GB306942A - Improvements in radial cylinder for internal combustion engines - Google Patents

Improvements in radial cylinder for internal combustion engines

Info

Publication number
GB306942A
GB306942A GB4510/29A GB451029A GB306942A GB 306942 A GB306942 A GB 306942A GB 4510/29 A GB4510/29 A GB 4510/29A GB 451029 A GB451029 A GB 451029A GB 306942 A GB306942 A GB 306942A
Authority
GB
United Kingdom
Prior art keywords
cylinders
row
crank
radial cylinder
súguin
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
GB4510/29A
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 GB306942A publication Critical patent/GB306942A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • F02B75/222Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement

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

306,942. SÚguin, L., and SÚguin, A. Feb. 28, 1928, [Convention date]. Balancing moving parts by weights. - In radial cylinder engines particularly for use on aircraft and having a number of rows of cylinders the overall length of the engine measured axially along the crank shaft is reduced by arranging the cylinders in each row out of line. As shown in Fig. 3, alternate cylinders are displaced; in another form the centres of the cylinders may form a helix or as shown in Fig. 6 the middle cylinders of a row are side by side but behind the outer cylinders. The crank throws are arranged at angles to suit the angular disposition of the cylinders and balance weights 3 are attached to the crank webs by dovetail joints and pairs of restraining plates 4, 5. The crank throws may be arranged as if the cylinders were in line in each row.
GB4510/29A 1928-02-28 1929-02-11 Improvements in radial cylinder for internal combustion engines Expired GB306942A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR306942X 1928-02-28

Publications (1)

Publication Number Publication Date
GB306942A true GB306942A (en) 1930-02-27

Family

ID=8888980

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4510/29A Expired GB306942A (en) 1928-02-28 1929-02-11 Improvements in radial cylinder for internal combustion engines

Country Status (1)

Country Link
GB (1) GB306942A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426871A (en) * 1942-05-22 1947-09-02 United Aireraft Corp Air cooling for radial engines
US2426879A (en) * 1944-09-01 1947-09-02 United Aircraft Corp Radial aircraft engine
US2426874A (en) * 1944-09-01 1947-09-02 United Aircraft Corp Radial aircraft engine
GB2341220A (en) * 1998-09-04 2000-03-08 Cummins Engine Co Ltd Camshaft alignment and arrangement relative to crankshaft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426871A (en) * 1942-05-22 1947-09-02 United Aireraft Corp Air cooling for radial engines
US2426879A (en) * 1944-09-01 1947-09-02 United Aircraft Corp Radial aircraft engine
US2426874A (en) * 1944-09-01 1947-09-02 United Aircraft Corp Radial aircraft engine
GB2341220A (en) * 1998-09-04 2000-03-08 Cummins Engine Co Ltd Camshaft alignment and arrangement relative to crankshaft

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