GB1098080A - Heat exchangers - Google Patents

Heat exchangers

Info

Publication number
GB1098080A
GB1098080A GB11003/66A GB1100366A GB1098080A GB 1098080 A GB1098080 A GB 1098080A GB 11003/66 A GB11003/66 A GB 11003/66A GB 1100366 A GB1100366 A GB 1100366A GB 1098080 A GB1098080 A GB 1098080A
Authority
GB
United Kingdom
Prior art keywords
members
heat
combustion
air
wall
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
GB11003/66A
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.)
Thermo Fisher Scientific Inc
Original Assignee
Thermo Electron Engineering Corp
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 Thermo Electron Engineering Corp filed Critical Thermo Electron Engineering Corp
Publication of GB1098080A publication Critical patent/GB1098080A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J45/00Discharge tubes functioning as thermionic generators
    • 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
    • F28D9/0012Heat-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 apparatus having an annular form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F9/00Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
    • F28F9/24Arrangements for promoting turbulent flow of heat-exchange media, e.g. by plates

Abstract

1,098,080. Tubular heat exchangers. THERMO ELECTRON ENGINEERING CORPORATION. March 14, 1966 [March 29, 1965], No. 11003/66. Heading F4S. A heat exchanger comprises a stack of members M each of which is formed from a stepped tubular body, the narrowest end being closed by a plate 51, and has disposed at two levels around its periphery a plurality of apertures 39, 48, said members M being designed so that on stacking, two sinuous flow paths F 1 and F 2 , separated by a common heat transfer wall S, are produced. Terminal members M<SP>1</SP>, M<SP>11</SP> and M<SP>111</SP> are formed by removing a part of the basic member M, whereas areas of contact 43, 44 of adjacent members are suitably shaped and ground so that the resultant dry joint 45 is fluid tight. The heat exchange fluids may be liquid or gaseous and the elements of the heat exchanger may be made of refractory ceramic materials, e.g. silicon carbide, or from ferrous or non-ferrous metal or alloy. In the form shown in Fig. 1 combustion gases from a combustion chamber 10 supplying heat to a thermionic emitter 11 are used in the heat exchanger to pre-heat combustion air. The air is supplied through duct 55 and tubes, by virtue of apertures 39, the sinusoidal path F 1 and is thus forced to flow towards and away from the wall S. On entering, through apertures 23, the combustion chamber 10, the air is mixed with fuel, supplied by ducts 14, and the resultant hot combustion products impinge upon a plurality of thermionic emitters 11 before entering duct 13. From said duct 13 the gases enter the exchanger through apertures 58 and again are forced to flow toward and away from wall S, thus taking a similar sinusoidal path F 2 . Air entering through duct 55 is thus heated by combustion products before being used itself for combustion. The nature of the material from which members M are constructed is determined by the conditions under which the exchanger is used, with the wall S being made as thin as possible. In an alternate embodiment, shown in Fig. 4, the exchanger is made from a plurality of concentric cylinders 88, S<SP>1</SP> extending between upper and lower manifolds 110 and 96 resp. and having disposed between them members 91 which connect oppositely extending flanges 93 and 94, each of said members 91 having an aperture 92. Air for heating supplied to the lower manifold 96 takes any one of the sinusoidal flow paths F 4 , F 6 , F 8 or F 10 with hot combustion gases, supplied to the upper manifold, taking the remaining sinusoidal paths F 5 , F 7 , F 9 or F 11 , the walls through which exchange takes place being denoted S<SP>1</SP>. As above the gases are caused to flow towards and away from the wall S<SP>1</SP> by virture of the arrangement and nature of the individual members 91.
GB11003/66A 1965-03-29 1966-03-14 Heat exchangers Expired GB1098080A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US446476A US3416011A (en) 1965-03-29 1965-03-29 Thermionic converter heat exchangers

Publications (1)

Publication Number Publication Date
GB1098080A true GB1098080A (en) 1968-01-03

Family

ID=23772732

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11003/66A Expired GB1098080A (en) 1965-03-29 1966-03-14 Heat exchangers

Country Status (3)

Country Link
US (1) US3416011A (en)
DE (1) DE1501657B1 (en)
GB (1) GB1098080A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2360085A (en) * 2000-03-09 2001-09-12 Centrax Ltd Annular heat exchanger with concentric cells for use in gas turbine engine

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1380003A (en) * 1971-07-23 1975-01-08 Thermo Electron Corp Jet impingement heat exchanger
US3804159A (en) * 1972-06-13 1974-04-16 Thermo Electron Corp Jet impingement fin coil
US3908628A (en) * 1973-10-16 1975-09-30 Thermo Electron Corp Jet impingement recuperator
US5228513A (en) * 1991-05-03 1993-07-20 Indugas, Inc. Convective heat transfer by cascading jet impingement
US6675880B2 (en) 1996-03-29 2004-01-13 Mitsui Engineering And Shipbuilding Company Limited Air heater for recovering a heat of exhaust gas
US6378605B1 (en) 1999-12-02 2002-04-30 Midwest Research Institute Heat exchanger with transpired, highly porous fins
WO2008048493A2 (en) * 2006-10-13 2008-04-24 Nuventix, Inc. Thermal management of very small form factor projectors with synthetic jets
US20200294779A1 (en) * 2019-03-12 2020-09-17 Modern Electron, LLC Combined heating and power modules and devices

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE443349C (en) * 1927-04-26 Ewald Luetschen Heat exchange device
US1275366A (en) * 1915-07-21 1918-08-13 John E Bell Water-tube boiler.
US1736906A (en) * 1927-07-26 1929-11-26 Flintermann Gerhard Heat-exchange device
US1880533A (en) * 1932-02-03 1932-10-04 Servel Sales Inc Heat exchanger
US2688986A (en) * 1950-09-02 1954-09-14 Gen Motors Corp Heat exchanger
US3034769A (en) * 1956-10-26 1962-05-15 Bertin & Cie Heat exchangers
US2949679A (en) * 1957-05-09 1960-08-23 Whirlpool Co Laundry machine with heat storage means
US3137798A (en) * 1961-11-22 1964-06-16 North American Aviation Inc Thermionic power supply

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2360085A (en) * 2000-03-09 2001-09-12 Centrax Ltd Annular heat exchanger with concentric cells for use in gas turbine engine

Also Published As

Publication number Publication date
US3416011A (en) 1968-12-10
DE1501657B1 (en) 1970-07-23

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