GB552164A - Improvements in or relating to the cooling of internal-combustion engines - Google Patents

Improvements in or relating to the cooling of internal-combustion engines

Info

Publication number
GB552164A
GB552164A GB1226241A GB1226241A GB552164A GB 552164 A GB552164 A GB 552164A GB 1226241 A GB1226241 A GB 1226241A GB 1226241 A GB1226241 A GB 1226241A GB 552164 A GB552164 A GB 552164A
Authority
GB
United Kingdom
Prior art keywords
passages
air
cylinders
engine
bank
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
GB1226241A
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.)
FERDINAND BASIL GREATRIX
Original Assignee
FERDINAND BASIL GREATRIX
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 FERDINAND BASIL GREATRIX filed Critical FERDINAND BASIL GREATRIX
Priority to GB1226241A priority Critical patent/GB552164A/en
Publication of GB552164A publication Critical patent/GB552164A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P7/00Controlling of coolant flow
    • F01P7/02Controlling of coolant flow the coolant being cooling-air
    • F01P7/023Cowlings for airplane engines

Abstract

552,164. Cooling cylinders, charge, oil &c. READ, J. R., and GREATRIX, F. B. Sept. 22, 1941, No. 12262. [Class 7 (ii)] [Also in Groups XXXIII and XXXIV] In an air-cooled aircraft or other engine having one or more banks of cylinders extending lengthwise of the crankshaft, an air-cooled cooling device, for example for oil or charging air, is mounted at one or each end of the bank of cylinders with its cooling-air passages normal to the length of the bank, and a flow of air is directed transversely of the bank through the cooler and in parallel between the cylinders. The cooling device may cool oil for lubricating the engine or for operating mechanism in the aircraft, or may cool the air supply to the engine between or after the stages of a multi-stage supercharger. In one form, Figs. 1 and 2, the engine has four banks of cylinders 11 and a cooling device 26 of substantially the same dimensions as a cylinder is arranged at the rear end or at each end of each bank. The engine is enclosed in a nacelle 12 and baffles 15 along each bank of cylinders divide the space around the engine into upper and lower passages 16 and side passages 17 closed at the ends by bulkheads 14, 21. Air entering through passages 23 in the wing 13 flows over a supercharger 19 in the compartment 18, through the passages 16, cooling devices 26 and passages 17 to outlets 24 controlled by adjustable flaps 25. The air also passes between the cylinders from the passages 16 to the passages 17. Exhaust manifolds 27 are arranged in the passages 17 and discharge through the outlets 24. In a modification, the air is admitted through the nose of the nacelle and through the lower passage 16 and compartment 18 to the upper passage 16 ; from both passages 16 it flows to the passages 17 through the coolers and between the cylinders. In another form, Fig. 4, an inverted V-engine has a single air-entry passage 16 from which the air flows through the coolers 26 and between the cylinders to an outlet space 17.
GB1226241A 1941-09-22 1941-09-22 Improvements in or relating to the cooling of internal-combustion engines Expired GB552164A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1226241A GB552164A (en) 1941-09-22 1941-09-22 Improvements in or relating to the cooling of internal-combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1226241A GB552164A (en) 1941-09-22 1941-09-22 Improvements in or relating to the cooling of internal-combustion engines

Publications (1)

Publication Number Publication Date
GB552164A true GB552164A (en) 1943-03-25

Family

ID=10001332

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1226241A Expired GB552164A (en) 1941-09-22 1941-09-22 Improvements in or relating to the cooling of internal-combustion engines

Country Status (1)

Country Link
GB (1) GB552164A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE969990C (en) * 1953-07-16 1958-08-07 Motoren Werke Mannheim Ag Air-cooled internal combustion engine with cylinder arrangement in V-shape
GB2348670A (en) * 1999-04-19 2000-10-11 Seneca Tech Ltd Lubricant or coolant heat exchanger location for inverted i.c. piston engine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE969990C (en) * 1953-07-16 1958-08-07 Motoren Werke Mannheim Ag Air-cooled internal combustion engine with cylinder arrangement in V-shape
GB2348670A (en) * 1999-04-19 2000-10-11 Seneca Tech Ltd Lubricant or coolant heat exchanger location for inverted i.c. piston engine
GB2348670B (en) * 1999-04-19 2001-03-07 Seneca Tech Ltd Inverted aircraft configuration - radiator location
US6446592B1 (en) * 1999-04-19 2002-09-10 Seneca Technology Limited Inverted internal combustion engine configuration
US6536382B1 (en) 1999-04-19 2003-03-25 Seneca Technology Ltd. Radiator for inverted aircraft engine configuration

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