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GB2044430A - Turbulators - Google Patents

Turbulators Download PDF

Info

Publication number
GB2044430A
GB2044430A GB8004654A GB8004654A GB2044430A GB 2044430 A GB2044430 A GB 2044430A GB 8004654 A GB8004654 A GB 8004654A GB 8004654 A GB8004654 A GB 8004654A GB 2044430 A GB2044430 A GB 2044430A
Authority
GB
United Kingdom
Prior art keywords
coils
turbulator
loops
core
length
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.)
Withdrawn
Application number
GB8004654A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MIDLAND WIRE CORDAGE CO Ltd
Original Assignee
MIDLAND WIRE CORDAGE CO Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MIDLAND WIRE CORDAGE CO Ltd filed Critical MIDLAND WIRE CORDAGE CO Ltd
Priority to GB8004654A priority Critical patent/GB2044430A/en
Publication of GB2044430A publication Critical patent/GB2044430A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F13/06Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media
    • F28F13/12Arrangements for modifying heat-transfer, e.g. increasing, decreasing by affecting the pattern of flow of the heat-exchange media by creating turbulence, e.g. by stirring, by increasing the force of circulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

A turbulator for insertion in a heat exchange tube to increase the turbulence of fluid flowing through the tube comprises a twisted wire member which has loop or coiled portions, extending along the length of the tube axis, of high density alternating with portions of low or nil density. <IMAGE>

Description

SPECIFICATION Turbulators This invention relates to turbulators, which are inserts for location in tubes forming flow passages for fluids (and that term is used herein to mean liquids, air, vapours, gases and mixtures and which are primarily intended -- as the name suggests for creating turbulence so as, for example, improve heat exchange between the fluid and the tube wall, or promote mixing in the fluid.
In accordance with the invention, a turbulator comprises an elongate member provided along its length with wire or like loops having the function of creating turbulence in fluid flow past the loops, characterised in that the loops are provided along portions which alternate along the length of the member with interposed portions where the loops are at least of a different density.
The density may alternate between a high value and a nil value, or in other words, a looped portion may alternate with a portion not provided with loops; alternatively the density may alternate between high and low values, as by cyclically increasing and decreasing the number of loops per unit length along the member.
The loops may be effective to improve heat exchange in two ways namely by creating turbulence so as to improve heat exchange between the fluid and tube wall or by heat transfer between the loops and the tube wall. For the latter purpose the turbulators may be bonded to the tubes, or an interference fit to ensure thermal conductivity. In all cases the heat exchange may be to or from the fluid.
In a first embodiment of the invention, a turbulator is made by assembling a pair of heavy gauge wires in parallel relationship, and disposing a series of regularly spaced helically wound coils of lighter gauge wire so that they are threaded by one of the heavy gauge wires but not the other.
This is shown in Figure 1. The two heavy gauge wires are then twisted together and this displaces the successive convolutions of the helically wound coils so that the convolutions spiral around the twisted core, the number of convolutions per unit length depending upon the parameters of the original coils and the degree of twisting. Figure 2 shows this assembled in a flow tube.
Instead of using separate coils which are individually spaced along the core wires before the twisting step, all of the helically wound coils may be made integral and unitary, each coiled portion being separated by a non-coiled portion of material of appropriate length as shown in Figure 3 to create the desired gap between the successive coils, and after the twisting step, the straight portion between successive coils will be twisted with the core.
In another embodiment, the space between successive ones of the helical coils is occupied by an additional helical coil which is not displaced by the core twisting step and hence does not go to the spirally located convolution condition when the core is twisted. This is shown in Figure 4 and may be done by arranging for both of the cores to be threaded through the additional coils in the assembly operation prior to the twisting operation.
The additional coils may be provided as an integral part of a single component, which is to provide the coils which are to be twisted with the core and the coils which are not to be twisted with the core alternately along its length to produce the arrangement of Figure 5 or the two sets of coils may be made separately as in Figure 6 leading to the arrangement of Figure 7. Further, the coils may be of different diameters so that those which are to be twisted with the core form a spirally wound bundle of convolutions having an overall diameter which is generally the same as that of the coils which are not to be twisted; the latter is also shown in Figure 8.
One particular version of the arrangement discussed in the preceding paragraph is where each of the coils which is not to be twisted with the core has only a single end effectively anchored to the core, and the diameter may be such in relation to the heat exchanger or other tube in which the turbulator is to be used that upon insertion, there is a slight interference fit with the untwisted coils so that they elongate during the insertion opertion as also shown in Figure 8. In this case it will be appreciated that the length of the untwisted coils prior to assembly into the heat exchange or like tube will be less than the gap between adjacent ones of the coils which are to be twisted with the core.
In another embodiment, the-untwisted helical coils which provide the low density turbulator effect as described above are used without the twisted and spirally located helical coils, and the variation in density is achieved by the spacing of the helical coils along individual convolutions as in Figure 9, thus enabling a single helical coil to be assembled to a core to provide the turbulator of the invention. The coil may be fixed to the core at one or both ends or at a series of spaced intervals along the length of the parts.
Instead of using wires for the core or for the coil or coils, strip material or other filamentary material may be used. Baffles may be provided, for example, made of metal pressings, which may be fixed to the core for example at each end and to act as spacers so as to locate the core on the axis of the tube in which the turbulator is to be located.
Additional baffles may be located between successive coils as shown in Figure 10 and Figure 14, and may take the form of disc-like pressings with apertures therein, or wire rings, which can be of smaller diameter than the tube bore. The baffles may be fixed in place or e.g. free to rotate so as to promote turbulence with less pressure drop.
Figures 11 and 12 are sections on the line 11-11 of Figure 10 showing two alternative designs of baffle, and Figures 1 5-1 8 show other forms of baffle.
The coils may be made of a plurality of wires, strips or other filaments which are collectively coiled, and during a twisting operation with the core respective coils will tend to separate from one another, thus creating a greater number of flow passages through the turbulator. The wire or other material may be crimped to a non-linear condition prior to forming into the coils or like, or can be coiled to a smaller diameter before being formed into coiled coils of large diameter.
Particularly (but not exclusively) when the fluid is viscous, a knitted wire stocking or sleeve may be used to line the tube as in Figure 1 3 with the turbulator located in the sleeve and serving the additional function of holding the sleeve against the tube wall. This may prevent the formation of laminar layers of the fluid Qn the tube wall and hence improve heat transfer further.

Claims (4)

1. A turbulator comprising an elongate member provided along its length with wire or like loops having the function of creating turbulence in fluid flow past the loops, characterised in that the loops are provided along portions which alternate along the length of the member with interposed portions where the loops are at least of a different density.
2. A turbulator as claimed in Claim 1 wherein the density alternates between a high value and a nil value.
3. A turbulator as claimed in Claim 1 wherein the density alternates between a high and low values.
4. A turbulator substantially as described with reference to any of the Figures of the accompanying drawings.
GB8004654A 1979-02-24 1980-02-12 Turbulators Withdrawn GB2044430A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8004654A GB2044430A (en) 1979-02-24 1980-02-12 Turbulators

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7906618 1979-02-24
GB8004654A GB2044430A (en) 1979-02-24 1980-02-12 Turbulators

Publications (1)

Publication Number Publication Date
GB2044430A true GB2044430A (en) 1980-10-15

Family

ID=26270692

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8004654A Withdrawn GB2044430A (en) 1979-02-24 1980-02-12 Turbulators

Country Status (1)

Country Link
GB (1) GB2044430A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0061154A2 (en) * 1981-03-20 1982-09-29 Cal Gavin Limited Insert for placement in a tube and method for its manufacturing
US4818842A (en) * 1986-08-22 1989-04-04 Walty Robert J Diesel fuel heater
DE29709073U1 (en) * 1997-05-23 1997-07-17 Behr GmbH & Co., 70469 Stuttgart Heat exchanger
US6119769A (en) * 1998-08-05 2000-09-19 Visteon Global Technologies, Inc. Heat transfer device
US6732788B2 (en) * 2002-08-08 2004-05-11 The United States Of America As Represented By The Secretary Of The Navy Vorticity generator for improving heat exchanger efficiency
US6997246B2 (en) * 2001-06-25 2006-02-14 Delphi Technologies, Inc. Laminar flow optional liquid cooler
WO2009075958A1 (en) * 2007-12-11 2009-06-18 Praxair Technology, Inc. Oxygen separation element and method
DE102009056274A1 (en) * 2009-12-01 2011-06-09 Benteler Automobiltechnik Gmbh heat exchangers
US20160013526A1 (en) * 2014-07-11 2016-01-14 Denso Corporation Battery pack

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0061154A2 (en) * 1981-03-20 1982-09-29 Cal Gavin Limited Insert for placement in a tube and method for its manufacturing
EP0061154A3 (en) * 1981-03-20 1983-05-18 Cal Gavin Limited Insert for placement in a vessel
US4818842A (en) * 1986-08-22 1989-04-04 Walty Robert J Diesel fuel heater
DE29709073U1 (en) * 1997-05-23 1997-07-17 Behr GmbH & Co., 70469 Stuttgart Heat exchanger
US6119769A (en) * 1998-08-05 2000-09-19 Visteon Global Technologies, Inc. Heat transfer device
US6997246B2 (en) * 2001-06-25 2006-02-14 Delphi Technologies, Inc. Laminar flow optional liquid cooler
US6732788B2 (en) * 2002-08-08 2004-05-11 The United States Of America As Represented By The Secretary Of The Navy Vorticity generator for improving heat exchanger efficiency
WO2009075958A1 (en) * 2007-12-11 2009-06-18 Praxair Technology, Inc. Oxygen separation element and method
DE102009056274A1 (en) * 2009-12-01 2011-06-09 Benteler Automobiltechnik Gmbh heat exchangers
US20160013526A1 (en) * 2014-07-11 2016-01-14 Denso Corporation Battery pack
US10374269B2 (en) * 2014-07-11 2019-08-06 Denso Corporation Battery pack

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)