GB128419A - Improvements in and relating to Rotary Engines, Pumps, Blowers and the like. - Google Patents
Improvements in and relating to Rotary Engines, Pumps, Blowers and the like.Info
- Publication number
- GB128419A GB128419A GB10854/18A GB1085418A GB128419A GB 128419 A GB128419 A GB 128419A GB 10854/18 A GB10854/18 A GB 10854/18A GB 1085418 A GB1085418 A GB 1085418A GB 128419 A GB128419 A GB 128419A
- Authority
- GB
- United Kingdom
- Prior art keywords
- drum
- vanes
- casing
- exhaust
- ports
- 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
- F01C1/02—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F01C1/063—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them
- F01C1/067—Rotary-piston machines or engines of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them having cam-and-follower type drive
-
- 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
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/18—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
128,419. Bevington, M. Ling-. July 2, 1918. Movable-abutment type; cooling parts; packing drums, vanes, etc.; valves, distributing etc.; working-fluid supply. - Relates to rotary engines, pumps, and the like comprising a drum 4 with outwardly arranged radial vanes 14 alternating with vanes 13 projecting inwardly from a casing 1, 1<a>, in which the drum alternately over-runs, and is over-run by, the casing. In the construction of internal-combustion engine shown, the exhaust fluid passes radially outwards across sets of vanes 36 carried by the casing 1, 1<a> and through an impact wheel 44 geared to the casing. Rotary valves 21 mounted in the vanes 13 are operated by sun-and-planet gear to control the admission and exhaust of the working fluid in the spaces between the vanes, as well as a scavenging air-blast supplied by the fans F<1>, F<2>. Each casing-vane 13 has a fuel-supply passage 19, air cooling passages 15, 16 communicating at 17, 18, and a boring to receive the valve 21. Each valve is also formed with a main admission port 30, a main exhaust port 31, and ports 28, 29 serving alternately for admission and exhaust. Packing-strips 60 having oil passages 61, 62 are recessed into the vanes 13, and pressed against the surface of the drum 4 by springs 64. Each drum vane 14 has internal walls 72, 75, Fig. 7, braced by tubes 67, 68, leaving a space 71, 73, 76 which communicates through borings 74, 77 with the inner periphery of the drum 4. The rubbing surfaces of the vanes are packed by metal strips 82, 86, 93, Fig. 8, having oil passages &c. 89, 90 communicating by borings with annular passages 151 on the drum. The drum 4 is also formed with internal annular grooves 148, 149 from which lubricant is supplied to the passage 151, the ballbearings 2, and by passages 120, 121, 122 to the surface of a fixed drum 106. The latter is supported on the shaft 109 through the bearings 136. In the arrangement shown, lubricant is supplied by a pipe 172 and circulated by pumps P round the engine to the delivery-pipe 171. Each pump P, shown separately in Fig. 13, is of the same general type as the main engine, comprising a casing 154 with vanes 153 alternating with vanes 155 carried by a drum 156. Ports 161, 162, 163 co-operate with ports 123, 124 arranged around the reduced ends of the drum 106, the ports 123 at one end, and the ports 124 at the other end, leading by channels 126 to the annular passage 120 to supply the vane lubrication. The casing vanes are cooled by a fan F<1> driving air through the channels 15, 16, the drum vanes being cooled by a fan F<2> which also supplies air to the interior of the drum 106. This drum carries ferrules 114 adapted to register successively with apertures G in the drum 4 towards the end of the exhaust strokes for scavenging the working spaces between the sets of vanes. Figs. 3 and 4 show the gear for operating the valves 21. A sleeve 215 carries guides 212 for straps 211 of eccentric pins 209 which project from disks 202. The latter carry sprockets 221 which drive, through intermediate gears 223, sprockets 224 on the valve spindles. In the position shown in Fig. 2, A, C, I, E represent admission, compression, ignition, and exhaust as taking place in the respective spaces, four working cycles being effected during each revolution. The valve may be modified for a two-stroke engine or for operation by steam or compressed air.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10854/18A GB128419A (en) | 1918-07-02 | 1918-07-02 | Improvements in and relating to Rotary Engines, Pumps, Blowers and the like. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB10854/18A GB128419A (en) | 1918-07-02 | 1918-07-02 | Improvements in and relating to Rotary Engines, Pumps, Blowers and the like. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB128419A true GB128419A (en) | 1919-06-26 |
Family
ID=32344741
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB10854/18A Expired GB128419A (en) | 1918-07-02 | 1918-07-02 | Improvements in and relating to Rotary Engines, Pumps, Blowers and the like. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB128419A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007132071A1 (en) * | 2006-05-12 | 2007-11-22 | Mrcc Industries Sas | Lubrication and cooling of rotary piston engines |
WO2007132070A1 (en) * | 2006-05-12 | 2007-11-22 | Mrcc Industries Sas | Management of gaseous flows for rotary engines |
CN103352755A (en) * | 2013-07-29 | 2013-10-16 | 于魁江 | Novel internal combustion engine |
-
1918
- 1918-07-02 GB GB10854/18A patent/GB128419A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2007132071A1 (en) * | 2006-05-12 | 2007-11-22 | Mrcc Industries Sas | Lubrication and cooling of rotary piston engines |
WO2007132070A1 (en) * | 2006-05-12 | 2007-11-22 | Mrcc Industries Sas | Management of gaseous flows for rotary engines |
CN103352755A (en) * | 2013-07-29 | 2013-10-16 | 于魁江 | Novel internal combustion engine |
CN103352755B (en) * | 2013-07-29 | 2015-10-21 | 于魁江 | A kind of internal combustion engine |
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