GB811454A - Improvements in and relating to liquid-cooled internal combustion engines - Google Patents

Improvements in and relating to liquid-cooled internal combustion engines

Info

Publication number
GB811454A
GB811454A GB383656A GB383656A GB811454A GB 811454 A GB811454 A GB 811454A GB 383656 A GB383656 A GB 383656A GB 383656 A GB383656 A GB 383656A GB 811454 A GB811454 A GB 811454A
Authority
GB
United Kingdom
Prior art keywords
chamber
coolant
engine
rotor
blade
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
GB383656A
Inventor
William Eugene Swenson
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.)
Minneapolis Moline Co
Original Assignee
Minneapolis Moline Co
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 Minneapolis Moline Co filed Critical Minneapolis Moline Co
Priority to GB383656A priority Critical patent/GB811454A/en
Publication of GB811454A publication Critical patent/GB811454A/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
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • 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
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/10Pumping liquid coolant; Arrangements of coolant pumps
    • 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
    • F01P2070/00Details
    • F01P2070/30Rotating radiators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

811,454. Centrifugal pumps and fans. MINNEAPOLIS-MOLINE CO. Feb. 7, 1956, No. 3836/56. Class 110 (1). [Also in Group XIII] Apparatus combining the functions of a fan, radiator, pump and flywheel for use with a liquid-cooled internal combustion engine comprises a fan rotor 10 through which engine coolant liquid circulates, said rotor being provided with a plurality of fan blades 11 each having a cham. ber 21 formed therein with an inlet 29 to the chamber disposed radially inwardly of an outlet 30 from the chamber, the rotor incorporating an annular manifold 34 connecting all the blade chamber inlets and an annular chamber 17 connecting all the blade chamber outlets. In the form shown the fan blades 11 extend between the manifold 34 and chamber 17 the latter being formed by a disc 55 and a back plate 12 incorporating a hub 13 whereby the rotor is secured to the engine shaft c. Each blade 11 is externally finned and is of the cross-section shown in Fig. 4 providing a tortuous path engine for coolant flowing therethrough. Forwardly and axially aligned with the hub 13 is a stationary assembly comprising a sleeve 36 partitioned to provide within the sleeve a separate chamber 52. Hot coolant flows from the engine through a duct 45 to chamber 52 and thence through pipes 61 to chamber 34 from which the coolant enters the fan blades through the inlets 29. The coolant cooled in blades 29 is forced by centrifugal action through outlets 30 and enters the rotating annular chamber 17 from which it is collected by stationary scoops 67 which direct the coolant through the sleeve 36, through a port 46 leading to a duct 44 (Fig. 1) and thence to the engine B. Cooling air is expelled radially outwardly, between the fan blades. The blade assembly may be cast as an integral unit.
GB383656A 1956-02-07 1956-02-07 Improvements in and relating to liquid-cooled internal combustion engines Expired GB811454A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB383656A GB811454A (en) 1956-02-07 1956-02-07 Improvements in and relating to liquid-cooled internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB383656A GB811454A (en) 1956-02-07 1956-02-07 Improvements in and relating to liquid-cooled internal combustion engines

Publications (1)

Publication Number Publication Date
GB811454A true GB811454A (en) 1959-04-08

Family

ID=9765846

Family Applications (1)

Application Number Title Priority Date Filing Date
GB383656A Expired GB811454A (en) 1956-02-07 1956-02-07 Improvements in and relating to liquid-cooled internal combustion engines

Country Status (1)

Country Link
GB (1) GB811454A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1222949B (en) * 1961-04-01 1966-08-18 Ingeborg Laing Heat exchanger designed as a drum-shaped fan runner
DE1256665B (en) * 1962-04-19 1967-12-21 Accessair Sa Air heater with a burner and a circulating heat exchanger designed as a fan for conveying both the air and the heating gases
DE1263036B (en) * 1961-04-01 1968-03-14 Ingeborg Laing Heat exchanger designed as a drum-shaped fan runner
GB2239491A (en) * 1989-11-28 1991-07-03 Copermill Ltd Cooling hot gas blower blades.
US7329102B2 (en) 2004-11-13 2008-02-12 Rolls-Royce Plc Blade
CN112324553A (en) * 2020-11-02 2021-02-05 安福锦湖(湖南)气门有限公司 Cooling device for engine exhaust valve

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1222949B (en) * 1961-04-01 1966-08-18 Ingeborg Laing Heat exchanger designed as a drum-shaped fan runner
DE1263036B (en) * 1961-04-01 1968-03-14 Ingeborg Laing Heat exchanger designed as a drum-shaped fan runner
DE1256665B (en) * 1962-04-19 1967-12-21 Accessair Sa Air heater with a burner and a circulating heat exchanger designed as a fan for conveying both the air and the heating gases
GB2239491A (en) * 1989-11-28 1991-07-03 Copermill Ltd Cooling hot gas blower blades.
GB2239491B (en) * 1989-11-28 1993-09-29 Copermill Ltd Hot gas blower
US7329102B2 (en) 2004-11-13 2008-02-12 Rolls-Royce Plc Blade
CN112324553A (en) * 2020-11-02 2021-02-05 安福锦湖(湖南)气门有限公司 Cooling device for engine exhaust valve
CN112324553B (en) * 2020-11-02 2023-06-09 湖南金跃气门科技有限公司 Cooling device of engine exhaust valve

Similar Documents

Publication Publication Date Title
US2822974A (en) Turbine-driven supercharger
US2384251A (en) Liquid cooled supercharger
ES322897A1 (en) A cooling provision for elastic fluid turbine rotor. (Machine-translation by Google Translate, not legally binding)
US2648519A (en) Cooling combustion turbines
GB1401486A (en) Centrifugal compressors especially for supercharging engines
GB1079195A (en) Gas turbine engine cooling
GB1270905A (en) Cooling system for an axial flow elastic fluid utilizing machine
GB520045A (en) Improvements in or relating to elastic fluid turbines
US2578481A (en) Gas turbine power plant with auxiliary compressor supplying cooling air for the turbine
US2428005A (en) Dynamometer
GB730506A (en) Improvements in or relating to gas turbine engines
GB709256A (en) Improvements in gas turbine engines
GB811454A (en) Improvements in and relating to liquid-cooled internal combustion engines
GB667565A (en) Improvements in the cooling of rotating bodies
GB578306A (en) Improvements in an exhaust turbosupercharger
US2684196A (en) Turbine driven fan unit
US2109997A (en) Gas turbine driven supercharger
SE305711B (en)
GB457574A (en) Improvements in bearings for air circulating fans
GB1011477A (en) Rotary piston internal combustion engine
GB864545A (en) An engine super-charger unit
US2659529A (en) Cooling means for the rotors of gas turbine power plants
GB711985A (en) Improvements in gas turbines
JP5932868B2 (en) Cooling structure of axial gap type power generator
US2452185A (en) Fluid pump