US1974110A - Curved conduit - Google Patents
Curved conduit Download PDFInfo
- 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
- Authority
- US
- United States
- Prior art keywords
- way
- pipe
- fins
- stream
- conduit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000002184 metal Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 238000011144 upstream manufacturing Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 239000000037 vitreous enamel Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
- F15D1/00—Influencing flow of fluids
- F15D1/02—Influencing flow of fluids in pipes or conduits
- F15D1/04—Arrangements of guide vanes in pipe elbows or duct bends; Construction of pipe conduit elements for elbows with respect to flow, e.g. for reducing losses of 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,
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US648263A US1974110A (en) | 1932-12-21 | 1932-12-21 | Curved conduit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US648263A US1974110A (en) | 1932-12-21 | 1932-12-21 | Curved conduit |
Publications (1)
Publication Number | Publication Date |
---|---|
US1974110A true US1974110A (en) | 1934-09-18 |
Family
ID=24600090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US648263A Expired - Lifetime US1974110A (en) | 1932-12-21 | 1932-12-21 | Curved conduit |
Country Status (1)
Country | Link |
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US (1) | US1974110A (en) |
Cited By (31)
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 |
US20220349430A1 (en) * | 2019-09-19 | 2022-11-03 | Fmc Technologies, Inc. | Flow bore guide vane insert |
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 |
-
1932
- 1932-12-21 US US648263A patent/US1974110A/en not_active Expired - Lifetime
Cited By (62)
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 |
US10458446B1 (en) | 2018-11-29 | 2019-10-29 | Vortex Pipe Systems LLC | Material flow amplifier |
US10683881B1 (en) | 2018-11-29 | 2020-06-16 | Vortex Pipe Systems LLC | Material flow amplifier |
US10890200B2 (en) | 2018-11-29 | 2021-01-12 | Vortex Pipe Systems LLC | Clamshell material flow amplifier |
US10895274B2 (en) | 2018-11-29 | 2021-01-19 | Vortex Pipe Systems LLC | Material flow amplifier |
US12006957B2 (en) | 2018-11-29 | 2024-06-11 | 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 |
US12012980B2 (en) | 2018-11-29 | 2024-06-18 | Vortex Pipe Systems LLC | Cyclonic flow-inducing pump |
US12196235B2 (en) * | 2019-09-19 | 2025-01-14 | Fmc Technologies, Inc. | Flow bore guide vane insert |
US20220349430A1 (en) * | 2019-09-19 | 2022-11-03 | Fmc Technologies, Inc. | Flow bore guide vane insert |
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 |
EP4170177A1 (en) * | 2021-10-20 | 2023-04-26 | Wilo Se | Double pump |
LU102868B1 (en) * | 2021-10-20 | 2023-04-20 | 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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