GB162008A - Improvements in internal combustion engines - Google Patents

Improvements in internal combustion engines

Info

Publication number
GB162008A
GB162008A GB2603119A GB2603119A GB162008A GB 162008 A GB162008 A GB 162008A GB 2603119 A GB2603119 A GB 2603119A GB 2603119 A GB2603119 A GB 2603119A GB 162008 A GB162008 A GB 162008A
Authority
GB
United Kingdom
Prior art keywords
cylinders
planes
crank
pins
angles
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
GB2603119A
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.)
SHINGE YANO
Original Assignee
SHINGE YANO
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 SHINGE YANO filed Critical SHINGE YANO
Priority to GB2603119A priority Critical patent/GB162008A/en
Publication of GB162008A publication Critical patent/GB162008A/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
    • 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
    • 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
    • F02B2075/1804—Number of cylinders
    • F02B2075/184—Number of cylinders ten
    • 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
    • F02B2075/1804—Number of cylinders
    • F02B2075/1884—Number of cylinders thirty-two

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

162,008. Hall, W., and Yano, S. Oct. 23, 1919. Four-stroke-cycle engines.-In an engine having not less than thirty-two cylinders, an even number of equally-spaced radial cylinders is disposed in each of an even number of planes at right-angles to the crank-shaft the interval between successive ignitions being equal to 720‹ divided by the total number of cylinders. Engines are described having (1) thirty-two cylinders in four planes and a four throw crankshaft the pins of which, when viewed in. end elevation, each make with the adjacent pins angles of 67¢ and 112¢‹ respectively, (2) thirtysix cylinders in six planes, and a six-throw crankshaft in which the crank pins are arranged in three plants separated by angles of 40‹ as shown in Figs. 11, 12, and (3) forty cylinders in four planes as shown in Fig. 20 and a four-throw crank-shaft with crank-pins separated by 90‹, as shown in Fig. 22. Further, an engine may comprise six cylinders in each of eight or ten planes.
GB2603119A 1919-10-23 1919-10-23 Improvements in internal combustion engines Expired GB162008A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2603119A GB162008A (en) 1919-10-23 1919-10-23 Improvements in internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2603119A GB162008A (en) 1919-10-23 1919-10-23 Improvements in internal combustion engines

Publications (1)

Publication Number Publication Date
GB162008A true GB162008A (en) 1921-04-25

Family

ID=10237251

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2603119A Expired GB162008A (en) 1919-10-23 1919-10-23 Improvements in internal combustion engines

Country Status (1)

Country Link
GB (1) GB162008A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767184C (en) * 1938-07-16 1951-12-20 Daimler Benz Ag Internal combustion engine, in particular aircraft engine, with six cylinder stars, each consisting of six cylinders, one behind the other

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE767184C (en) * 1938-07-16 1951-12-20 Daimler Benz Ag Internal combustion engine, in particular aircraft engine, with six cylinder stars, each consisting of six cylinders, one behind the other

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