GB296564A - Improvements in rotary engines and pumps - Google Patents

Improvements in rotary engines and pumps

Info

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
Application number
GB1274327A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB1274327A priority Critical patent/GB296564A/en
Publication of GB296564A publication Critical patent/GB296564A/en
Expired legal-status Critical Current

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

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.
GB1274327A 1928-03-12 1928-03-12 Improvements in rotary engines and pumps Expired GB296564A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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