GB296564A - Improvements in rotary engines and pumps - Google Patents
Improvements in rotary engines and pumpsInfo
- Publication number
- GB296564A GB296564A GB1274327A GB1274327A GB296564A GB 296564 A GB296564 A GB 296564A GB 1274327 A GB1274327 A GB 1274327A GB 1274327 A GB1274327 A GB 1274327A GB 296564 A GB296564 A GB 296564A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- compressor
- rotor
- abutment
- valve
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/356—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
- F01C1/3562—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Abstract
296,564. Lammeren, W. P. van. March 12, 1928. Movable abutment type; working-fluid supply; cooling parts. - A rotary engine or pump of the sliding abutment type with an annular chamber and piston 4 of circular cross-section has the piston 4 formed cam-shape and with a groove 13 of a shape to correspond with the semi-circular abutting end of the sliding abutment, Fig. 10. Fig. 6 shows an internal-combustion engine in which mixture compressed in a compressor chamber 24 is transferred past a rotary disc valve 29 to the explosion chamber 25. The compressor and engine pistons are arranged at an angle to each other and also the disc valve 29 are carried by a rotor which is formed with flanges co-operating with the stator to form the annular chambers 24, 25 of circular cross-section. The abutments 5 may be spring-actuated but are shown fitted with control pistons 6 for pneumatic operation, the compressor abutment being actuated by the exhaust gas pressure and the engine abutment by the compressed gas pressure through the medium of the disc valve 29 carried by the rotor. The rotor is cooled by openings 36 for the passage of air and the stator by water jackets 37. In the modification shown in Fig. 8 the engine unit is replaced by turbine blades 46. Mixture is compressed past a valve 42 into an explosion chamber 43 and after ignition is delivered past a valve 45 on to the blades. The compressor piston, valves 42, 45, and turbine blades 46 are carried by a single rotor 47.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1274327A GB296564A (en) | 1928-03-12 | 1928-03-12 | Improvements in rotary engines and pumps |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1274327A GB296564A (en) | 1928-03-12 | 1928-03-12 | Improvements in rotary engines and pumps |
Publications (1)
Publication Number | Publication Date |
---|---|
GB296564A true GB296564A (en) | 1928-09-13 |
Family
ID=10010280
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1274327A Expired GB296564A (en) | 1928-03-12 | 1928-03-12 | Improvements in rotary engines and pumps |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB296564A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3262432A (en) * | 1964-04-06 | 1966-07-26 | Leroy W Ross | Rotary engine |
US4028885A (en) * | 1971-07-15 | 1977-06-14 | Ganley Thomas J | Rotary engine |
-
1928
- 1928-03-12 GB GB1274327A patent/GB296564A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3262432A (en) * | 1964-04-06 | 1966-07-26 | Leroy W Ross | Rotary engine |
US4028885A (en) * | 1971-07-15 | 1977-06-14 | Ganley Thomas J | Rotary engine |
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