GB653407A - Heat exchanger - Google Patents

Heat exchanger

Info

Publication number
GB653407A
GB653407A GB47/48A GB4748A GB653407A GB 653407 A GB653407 A GB 653407A GB 47/48 A GB47/48 A GB 47/48A GB 4748 A GB4748 A GB 4748A GB 653407 A GB653407 A GB 653407A
Authority
GB
United Kingdom
Prior art keywords
heat exchanger
jan
aircraft
turbine
duct
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
GB47/48A
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.)
Garrett Corp
Original Assignee
Garrett 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 Garrett Corp filed Critical Garrett Corp
Publication of GB653407A publication Critical patent/GB653407A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00—Pumping cooling-air or liquid coolants
    • F01P5/02—Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases

Landscapes

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

Abstract

653,407. Cooling radiators for aircraft &c. GARRETT CORPORATION. Jan. 1, 1948, No. 47. Convention date, Jan. 3, 1947. [Class 64(iii)] In a cooling device, e.g. an oil cooler for ;aircraft, coolant air flowing through a duct 11 containing a coaxial annular heat exchanger 32 is cooled before entering the latter by driving rotary heat energy extraction means, e.g. a turbine 15, which drives a fan 45 mounted on the same shaft 19, or a generator, fuel pump, vacuum pump &c.
GB47/48A 1947-01-03 1948-01-01 Heat exchanger Expired GB653407A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US653407XA 1947-01-03 1947-01-03

Publications (1)

Publication Number Publication Date
GB653407A true GB653407A (en) 1951-05-16

Family

ID=22062033

Family Applications (1)

Application Number Title Priority Date Filing Date
GB47/48A Expired GB653407A (en) 1947-01-03 1948-01-01 Heat exchanger

Country Status (1)

Country Link
GB (1) GB653407A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2632012A1 (en) * 1988-05-31 1989-12-01 Peugeot Cooling element with two sets of fan blades
CN103046992A (en) * 2011-12-29 2013-04-17 摩尔动力(北京)技术股份有限公司 Unpowered fan radiator

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2632012A1 (en) * 1988-05-31 1989-12-01 Peugeot Cooling element with two sets of fan blades
CN103046992A (en) * 2011-12-29 2013-04-17 摩尔动力(北京)技术股份有限公司 Unpowered fan radiator

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