GB333790A - Improvements in two-stroke internal combustion engines - Google Patents
Improvements in two-stroke internal combustion enginesInfo
- Publication number
- GB333790A GB333790A GB30342/29A GB3034229A GB333790A GB 333790 A GB333790 A GB 333790A GB 30342/29 A GB30342/29 A GB 30342/29A GB 3034229 A GB3034229 A GB 3034229A GB 333790 A GB333790 A GB 333790A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- rotation
- nozzle
- piston
- combustion air
- 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
- F02B25/00—Engines characterised by using fresh charge for scavenging cylinders
-
- 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
- F02B2720/00—Engines with liquid fuel
- F02B2720/23—Two stroke engines
- F02B2720/237—Two stroke engines with measures for improving combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
333,790. Krupp Germaniawerft Akt.- Ges., F. Oct. 15, 1928, [Convention date]. Cylinders receiving liquid fuel.-In an airless injection two-stroke engine a rotary motion transverse to the cylinder axis is imparted to the combustion air which enters through ports E directed towards a dished crown in the piston. Exhaust ports are located at F. The combustion head may be of the same concave form as the piston crown B or it may be tapered, as shown in plan in Fig. 6. Oppositely located fuel nozzles D, Fig. 6may be disposed on the axis of rotation of the combustion air, the orifices of each nozzle being so arranged that the opposing jets of fuel lie in different planes. Alternatively, one fuel nozzle may be located centrally in the cylinder head; in each arrangement the fuel is injected transversely to the direction of rotation of the air.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE333790X | 1928-10-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB333790A true GB333790A (en) | 1930-08-21 |
Family
ID=6212153
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30342/29A Expired GB333790A (en) | 1928-10-15 | 1929-10-07 | Improvements in two-stroke internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB333790A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0159429B1 (en) * | 1982-08-10 | 1988-06-15 | Howard G. Westerman | Two-cycle stratified charge gas engine |
-
1929
- 1929-10-07 GB GB30342/29A patent/GB333790A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0159429B1 (en) * | 1982-08-10 | 1988-06-15 | Howard G. Westerman | Two-cycle stratified charge gas engine |
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