GB191500620A - Improvements in Internal Combustion Engines. - Google Patents
Improvements in Internal Combustion Engines.Info
- Publication number
- GB191500620A GB191500620A GB191500620DA GB191500620A GB 191500620 A GB191500620 A GB 191500620A GB 191500620D A GB191500620D A GB 191500620DA GB 191500620 A GB191500620 A GB 191500620A
- Authority
- GB
- United Kingdom
- Prior art keywords
- port
- ports
- shaft
- passages
- enters
- 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
- F02B75/28—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
- F02B75/282—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders the pistons having equal strokes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F01B3/02—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis with wobble-plate
-
- 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
- F02B75/26—Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
-
- 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
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/025—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Valve Device For Special Equipments (AREA)
Abstract
620. Froehlich, W. Jan. 14. Two-stroke-cycle engines; driving-gear.-An engine having a number of parallel cylinders arranged around a central shaft 2, and in which oppositely-moving pistons actuate a pair of wobbling rings 6, compresses scavenging-air and combustible mixture in the closed ends x, y respectively of each cylinder. Combustible mixture enters the pump spaces y through ports 8, 10 in the shaft 2 and passages 11, through which the mixture is delivered, after compression, to ports 28 opening into a reservoir p and a hollow portion of the shaft leading to passages 22, each terminating in a cylinder admission port 16. Scavenging-air, which enters the cylinders through passages 20 and the ports 16, is admitted to the pump spaces x through a port 14 and, after compression, is delivered to the hollow portion of the shaft on the lefthand side of the partition 12 and to the reservoir m. Upon the closing of the admission ports 16, the combustible mixture remaining in a passage 22 is withdrawn through a port 24, which coincides with a port 23 opening into the chamber 9. Simultaneously-compressed air enters the passages 20, 22 through a port 25. Mixture leaking along the shaft is arrested in annular channels 26, 27, which are exhausted by the pumps y. The exhaust ports are controlled by a ring valve 17.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB191500620T | 1915-01-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB191500620A true GB191500620A (en) | 1915-07-15 |
Family
ID=32648615
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB191500620D Expired GB191500620A (en) | 1915-01-14 | 1915-01-14 | Improvements in Internal Combustion Engines. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB191500620A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1986006136A1 (en) * | 1985-04-12 | 1986-10-23 | Edwin Ott | Convertible diesel engine for aircraft or other applications with optimalized high output, high supercharge and total energy utilization |
WO2012071021A1 (en) * | 2010-11-24 | 2012-05-31 | Orth Albin | Valve-free four-stroke combustion engine with axially opposed pistons |
-
1915
- 1915-01-14 GB GB191500620D patent/GB191500620A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1986006136A1 (en) * | 1985-04-12 | 1986-10-23 | Edwin Ott | Convertible diesel engine for aircraft or other applications with optimalized high output, high supercharge and total energy utilization |
US4905637A (en) * | 1985-04-12 | 1990-03-06 | Edwin Ott | Diesel aircraft engine--also convertible for other applications--optimized for high output, high supercharge and total energy utilization |
WO2012071021A1 (en) * | 2010-11-24 | 2012-05-31 | Orth Albin | Valve-free four-stroke combustion engine with axially opposed pistons |
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