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GB578523A - Improvements in or relating to heat exchange apparatus - Google Patents

Improvements in or relating to heat exchange apparatus

Info

Publication number
GB578523A
GB578523A GB18999/43A GB1899943A GB578523A GB 578523 A GB578523 A GB 578523A GB 18999/43 A GB18999/43 A GB 18999/43A GB 1899943 A GB1899943 A GB 1899943A GB 578523 A GB578523 A GB 578523A
Authority
GB
United Kingdom
Prior art keywords
passages
nests
headers
tanks
header
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
GB18999/43A
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.)
Gallay Ltd
Original Assignee
Gallay 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 Gallay Ltd filed Critical Gallay Ltd
Priority to GB18999/43A priority Critical patent/GB578523A/en
Priority to FR923345D priority patent/FR923345A/en
Publication of GB578523A publication Critical patent/GB578523A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10Radiator arrangement
    • 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
    • F28F2250/00Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
    • F28F2250/10Particular pattern of flow of the heat exchange media
    • F28F2250/102Particular pattern of flow of the heat exchange media with change of flow direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

578,523. Heat-exchange apparatus. CHURCHILL, J. A., BELAIEFF, J. F., DELANEY, C. T., and GALLAY, Ltd. Nov. 15, 1943, No. 18999. [Class 64 (iii)] Annular heat exchange apparatus, e.g., a radiator for an aircraft engine, comprises a plurality of passages for fluid to be cooled disposed in cylindrical formation about the axis of the apparatus, and one or more passages for cooling medium radiating from that axis and progressing axially of the apparatus. In one form, an annular radiator comprises two conical cowlings 21, 22 disposed one within the other with a common axis, annular header tanks 23, 24, 25, 26 on the cowlings 21, 22, and a cylindrical matrix 20 containing U-shaped passages 27, 28 which are arranged in nests, each nest lying radially and the nests being separated by radial gaps in which are disposed pairs of sheets of corrugated metal, forming the passages for the cooling air. The corrugations run parallel to the surfaces of the cowlings. The passages 27, 28 may be formed by corrugated plates in rhomboidal casings, or by U-shaped tubes nested within one another and passing through conical supporting gills which replace the corrugated sheets between the nests. The passages 27 in some of the nests, e.g., alternate nests or pairs of nests, open into the header tanks 25, 26, and the passages 28 in the intermediate nests open into the tanks 23, 24. Oil to be cooled may flow through the tanks 23, 24 and passages 28, and water through the tanks 25, 26 and passages 27. To enable liquid to pass to and from the headers 23, 24 without interference with the flow of air through the passage 58, a pair of passages arranged in positions similar to the nests of passages 27, 28 extend right through the headers 25, 26 at the rear, and at the front open one into each of the headers 23, 24. The headers at both ends may be divided diametrically. The two halves of each header at the front may be connected together so that the fluid can flow from one half to the other. In another form, there is a single annular header on each cowling, and these headers are connected by straight tubes across the conical air passage. In this passage are arranged a series of parallel frustoconical plates or gills through which the tubes pass. Radiators may be formed in two or more segments to facilitate assembly or removal.
GB18999/43A 1943-11-15 1943-11-15 Improvements in or relating to heat exchange apparatus Expired GB578523A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB18999/43A GB578523A (en) 1943-11-15 1943-11-15 Improvements in or relating to heat exchange apparatus
FR923345D FR923345A (en) 1943-11-15 1946-03-04 Heat exchange device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18999/43A GB578523A (en) 1943-11-15 1943-11-15 Improvements in or relating to heat exchange apparatus

Publications (1)

Publication Number Publication Date
GB578523A true GB578523A (en) 1946-07-02

Family

ID=10122044

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18999/43A Expired GB578523A (en) 1943-11-15 1943-11-15 Improvements in or relating to heat exchange apparatus

Country Status (2)

Country Link
FR (1) FR923345A (en)
GB (1) GB578523A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2234805A (en) * 1989-08-04 1991-02-13 Rolls Royce Plc A heat exchanger arrangement for a gas turbine engine
CN102410759A (en) * 2011-07-26 2012-04-11 中国北车集团大连机车研究所有限公司 Multi-system Integral Cooling Module
CN115597420A (en) * 2022-12-15 2023-01-13 四川大学(Cn) A staggered counter-flow precooling heat exchanger

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117842406B (en) * 2024-03-07 2024-05-28 中国空气动力研究与发展中心空天技术研究所 Heat radiation system and oil-electricity hybrid unmanned aerial vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2234805A (en) * 1989-08-04 1991-02-13 Rolls Royce Plc A heat exchanger arrangement for a gas turbine engine
CN102410759A (en) * 2011-07-26 2012-04-11 中国北车集团大连机车研究所有限公司 Multi-system Integral Cooling Module
CN115597420A (en) * 2022-12-15 2023-01-13 四川大学(Cn) A staggered counter-flow precooling heat exchanger

Also Published As

Publication number Publication date
FR923345A (en) 1947-07-03

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