025897A1 (en) * 1994-03-24 1995-09-28 Koch Engineering Company, Inc. Laminar flow elbow system
US5529084A (en) * 1994-03-24 1996-06-25 Koch Engineering Company, Inc. Laminar flow elbow system and method
US5992465A (en) * 1996-08-02 1999-11-30 Jansen; Robert C. Flow system for pipes, pipe fittings, ducts and ducting elements
FR2767160A1 (en) * 1997-08-06 1999-02-12 Ksb Ag GUIDING DEVICE FOR PIPE ELBOWS
US5916134A (en) * 1997-09-10 1999-06-29 Industrial Technology Research Institute Catalytic converter provided with vortex generator
US10188532B2 (en) 1998-12-29 2019-01-29 Vascular Flow Technologies Limited Blood-flow tubing
US20020179166A1 (en) * 2001-06-05 2002-12-05 Houston John Graeme Flow means
US6776194B2 (en) * 2001-06-05 2004-08-17 Tayside Flow Technologies Limited Flow means
US20060124187A1 (en) * 2002-11-23 2006-06-15 Tayside Flow Technologies Limited Helical formation for a conduit
US20080308653A1 (en) * 2007-06-15 2008-12-18 Dah Yu Cheng Method and apparatus for balancing flow through fuel nozzles
US9079203B2 (en) * 2007-06-15 2015-07-14 Cheng Power Systems, Inc. Method and apparatus for balancing flow through fuel nozzles
US9068780B2 (en) * 2007-10-05 2015-06-30 The Boeing Company Twist vane counter-parallel flow heat exchanger apparatus and method
US20130192805A1 (en) * 2007-10-05 2013-08-01 The Boeing Company Twist Vane Counter-Parallel Flow Heat Exchanger Apparatus And Method
US8272836B1 (en) 2008-01-25 2012-09-25 Lynx Product Group, LLC Pump suction assembly
US8281817B2 (en) * 2008-11-06 2012-10-09 Team Oil Tools, Lp Laminar flow tool
US20100132937A1 (en) * 2008-11-06 2010-06-03 Tinker Donald W Laminar Flow Tool
US8286428B2 (en) * 2008-11-19 2012-10-16 Ford Global Technologies Inlet system for an engine
US20100122531A1 (en) * 2008-11-19 2010-05-20 Ford Global Technologies, Llc Inlet system for an engine
US20120304628A1 (en) * 2010-05-07 2012-12-06 Ford Global Technologies, Llc Exhaust system mixing device
US8997460B2 (en) * 2010-05-07 2015-04-07 Ford Global Technologies, Llc Exhaust system mixing device
DE102011100637A1 (en) * 2011-05-05 2012-11-08 Striko Verfahrenstechnik W. Strikfeldt & Koch Gmbh swirler
US8826649B2 (en) * 2011-10-18 2014-09-09 GM Global Technology Operations LLC Assembly for mixing liquid within gas flow
US20130091830A1 (en) * 2011-10-18 2013-04-18 GM Global Technology Operations LLC Assembly for mixing liquid within gas flow
US20150107563A1 (en) * 2012-07-11 2015-04-23 Kawasaki Jukogyo Kabushiki Kaisha Air intake duct of saddle-ridden vehicle
US9638149B2 (en) 2012-07-11 2017-05-02 Kawasaki Jukogyo Kabushiki Kaisha Air intake duct of saddle-ridden vehicle
US9651005B2 (en) * 2012-07-11 2017-05-16 Kawasaki Jukogyo Kabushiki Kaisha Air intake duct of saddle-ridden vehicle
US9677516B2 (en) 2012-07-11 2017-06-13 Kawasaki Jukogyo Kabushiki Kaisha Saddle-ridden vehicle engine
US20140116567A1 (en) * 2012-10-31 2014-05-01 Toyota Jidosha Kabushiki Kaisha Pipe with rib and method for manufacturing pipe with rib
US9713840B2 (en) 2012-10-31 2017-07-25 Toyota Jidosha Kabushiki Kaisha Pipe with rib and method for manufacturing pipe with rib
US20160032809A1 (en) * 2014-07-31 2016-02-04 Eberspächer Exhaust Technology GmbH & Co. KG Mixer and mixing device for an exhaust system
US9790833B2 (en) * 2014-07-31 2017-10-17 Eberspächer Exhaust Technology GmbH & Co. KG Mixer and mixing device for an exhaust system
US9534525B2 (en) 2015-05-27 2017-01-03 Tenneco Automotive Operating Company Inc. Mixer assembly for exhaust aftertreatment system
US10890200B2 (en) 2018-11-29 2021-01-12 Vortex Pipe Systems LLC Clamshell material flow amplifier
US10683881B1 (en) 2018-11-29 2020-06-16 Vortex Pipe Systems LLC Material flow amplifier
US10458446B1 (en) 2018-11-29 2019-10-29 Vortex Pipe Systems LLC Material flow amplifier
US10895274B2 (en) 2018-11-29 2021-01-19 Vortex Pipe Systems LLC Material flow amplifier
US11221028B1 (en) 2018-11-29 2022-01-11 Vortex Pipe Systems LLC Cyclonic flow-inducing pump
US11319974B2 (en) 2018-11-29 2022-05-03 Vortex Pipe Systems LLC Clamshell material flow amplifier
US11391309B2 (en) 2018-11-29 2022-07-19 Vortex Pipe Systems LLC Material flow amplifier
US11002301B1 (en) 2020-09-15 2021-05-11 Vortex Pipe Systems LLC Material flow modifier and apparatus comprising same
US11976678B2 (en) 2020-09-15 2024-05-07 Vortex Pipe Systems LLC Material flow modifier and apparatus comprising same
US11624381B2 (en) 2020-09-15 2023-04-11 Vortex Pipe Systems LLC Material flow modifier and apparatus comprising same
LU102868B1 (en) * 2021-10-20 2023-04-20 Wilo Se double pump
EP4170177A1 (en) * 2021-10-20 2023-04-26 Wilo Se Double pump
US20230220858A1 (en) * 2022-01-05 2023-07-13 Vortex Pipe Systems LLC Flexible fluid flow modifying device
US11841037B2 (en) * 2022-01-05 2023-12-12 Vortex Pipe Systems, LLC Flexible fluid flow modifying device
US11378110B1 (en) 2022-01-05 2022-07-05 Vortex Pipe Systems LLC Flexible fluid flow modifying device
US11739774B1 (en) 2023-01-30 2023-08-29 Vortex Pipe Systems LLC Flow modifying device with performance enhancing vane structure

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