GB2308181A - Heat exchange elements - Google Patents

Heat exchange elements Download PDF

Info

Publication number
GB2308181A
GB2308181A GB9625689A GB9625689A GB2308181A GB 2308181 A GB2308181 A GB 2308181A GB 9625689 A GB9625689 A GB 9625689A GB 9625689 A GB9625689 A GB 9625689A GB 2308181 A GB2308181 A GB 2308181A
Authority
GB
United Kingdom
Prior art keywords
plate
fluid
heat transfer
channels
indentations
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.)
Granted
Application number
GB9625689A
Other versions
GB9625689D0 (en
GB2308181B (en
Inventor
Martin Johns
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.)
LLOYD PETA
Original Assignee
LLOYD PETA
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 LLOYD PETA filed Critical LLOYD PETA
Publication of GB9625689D0 publication Critical patent/GB9625689D0/en
Publication of GB2308181A publication Critical patent/GB2308181A/en
Application granted granted Critical
Publication of GB2308181B publication Critical patent/GB2308181B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24DDOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS; DOMESTIC HOT-WATER SUPPLY SYSTEMS; ELEMENTS OR COMPONENTS THEREFOR
    • F24D5/00Hot-air central heating systems; Exhaust gas central heating systems
    • F24D5/06Hot-air central heating systems; Exhaust gas central heating systems operating without discharge of hot air into the space or area to be heated
    • F24D5/10Hot-air central heating systems; Exhaust gas central heating systems operating without discharge of hot air into the space or area to be heated with hot air led through heat-exchange ducts in the walls, floor or ceiling

Description

DESCRIPTION HEAT EXCHAN ELStiENrS This invention relates to heat exchanger plates for gas/solid valve regenerative application and to their assembly in the floor constructions of buildings to construct aerdecks. The plates are of corrugated or folded configuration, forming a multitude of separated longitudinal channels which afford direct contact of a heat transfer medium contained within them with the floor slab, and indirect contact with any contiguous floor screed laid above the plate.
Aerdecks are proposals intended to be integrally part of the building and of its thermal conditioning. For aerdecks the transport fluid is air which is made to pass over the fabric of the building, for example the concrete of the floors. Other massive constructional elements may alternatively be employed, eg. walls.
Previous designs of aerdeck systems have envisaged interconnected air pathways across the area of a floor slab, formed either of linked matrix sheet components or of individual domes and connectors. For these the air in the system is in direct contact with the supporting floor slab. The elements forming the air pathways may also be used as permanent shuttering for a floor screed, which then performs as an indirect contact1 second regenerative heat sink. The fluid is valved and is made to periodically flow through the air system, rejecting thermal energy to or retrieving it from contiguous or thermally connected sinks.
It is the aim of the current invention to improve the heat transfer-pressure loss performance of aerdecks through the configuration of the element used, while presenting a simple, cost effective means of its realisation. This plate form of element may also be of application to fluid/solid single plate valve regenerative heat exchangers in general, and to recuperative exchangers, both using alternative fluids.
Figure 1 shows a form of plate of equal trapezoidal profiled configuration.
Figure 2 shows a form of plate of equal trapezoidal contoured configuration.
Figure 3 shows a form of indentingimoulding of asymmetrical, aerofoil configuration.
Figure 4 shows a profiled plate assembled in an aerdeck application.
Figure 5 shows a contoured plate assembled in an aerodeck application.
The present invention is for aerdeck applications, where it is proposed that the plates that form the air paths be of a form that defines linear isolated channels, with no interconnection. These may be of any geometry, typically formed by vacuum, folding or rolling. The figures given utilise an equal trapezoidal configuration for example only. This may be changed to other preferred geometries, to increase the air channel volume and the air contact area, and to decrease the downstand rib section, or to suit other criteria.
At its simplest, the cross-section of this configuration of plate may be characterised as shown in fig. 1, and is constant at all points along the length of the profile.
The configuration may be developed by one or more surfaces of the plate being indented, as characterised in fig. 2. Such indentations may be continuous or intermittent, have surfaces transverse or at an angle to the direction of air flow, and be of various extent toward or away from the central plane of the plate.
This may be further developed by the incorporation of indentations of an asymmetrical form with dissimilar leading and trailing surfaces configurations and a point of inflexion, as characterised in fig. 3. These forms are termed aerofoil configurations and when used in directed fluid flow, as indicated F fig. 3, promote separation of the boundary layer. These configurations and flow arrangements produce aerofoil effects, where such effects are realised not at the fixed solid element, but in the fluid stream.
Plates with constant cross section are referred to as 'profiled'. Plates with indentations or mouldings of any form are referred to as 'contoured'.
Figure 4 shows a first embodiment of the invention in the form of a regular trapezoidal profiled plate as fig. 1, in an aerdeck construction (P), with a floor screed over (S1), where this floor screed is optional. When such a profiled sheet is in contact with a plane or approximately plane surface (S2) a plurality of continuous, unconnected channels (A) are formed which may be occupied by the fluid of the system, and within which it may be made to flow. The channels present regenerative heat transfer boundaries. Flow resistance and pressure loss is low.
Figure 5 shows a second embodiment of the invention in the form of a regular trapezoidal contoured plate as fig. 2, in an aerdeck construction (P), with an optional floor screed (S1) over. Similar to embodiment 1, when such a contoured sheet is in contact with a plane or approximately plane surface (S2) a plurality of continuous, unconnected channels (A) are formed which may be occupied by the fluid of the system, and within which it may be made to flow. For a heat transfer fluid moving between the sheet and the surface, the boundary formed by the contoured sheet shown presents indentations into the channel (ridge indentations shown as example), intruding intermittently into the enclosed spaces, and affecting flow type and pressure. The indentations may be shaped and spaced to promote disruption of the boundary layer due to circulation or turbulence of the fluid.Fluid mixing is induced, reducing the fluid temperature profile and increasing the rate of any convective heat transfer. The configuration of plate is referred to as an aerodeck form and the construction as an aerodeck system.
This may be further developed by asymmetrically moulding the indentations to form aerofoil configurations, as detailed above and shown in fig. 3, and co-orientating the indentation and fluid flow directions.
The indentations will enhance convective heat transfer at the regenerative heat transfer boundaries of the passages. This can be optimised with respect to consequential increase of pressure loss by the selection of indentation geometry and configuration with regard to the properties of the heat transfer fluid.
The configuration of plates of the invention may be manufactured in a number of materials by vacuum forming, and by traditional rolling and pressing methods.

Claims (3)

CWMS
1 / A heat exchanger plate for gas/solid valve regenerative application in the aerdecks of buildings, of corrugated or folded configuration, forming a multitude of separated longitudinal channels affording direct contact of a heat transfer medium contained within them with the floor slab, and indirect contact with any contiguous floor screed laid above the plate.
2 / A plate according to Claim 1 In which some percentage of the area of the surfaces are deformed or moulded but not punched through, to produce continuous or isolated indentations of the channel surface of one or various symmetrical or irregular geometries, of various surface area extents and toward or away from the central plane of the plate, producing a contoured plate which modifies the flow pattern of a heat transfer fluid when it is flowing through the channels so formed.
3 I A plate according to Claim 2 in which one or more of the deformations or mouldings include a surface asymmetrical or aerofoil in form which is used with some component of the principal direction of fluid flow in the direction of orientation of the aerofoil indentations.
4 / Jointing, blanking, and manifold components to join to the elements or components of the invention.
5 / A heat transfer element or component substantially as described herein or as shown in Figures 1-5 of the accompanying drawings.
3 / A plate according to Claim 2 in which one or more of the deformations or mouldings include a surface asymmetrical or aerofoil in form which is used with some component of the direction of fluid flow in the direction of orientation of the aerofoil indentations.
4 / Jointing, blanking, and manifold components to join to the elements or components of the invention.
5 I A heat transfer element or component substantially as described herein or as shown in Figures 1-5 of the accompanying drawings.
Amendments to the claims have been filed as follows II A heat exchanger plate for fluid/solid valve regenerator application in the aerdecks of buildings or similar situations, of corrugated or folded configuration,which when located on a surface form a multitude of separated channels affording direct contact of a heat transfer medium contained within them with a primary heat sink eg. floor slab, and indirect contact with any contiguous secondary heat sink eg. floor screed laid above the plate, and which by the physical enclosure of the channel, constrain the flow of any fluid within it to principally the longitudinal axis of the corrugation.
2 / A plate according to Claim 1 in which some percentage of the area of the surfaces are formed, deformed or moulded but not punched through, to produce continuous or isolated indentations of the channel surface of one or various symmetrical or irregular geometries, of various surface area extents and toward or away from the central plane of the plate, producing a contoured plate which modifies the flow pattern of a heat transfer fluid when it is flowing through the channels so formed, imparting fluid motion contrary to the longitudinal axis of these channels.
GB9625689A 1995-12-12 1996-12-11 Heat exchange elements Expired - Fee Related GB2308181B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9525351.4A GB9525351D0 (en) 1995-12-12 1995-12-12 Heat exchange elements

Publications (3)

Publication Number Publication Date
GB9625689D0 GB9625689D0 (en) 1997-01-29
GB2308181A true GB2308181A (en) 1997-06-18
GB2308181B GB2308181B (en) 2000-05-17

Family

ID=10785274

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9525351.4A Pending GB9525351D0 (en) 1995-12-12 1995-12-12 Heat exchange elements
GB9625689A Expired - Fee Related GB2308181B (en) 1995-12-12 1996-12-11 Heat exchange elements

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB9525351.4A Pending GB9525351D0 (en) 1995-12-12 1995-12-12 Heat exchange elements

Country Status (1)

Country Link
GB (2) GB9525351D0 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2361529A (en) * 2000-02-11 2001-10-24 Philip Andrew Kennedy Heat transfer tile
GB2383408A (en) * 2001-12-13 2003-06-25 Rmjm Ltd Heat store for controlling air temperature

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1439674A (en) * 1973-11-24 1976-06-16 Central Electr Generat Board Matrix for regenerative heat exchangers
GB1566619A (en) * 1976-04-15 1980-05-08 Rothemuehle Brandt Kritzler Heat exchange element
US4594826A (en) * 1984-06-22 1986-06-17 H. H. Robertson Company Field-assembled raceway forming member
GB2296086A (en) * 1994-11-15 1996-06-19 Brian Warwicker Climate control for a building

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1439674A (en) * 1973-11-24 1976-06-16 Central Electr Generat Board Matrix for regenerative heat exchangers
GB1566619A (en) * 1976-04-15 1980-05-08 Rothemuehle Brandt Kritzler Heat exchange element
US4594826A (en) * 1984-06-22 1986-06-17 H. H. Robertson Company Field-assembled raceway forming member
GB2296086A (en) * 1994-11-15 1996-06-19 Brian Warwicker Climate control for a building

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2361529A (en) * 2000-02-11 2001-10-24 Philip Andrew Kennedy Heat transfer tile
GB2361529B (en) * 2000-02-11 2003-08-20 Philip Andrew Kennedy Heat transfer tile for use in a room ceiling, wall or floor
GB2383408A (en) * 2001-12-13 2003-06-25 Rmjm Ltd Heat store for controlling air temperature

Also Published As

Publication number Publication date
GB9525351D0 (en) 1996-02-14
GB9625689D0 (en) 1997-01-29
GB2308181B (en) 2000-05-17

Similar Documents

Publication Publication Date Title
CA2050281C (en) Heat exchangers
US20100012303A1 (en) Hollow plate heat exchangers
US8376036B2 (en) Air to air heat exchanger
EP1653185B1 (en) Heat exchanger
KR100938802B1 (en) Heat exchanger having micro-channels
US4705105A (en) Locally inverted fin for an air conditioner
US6715740B2 (en) Fill packs for use in heat and mass transfer devices
JPH11287580A (en) Heat exchanger
EP0828131A2 (en) Opposed flow heat exchanger
JPS5926237B2 (en) Heat exchanger
US4789027A (en) Ribbed heat exchanger
EP1361406A2 (en) Heat exchanger
CN110849197B (en) Inner fin of heat exchanger
GB2308181A (en) Heat exchange elements
CA2214255C (en) Heat exchanger turbulizers with interrupted convolutions
JPS58205094A (en) Heat exchange element
EP1680638B1 (en) Heat exchanger for ventilator
CZ179797A3 (en) Panel-like heating body
JPH02634B2 (en)
US20230304742A1 (en) Channel heat exchanger
EP0097612B1 (en) Heat exchanger
JP2690272B2 (en) Heat exchange element
SU1666913A1 (en) Heat exchange surface
JPS60226696A (en) Finned heat transfer pipe and manufacture thereof
CZ2007679A3 (en) Countercurrent recuperative heat-exchange apparatus

Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20071211