GB1376466A - Method of fabricating spirally wound duct-defining units - Google Patents

Method of fabricating spirally wound duct-defining units

Info

Publication number
GB1376466A
GB1376466A GB1859772A GB1859772A GB1376466A GB 1376466 A GB1376466 A GB 1376466A GB 1859772 A GB1859772 A GB 1859772A GB 1859772 A GB1859772 A GB 1859772A GB 1376466 A GB1376466 A GB 1376466A
Authority
GB
United Kingdom
Prior art keywords
strip
turns
wound
netting
spacer
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
Application number
GB1859772A
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.)
AGA AB
Original Assignee
AGA AB
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 AGA AB filed Critical AGA AB
Publication of GB1376466A publication Critical patent/GB1376466A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/04Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by spirally-wound plates or laminae
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00Making other particular articles
    • B21D53/02Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers
    • B21D53/027Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers by helically or spirally winding elongated elements

Landscapes

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

Abstract

1376466 Making spiral duct-defining units AGA AB and S KNOOS 21 April 1972 [23 April 1971] 18597/72 Heading B3A [Also in Division F4] A method of fabricating a spirally-wound duct-defining unit comprises simultaneously winding at least one strip (2), Fig. 1 (not shown), and at least one spacer element (3) such that the spacer element radially spaces the turns of the strip, securing the turns of the strip by passing elongate fixing elements, e.g. pins 9, Fig. 2, through respective sets of holes, which are radially aligned in the turns of the strip and the outermost holes are spaced about the circumference of the wound strip, each fixing element preventing movement of the strip turns in a plane perpendicular to the fixing element, and removing at least part of the spacer element from the space between some at least of the adjacent turns of the strip. Wires 4, 5, which comprise the spacer element, are wound together with a strip about a core between shields 6, 7, and holes are drilled through the coiled strip to accommodate the pins 9. When winding is completed, the shields 6, 7 are removed and the wires 3, 4 pulled out of the coil or they may be dissolved or melted out by heating. Two or more strips with their spacer elements may be wound simultaneously and alternate elements removed to form flow passages for heat exchange between two media, A, B, Fig. 7. The medium B is supplied through a pipe 29 on either side of the unit and the pipes are secured by soldering, gluing or by dipping in a metal bath. A plurality of units (16)-(20), Fig. 5 (not shown), may be located in axial relationship for use in refrigerating plant or as a thermal regenerator for a gas engine. A liquid fuel burner, Fig. 11, is fabricated by simultaneously winding two strips together with axially spaced spacer elements, which are removed from between alternate turns to form axially directed ducts 38, through which air is passed, and ducts 40 containing metal netting 41 for pumping the fuel by capillary action. In alternative forms of burners, capillary pumping takes place without the use of wire netting, or all the spacer elements are removed and netting is placed between alternate turns of the unit or the netting is located upstream, in the direction of fuel flow, of the spacers, Figs. 13-15 respectively (not shown).
GB1859772A 1971-04-23 1972-04-21 Method of fabricating spirally wound duct-defining units Expired GB1376466A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE529871A SE353388B (en) 1971-04-23 1971-04-23

Publications (1)

Publication Number Publication Date
GB1376466A true GB1376466A (en) 1974-12-04

Family

ID=20266163

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1859772A Expired GB1376466A (en) 1971-04-23 1972-04-21 Method of fabricating spirally wound duct-defining units

Country Status (5)

Country Link
JP (1) JPS577358B2 (en)
DE (1) DE2220012C3 (en)
GB (1) GB1376466A (en)
NL (1) NL171489C (en)
SE (1) SE353388B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5797449A (en) * 1995-07-12 1998-08-25 Rolls-Royce Plc Heat exchanger
US6233824B1 (en) * 1999-10-08 2001-05-22 Carrier Corporation Cylindrical heat exchanger
RU170207U1 (en) * 2016-08-17 2017-04-18 Общество с ограниченной ответственностью "Прогресс" HEAT EXCHANGE ELEMENT

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5840120B2 (en) * 1977-01-25 1983-09-03 日立造船株式会社 Fin tube manufacturing method
JPH0458171U (en) * 1990-09-25 1992-05-19

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5797449A (en) * 1995-07-12 1998-08-25 Rolls-Royce Plc Heat exchanger
US6233824B1 (en) * 1999-10-08 2001-05-22 Carrier Corporation Cylindrical heat exchanger
RU170207U1 (en) * 2016-08-17 2017-04-18 Общество с ограниченной ответственностью "Прогресс" HEAT EXCHANGE ELEMENT

Also Published As

Publication number Publication date
NL171489C (en) 1983-04-05
JPS4849060A (en) 1973-07-11
DE2220012C3 (en) 1978-05-24
JPS577358B2 (en) 1982-02-10
NL7205428A (en) 1972-10-25
DE2220012A1 (en) 1972-11-09
SE353388B (en) 1973-01-29
NL171489B (en) 1982-11-01
DE2220012B2 (en) 1977-10-13

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee