GB127326A - Improvements in Internal Combustion Engines for Aircraft and other purposes. - Google Patents
Improvements in Internal Combustion Engines for Aircraft and other purposes.Info
- Publication number
- GB127326A GB127326A GB552417A GB552417A GB127326A GB 127326 A GB127326 A GB 127326A GB 552417 A GB552417 A GB 552417A GB 552417 A GB552417 A GB 552417A GB 127326 A GB127326 A GB 127326A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- purposes
- internal combustion
- combustion engines
- valves
- 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
- F02B75/287—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with several pistons positioned in one cylinder one behind the other
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
127,326. Fowler, H., and Salmon, P. April 19, 1917. Valves.-To produce an impulse every stroke, two single-acting cylinders are disposed in line with, and one on each side of, a double-acting cylinder B. Rotary inlet valves, which are each common to a pair of adjacent explosion spaces, are provided at F<1>, K<2>, and exhaust valves, which are also common to a pair of explosion chambers, at L<1>, L<2>. The space above the piston F serves for circulating cooling-air through the pistons and piston-rods.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB552417A GB127326A (en) | 1917-04-19 | 1917-04-19 | Improvements in Internal Combustion Engines for Aircraft and other purposes. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB552417A GB127326A (en) | 1917-04-19 | 1917-04-19 | Improvements in Internal Combustion Engines for Aircraft and other purposes. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB127326A true GB127326A (en) | 1919-06-05 |
Family
ID=32342209
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB552417A Expired GB127326A (en) | 1917-04-19 | 1917-04-19 | Improvements in Internal Combustion Engines for Aircraft and other purposes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB127326A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS49113708A (en) * | 1973-02-13 | 1974-10-30 |
-
1917
- 1917-04-19 GB GB552417A patent/GB127326A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS49113708A (en) * | 1973-02-13 | 1974-10-30 | ||
JPS5419363B2 (en) * | 1973-02-13 | 1979-07-14 |
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