GB306942A - Improvements in radial cylinder for internal combustion engines - Google Patents
Improvements in radial cylinder for internal combustion enginesInfo
- 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
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
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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US2426871A (en) * | 1942-05-22 | 1947-09-02 | United Aireraft Corp | Air cooling for radial engines |
GB2341220A (en) * | 1998-09-04 | 2000-03-08 | Cummins Engine Co Ltd | Camshaft alignment and arrangement relative to crankshaft |
-
1929
- 1929-02-11 GB GB4510/29A patent/GB306942A/en not_active Expired
Cited By (4)
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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