GB569270A - Improvements in power plants - Google Patents
Improvements in power plantsInfo
- Publication number
- GB569270A GB569270A GB18623/43A GB1862343A GB569270A GB 569270 A GB569270 A GB 569270A GB 18623/43 A GB18623/43 A GB 18623/43A GB 1862343 A GB1862343 A GB 1862343A GB 569270 A GB569270 A GB 569270A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- valve
- gases
- pressure
- engine
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/02—Gas passages between engine outlet and pump drive, e.g. reservoirs
-
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
-
- 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
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
569,270. Combustion - product plant. AKTIEBOLAGET GOTAVERKEN. Nov. 9, 1943, Nos. 18623 and 18624. Convention dates, Nov. 9, 1942. [Class 7 (i)] [Also in Group XXVI] The plant comprises an internal-combustion two-stroke engine 1, a turbine 3 driven by exhaust gases from the engine supplied. at two different pressures at different times, and a compressor 2 driven by the turbine, which produces scavenging, and maybe supercharging, air for the engine. The gases are admitted to the turbine at different stages. The lowpressure gas pipe 23 (or 40) is alternately open to a low-pressure stage of the turbine, or a pipe 15 leading to the atmosphere. Scavenging air from the compressor passes through a pipe 5 and ports 6 in the engine cylinder. Lowpressure exhaust gases for the turbine are controlled by a valve 8 actuated by a cam or other shaft 13. Gases discharged through ports 16 and channel 17 leading to a conduit 18, are higher in pressure than the final pressure in the cylinder. A valve 19 controls this gas flow. For multi-cylinder engines, the turbine and compressor are common to all the cylinders. Turbine blades of the impulse type are preferably provided for the high-pressure stages, and reaction blades for the remainder. The impulse blades may rotate at a higher speed as by arranging them on the same blade wheel as the reaction blading, but at a greater radius. To facilitate starting of the engine, the lowpressure gases are passed to atmosphere either by manual or automatic means. Fig. 1 shows a valve 24 held closed by gas pressure from the conduit 18 acting through a pipe 25 on a piston 27. When the pressure in 18 is low, a spring forces the piston downwards and, through links 30, 31, the valve 24 drops to close the pipe 23. A silencer may be fitted to the pipe 15. The valve 19 is opened before the piston 4 uncovers the ports 16, and closes as the valve 8 begins to open. Two valves 8 may be provided, opening one after another. The engine may have two pistons running in opposite directions. The. engine may -be reversible with adjusting devices for the valves. The ports 16 may be replaced by a single, valve-controlled port. The turbine 3 may be supplied with a set of starting nozzles fed with compressed air or steam, and a compressor started up by an electric motor which may operate in parallel with the compressor driven by exhaust gases. In Fig. 3, the cylinder 1 is arranged for double or transverse flow scavenging. Scavenging and super-charging air enters a port 33 and exhaust gases are delivered through a single conduit 35. The gases pass to either of two branches 40, 41, high-pressure gases passing through 41, and low-pressure gases through 40 to the lowpressure stage of the turbine 3. The valve 37 alternately closes conduits 40, 41. It may be a slide valve. Exhaust gases may be used to impel separate turbine wheels on a common, or separate,' shafts. A Root's blower may be used in place of the compressor 2.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE569270X | 1942-11-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB569270A true GB569270A (en) | 1945-05-15 |
Family
ID=20312204
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18623/43A Expired GB569270A (en) | 1942-11-09 | 1943-11-09 | Improvements in power plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB569270A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3051147A (en) * | 1957-04-26 | 1962-08-28 | William Doxford & Sons Enginee | Exhaust means for multi-cylinder multiple piston internal combustion engines |
EP2098708A1 (en) * | 2008-03-06 | 2009-09-09 | Wärtsilä Schweiz AG | A method for the operation of a longitudinally scavenged two-stroke large diesel engine and a longitudinally scavenged two stroke large diesel engine |
-
1943
- 1943-11-09 GB GB18623/43A patent/GB569270A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3051147A (en) * | 1957-04-26 | 1962-08-28 | William Doxford & Sons Enginee | Exhaust means for multi-cylinder multiple piston internal combustion engines |
EP2098708A1 (en) * | 2008-03-06 | 2009-09-09 | Wärtsilä Schweiz AG | A method for the operation of a longitudinally scavenged two-stroke large diesel engine and a longitudinally scavenged two stroke large diesel engine |
RU2483220C2 (en) * | 2008-03-06 | 2013-05-27 | Вертзиле Швайц Аг | Method of operating large-size two-stroke diesel engine with cylinder longitudinal blow-out and large-size two-stroke diesel engine with cylinder longitudinal blow-out |
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