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GB685702A - Improvements in or relating to heat exchangers - Google Patents

Improvements in or relating to heat exchangers

Info

Publication number
GB685702A
GB685702A GB40350A GB40350A GB685702A GB 685702 A GB685702 A GB 685702A GB 40350 A GB40350 A GB 40350A GB 40350 A GB40350 A GB 40350A GB 685702 A GB685702 A GB 685702A
Authority
GB
United Kingdom
Prior art keywords
rotor
casing
cell
heat
heat transfer
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
GB40350A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB40350A priority Critical patent/GB685702A/en
Publication of GB685702A publication Critical patent/GB685702A/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
    • F28D19/00Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium
    • F28D19/04Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier
    • F28D19/041Regenerative heat-exchange apparatus in which the intermediate heat-transfer medium or body is moved successively into contact with each heat-exchange medium using rigid bodies, e.g. mounted on a movable carrier with axial flow through the intermediate heat-transfer medium

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)
  • Sorption Type Refrigeration Machines (AREA)

Abstract

685,702. Rotary-matrix type regenerators. RICARDO, H. R., and ALCOCK, J. F. Dec. 14, 1950 [Jan. 6, 1950], No. 403/50. Class 64 (i) [Also in Group XXXIV] In a rotary regenerative heat exchanger in which a rotor E, E<SP>1</SP> is subdivided by partitions (not shown) into angularly spaced cells containing heat transfer material E<SP>2</SP>, and is rotatably arranged in a casing provided with inlet and outlet ports B, B<SP>1</SP>, C, C<SP>1</SP> for two fluid streams (e.g. hot gas and cold gas) to flow in opposite wholly or mainly axial directions through the rotor, the casing is provided with a jacket through which a heat transfer fluid is circulated to maintain substantially equal temperatures at least at those parts of the casing structure which carry and determine the position of its mating surfaces i.e. those surfaces adjacent the end surfaces of the rotor, the mating surfaces E<SP>3</SP>, A<SP>6</SP> and E<SP>4</SP>, A<SP>7</SP> of the rotor and casing being of frusto-conical form (regarding a flat surface as a cone of 180 degrees apex angle) with the apices of the cones meeting substantially at an apex point F on the axis of rotation of the rotor and means being provided for locating the rotor axially with respect to the casing so that the effective point of axial location coincides substantially with the apex point. In the form shown the casing jacket comprises chambers A<SP>1</SP>- A<SP>5</SP> through which water is circulated. The rotor is supported by means of pins G<SP>3</SP> on a hub member G, the pins G<SP>3</SP> permitting free radial expansion of the rotor relatively to the hub G. Interspaced discs H resembling a labyrinth packing are provided to transfer heat between the hub G and the adjacent portion of the casing while the shaft and hub assembly G, G<SP>1</SP> is supported on ball and roller bearings the axial position of the rotor being determined by the ball bearing H4 which is so arranged that the nominal axis of rotation of each ball therein passes through the apex point F. It is stated that the position of the bearing H4 is maintained substantially unaffected by relative thermal expansion or contraction of the casing and the rotor. The heat transfer liquid may be circulated continuously through the chambers in the casing and the circuit may also include a radiator located in the duct leading to the cold gas inlet C to transfer heat absorbed by the circulating fluid to the incoming cold gas. The rotor shaft may be carried in a separate housing surrounded by a cooling chamber. The heat exchange material E<SP>2</SP> in the rotor may comprise metallic gauze or the like substantially filling each cell. Alternatively each cell of the matrix may contain a metallic tapered tube element L (Fig. 3) of cellular form and so disposed in the cell that hot gas flowing through the matrix enters the elements at their open ends so that the cell walls are contacted only by cold gas to be heated and by heating gas which has given up its heat to the matrix. The heat transfer elements may be supported by the cell walls alone or (as shown) they may each be arranged in a tubular casing K conforming in shape to a rotor cell. According to the provisional specification the cell walls contacted by the hot gases are provided with thermal insulation and the casing is maintained at a temperature just below the boiling point of the heat transfer fluid which is circulated therethrough by a pump. Specification 613,283 is referred to.
GB40350A 1950-01-06 1950-01-06 Improvements in or relating to heat exchangers Expired GB685702A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB40350A GB685702A (en) 1950-01-06 1950-01-06 Improvements in or relating to heat exchangers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB40350A GB685702A (en) 1950-01-06 1950-01-06 Improvements in or relating to heat exchangers

Publications (1)

Publication Number Publication Date
GB685702A true GB685702A (en) 1953-01-07

Family

ID=9703768

Family Applications (1)

Application Number Title Priority Date Filing Date
GB40350A Expired GB685702A (en) 1950-01-06 1950-01-06 Improvements in or relating to heat exchangers

Country Status (1)

Country Link
GB (1) GB685702A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2892615A (en) * 1953-06-12 1959-06-30 Carrier Corp Heat exchangers of the rotary regenerator type
US2896920A (en) * 1953-06-12 1959-07-28 Carrier Corp Regenerator structure
US3187804A (en) * 1963-06-21 1965-06-08 Combustion Eng Distortion control for high temperature heat exchangers
US3978913A (en) * 1973-09-24 1976-09-07 Granco Equipment, Inc. Incinerator and heat exchanger structure therefor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2892615A (en) * 1953-06-12 1959-06-30 Carrier Corp Heat exchangers of the rotary regenerator type
US2896920A (en) * 1953-06-12 1959-07-28 Carrier Corp Regenerator structure
US3187804A (en) * 1963-06-21 1965-06-08 Combustion Eng Distortion control for high temperature heat exchangers
US3978913A (en) * 1973-09-24 1976-09-07 Granco Equipment, Inc. Incinerator and heat exchanger structure therefor

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