GB450047A - Improvements in or relating to cooling arrangements in supercharged internal-combustion engines - Google Patents

Improvements in or relating to cooling arrangements in supercharged internal-combustion engines

Info

Publication number
GB450047A
GB450047A GB16491/35A GB1649135A GB450047A GB 450047 A GB450047 A GB 450047A GB 16491/35 A GB16491/35 A GB 16491/35A GB 1649135 A GB1649135 A GB 1649135A GB 450047 A GB450047 A GB 450047A
Authority
GB
United Kingdom
Prior art keywords
cooling
cylinders
manifold
forming
compressor
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
GB16491/35A
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.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane 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 Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Priority to GB16491/35A priority Critical patent/GB450047A/en
Publication of GB450047A publication Critical patent/GB450047A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04—Cooling of air intake supply
    • F02B29/0406—Layout of the intake air cooling or coolant circuit
    • F02B29/0412—Multiple heat exchangers arranged in parallel or in series
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18—Multi-cylinder engines
    • F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222—Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Abstract

450,047. Cooling charge. BRISTOL AEROPLANE CO., Ltd., FEDDEN, A. H. R., and BARRINGTON, T. B., Filton House, Bristol. June 6,1935, No. 16491. [Class 7 (ii)] A radial-cylinder internal-combustion engine for aircraft comprises a supercharging-compressor, an annular induction manifold having an unobstructed bore and communicating with all the inlet ports, and a number of multitubular cooling-radiators arranged within the area bounded by the manifold and opposite the spaces between the cylinders and each connected between the compressor and the manifold. As applied to an engine comprising a crank-case 10 and air-cooled cylinders 11, a blower-casing containing a centrifugal compressor 13 is attached to the rear of the crankcase and has outlets to each of which a union 14 is connected, each union forming a header for a bank of tubes 15 forming a cooling- radiator. The radiators are arranged on radial axes lying between the cylinders, and the outer end of each bank of tubes is connected to a header 17 formed in the wall of a pipe 18 having stuffing-box connections with a curved pipe 25 connected to the inlet ports of a cylinder, the series of pipes 18, 25 thus forming a continuous ring passing right around the engine. Specification 449,340 is referred to.
GB16491/35A 1935-06-06 1935-06-06 Improvements in or relating to cooling arrangements in supercharged internal-combustion engines Expired GB450047A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB16491/35A GB450047A (en) 1935-06-06 1935-06-06 Improvements in or relating to cooling arrangements in supercharged internal-combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB16491/35A GB450047A (en) 1935-06-06 1935-06-06 Improvements in or relating to cooling arrangements in supercharged internal-combustion engines

Publications (1)

Publication Number Publication Date
GB450047A true GB450047A (en) 1936-07-09

Family

ID=10078297

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16491/35A Expired GB450047A (en) 1935-06-06 1935-06-06 Improvements in or relating to cooling arrangements in supercharged internal-combustion engines

Country Status (1)

Country Link
GB (1) GB450047A (en)

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