GB428570A - Improvements in or relating to the cooling systems of internal combustion engines on aircraft - Google Patents

Improvements in or relating to the cooling systems of internal combustion engines on aircraft

Info

Publication number
GB428570A
GB428570A GB2232034A GB2232034A GB428570A GB 428570 A GB428570 A GB 428570A GB 2232034 A GB2232034 A GB 2232034A GB 2232034 A GB2232034 A GB 2232034A GB 428570 A GB428570 A GB 428570A
Authority
GB
United Kingdom
Prior art keywords
pipe
radiator
liquid
cooling
condenser
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
GB2232034A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co 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 Fairey Aviation Co Ltd filed Critical Fairey Aviation Co Ltd
Priority to GB2232034A priority Critical patent/GB428570A/en
Publication of GB428570A publication Critical patent/GB428570A/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
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • F01P11/02Liquid-coolant filling, overflow, venting, or draining devices

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

428,570. Cooling cylinders. FAIREY AVIATION CO., Ltd., Cranford Lane, Hayes, Middlesex, and LYON, G., Ranmoor, Fulmer Road, Gerrards Cross, Buckinghamshire. July 31, 1934, No. 22320. [Class 7 (ii)] [See also Group XIII] In a cooling system for an aircraft engine in which cooling liquid is circulated through a radiator 6 and, during overload, vapour, separated in a separator 4, is condensed in a condenser 11 located above the radiator, the hydraulic resistances are such that the drain pipe 13, by which the condensate returns to the radiator, always has a head of liquid standing therein, and air is thus prevented from entering the system. If the separator 4 is not large enough to take all the liquid when heated, the condenser is divided into two parts by a partition 19, a connecting steam pipe 20 acting as a water lock. A gravity-actuated valve on the end of this pipe, or on the end of the connecting pipe 9, closes during inverted flying, an inverted vent pipe 12 still being available to vent the system. An auxiliary drain pipe 22 is also arranged to have a head of liquid standing therein. The drain pipes 13, 22 may be connected to the throats of Venturi tubes in a byepass between the inlet and outlet pipes of the radiator, and the inlet pipe thereof, respectively.
GB2232034A 1934-07-31 1934-07-31 Improvements in or relating to the cooling systems of internal combustion engines on aircraft Expired GB428570A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2232034A GB428570A (en) 1934-07-31 1934-07-31 Improvements in or relating to the cooling systems of internal combustion engines on aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2232034A GB428570A (en) 1934-07-31 1934-07-31 Improvements in or relating to the cooling systems of internal combustion engines on aircraft

Publications (1)

Publication Number Publication Date
GB428570A true GB428570A (en) 1935-05-15

Family

ID=10177484

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2232034A Expired GB428570A (en) 1934-07-31 1934-07-31 Improvements in or relating to the cooling systems of internal combustion engines on aircraft

Country Status (1)

Country Link
GB (1) GB428570A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE753423C (en) * 1939-08-16 1952-09-22 Daimler Benz Ag Evaporative cooling device for internal combustion engines
FR2564140A1 (en) * 1984-05-11 1985-11-15 Evans Cooling Ass COOLING METHOD AND APPARATUS FOR INTERNAL COMBUSTION ENGINE

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE753423C (en) * 1939-08-16 1952-09-22 Daimler Benz Ag Evaporative cooling device for internal combustion engines
FR2564140A1 (en) * 1984-05-11 1985-11-15 Evans Cooling Ass COOLING METHOD AND APPARATUS FOR INTERNAL COMBUSTION ENGINE
GB2159878A (en) * 1984-05-11 1985-12-11 Evans Cooling Ass Cooling internal combustion engines with coolant vaporisation

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