GB527018A - Improvements in or relating to the cooling systems of liquid-cooled engines - Google Patents

Improvements in or relating to the cooling systems of liquid-cooled engines

Info

Publication number
GB527018A
GB527018A GB847639A GB847639A GB527018A GB 527018 A GB527018 A GB 527018A GB 847639 A GB847639 A GB 847639A GB 847639 A GB847639 A GB 847639A GB 527018 A GB527018 A GB 527018A
Authority
GB
United Kingdom
Prior art keywords
radiator
engine
liquid
inlet
pipe
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
GB847639A
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 GB847639A priority Critical patent/GB527018A/en
Publication of GB527018A publication Critical patent/GB527018A/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
    • F01P3/00—Liquid cooling
    • F01P3/18—Arrangements or mounting of liquid-to-air heat-exchangers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

527,018. Coolingsystems and radiators for aircraft. ELLOR, J. E. March 16, 1939. No. 8476. [Class 64 (iii)] In a liquid-cooled aircraft engine; a header tank 13 connected at 14 close to the coolantoutlet from the engine jacket is also connected by a single-pipe 15 to one side of a horse-shoe shaped radiator 20 round the bottom of the engine; and a single outlet pipe 17 from the other side of the radiator returns coolant to the inlet of the water jacket. A byepass 21 in the coolant circulation is formed integrally or contiguously with the radiator shell and has a thermally-controlled valve 22 on the inlet pipe, so that water passes through the matrix or the byepass. The radiator is placed in an air tunnel having a diverging inlet 25 and a converging outlet. The header tank and radiator are mounted on the engine.
GB847639A 1939-03-16 1939-03-16 Improvements in or relating to the cooling systems of liquid-cooled engines Expired GB527018A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB847639A GB527018A (en) 1939-03-16 1939-03-16 Improvements in or relating to the cooling systems of liquid-cooled engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB847639A GB527018A (en) 1939-03-16 1939-03-16 Improvements in or relating to the cooling systems of liquid-cooled engines

Publications (1)

Publication Number Publication Date
GB527018A true GB527018A (en) 1940-10-01

Family

ID=9853186

Family Applications (1)

Application Number Title Priority Date Filing Date
GB847639A Expired GB527018A (en) 1939-03-16 1939-03-16 Improvements in or relating to the cooling systems of liquid-cooled engines

Country Status (1)

Country Link
GB (1) GB527018A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2633834A (en) * 1950-12-01 1953-04-07 Elmer C Kiekhaefer Thermostatic control for engines
WO2000063541A1 (en) * 1999-04-19 2000-10-26 Seneca Technology Limited Inverted aircraft engine configuration - radiator location

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2633834A (en) * 1950-12-01 1953-04-07 Elmer C Kiekhaefer Thermostatic control for engines
WO2000063541A1 (en) * 1999-04-19 2000-10-26 Seneca Technology Limited Inverted aircraft engine configuration - radiator location
US6536382B1 (en) 1999-04-19 2003-03-25 Seneca Technology Ltd. Radiator for inverted aircraft engine configuration
AU769795B2 (en) * 1999-04-19 2004-02-05 Wilksch Airmotive Limited Inverted aircraft engine configuration - radiator location

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