GB478210A - Improvements in or relating to cooling systems for the engines of aircraft - Google Patents

Improvements in or relating to cooling systems for the engines of aircraft

Info

Publication number
GB478210A
GB478210A GB19441/36A GB1944136A GB478210A GB 478210 A GB478210 A GB 478210A GB 19441/36 A GB19441/36 A GB 19441/36A GB 1944136 A GB1944136 A GB 1944136A GB 478210 A GB478210 A GB 478210A
Authority
GB
United Kingdom
Prior art keywords
liquid
aircraft
engines
cooler
july
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
GB19441/36A
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
Publication of GB478210A publication Critical patent/GB478210A/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
    • F01P3/22—Liquid cooling characterised by evaporation and condensation of coolant in closed cycles; characterised by the coolant reaching higher temperatures than normal atmospheric boiling-point
    • 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
    • F01P7/00—Controlling of coolant flow
    • F01P7/14—Controlling of coolant flow the coolant being liquid
    • F01P7/16—Controlling of coolant flow the coolant being liquid by thermostatic control
    • F01P7/165—Controlling of coolant flow the coolant being liquid by thermostatic control characterised by systems with two or more loops
    • 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
    • F01P2060/00—Cooling circuits using auxiliaries
    • F01P2060/04—Lubricant cooler

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

478,210. Cooling systems for engines. HEINKEL, E. July 13, 1936, No. 19441. Convention date, July 12, 1935. [Class 29] An aircraft engine a is cooled by a liquid, e.g. glycol circulating in a closec cycle including a cool er c, which is coolec by an evaporating liquid, e.g. water, cir culating in a secon dary closed cycle in cluding a condense h. The primary cir cuit has a byepass conduit n controlled by a thermostatic valve e and the secondary circuit includes a valve f controlled by a thermostat or pressure sensitive device. The liquids are circulated by pumps d, i and are in counterflow in the cooler c. The cold part of the cooler may be used to cool lubricating oil in a circuit m. The system permits the use of a primary liquid of high boiling point and of a condenser h of light gauge metal for the lower temperature of the secondary liquid. The condenser may be in the wing of the aircraft as shown, or may be cooled by a further cooling circuit. Several secondary circuits in parallel may be employed.
GB19441/36A 1935-07-12 1936-07-13 Improvements in or relating to cooling systems for the engines of aircraft Expired GB478210A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE478210X 1935-07-12

Publications (1)

Publication Number Publication Date
GB478210A true GB478210A (en) 1938-01-13

Family

ID=6542222

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19441/36A Expired GB478210A (en) 1935-07-12 1936-07-13 Improvements in or relating to cooling systems for the engines of aircraft

Country Status (1)

Country Link
GB (1) GB478210A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2564140A1 (en) * 1984-05-11 1985-11-15 Evans Cooling Ass COOLING METHOD AND APPARATUS FOR INTERNAL COMBUSTION ENGINE

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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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