GB479278A - Improvements in and relating to the charging of compression ignition internal combustion engines - Google Patents
Improvements in and relating to the charging of compression ignition internal combustion enginesInfo
- Publication number
- GB479278A GB479278A GB12056/36A GB1205636A GB479278A GB 479278 A GB479278 A GB 479278A GB 12056/36 A GB12056/36 A GB 12056/36A GB 1205636 A GB1205636 A GB 1205636A GB 479278 A GB479278 A GB 479278A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- valve
- speed
- working
- cylinder
- 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
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
-
- 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
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
- F02B37/11—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump driven by other drive at starting only
-
- 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
- F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
-
- 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
479,278. Pumps. SMIRNOFF, V. May 28,1936, No. 12056. [Class 7 (ii)] One or more compressors M, G driven from the engine, either through gearing or through an exhaust turbine E, are provided with controlling means responsive to engine operating conditions ; a further pump supplies air only at operating conditions outside the effective working range of the main compressors. A slotted plate F covering a variable number of nozzles N regulates the speed of the turbine E, being mounted on a hollow shaft carrying a pinion f. A speed-governor g, Fig. 1, and a capsule a<1>, responsive to intake or exhaust pressure, control the position of the rack k. acting through oil-pressure servomotors and linkwork connecting the rack with pistons d<1>, d<2>. At starting, some working cylinders are used as pumps. The settings of the valve P<2> and of the cock D are changed to admit air to the cylinder shown at the right of Fig. 2, the air so compressed being transferred to the air-receiver K and the valve P<1> of the working cylinder to the left. In a modification, Fig. 4, air from the compressor (not shown) which suffices for normal running is supplied to the manifolds L<1>, L<2> by conduit J. At starting the normal exhaust valve R<2> becomes an air intake and the cock P is closed until sufficient pressure is attained in the manifold L<2>. A valve Q then lifts and simultaneously the valves R<2>, P are reset, and the temporary pump cylinder reverts to normal working conditions. The pump M may be driven through variable-speed gearing. Heated compressed air may be supplied when necessary to the air-receivers L<1>, L2.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12056/36A GB479278A (en) | 1936-05-28 | 1936-05-28 | Improvements in and relating to the charging of compression ignition internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB12056/36A GB479278A (en) | 1936-05-28 | 1936-05-28 | Improvements in and relating to the charging of compression ignition internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB479278A true GB479278A (en) | 1938-01-28 |
Family
ID=9997618
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB12056/36A Expired GB479278A (en) | 1936-05-28 | 1936-05-28 | Improvements in and relating to the charging of compression ignition internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB479278A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423417A (en) * | 1942-09-14 | 1947-07-01 | Hobson Ltd H M | Exhaust-driven supercharger for internal-combustion engines |
US2444644A (en) * | 1943-07-31 | 1948-07-06 | Alfred Buchi | Speed responsive regulation of turbosupercharged engines |
US2447388A (en) * | 1944-04-10 | 1948-08-17 | Honeywell Regulator Co | Control system and apparatus |
US2454038A (en) * | 1942-10-14 | 1948-11-16 | Gen Electric | Control system for aircraft turbosuperchargers |
US2454424A (en) * | 1944-04-10 | 1948-11-23 | Honeywell Regulator Co | Compressor control system |
US2477668A (en) * | 1943-02-22 | 1949-08-02 | Honeywell Regulator Co | Control apparatus |
US2480621A (en) * | 1940-01-06 | 1949-08-30 | Gen Electric | Intake and exhaust manifold pressure-responsive control for engine superchargers |
US2480758A (en) * | 1944-01-10 | 1949-08-30 | Bendix Aviat Corp | Control mechanism for supercharged aircraft engines |
US2540916A (en) * | 1943-02-01 | 1951-02-06 | Honeywell Regulator Co | Pressure, temperature, and speed control apparatus for supercharged combustion engines |
US2544852A (en) * | 1945-10-31 | 1951-03-13 | Honeywell Regulator Co | Exhaust gas turbine with variable nozzle area for maintaining constant pressure dropthrough the turbine |
US2581334A (en) * | 1947-01-18 | 1952-01-01 | Reggio Ferdinando Carlo | Engine air induction control system |
US2896598A (en) * | 1954-05-11 | 1959-07-28 | Reggio Ferdinando Carlo | Engine air induction control apparatus |
FR2435601A1 (en) * | 1978-09-07 | 1980-04-04 | Mtu Friedrichshafen Gmbh | INTERNAL COMBUSTION ENGINE HAVING ADDITIONAL CONTROL OF THE COMPRESSED GAS COMPRESSOR |
FR2441723A1 (en) * | 1978-11-16 | 1980-06-13 | Mtu Friedrichshafen Gmbh | INTERNAL COMBUSTION ENGINE WITH SUPPLY |
-
1936
- 1936-05-28 GB GB12056/36A patent/GB479278A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2480621A (en) * | 1940-01-06 | 1949-08-30 | Gen Electric | Intake and exhaust manifold pressure-responsive control for engine superchargers |
US2423417A (en) * | 1942-09-14 | 1947-07-01 | Hobson Ltd H M | Exhaust-driven supercharger for internal-combustion engines |
US2454038A (en) * | 1942-10-14 | 1948-11-16 | Gen Electric | Control system for aircraft turbosuperchargers |
US2540916A (en) * | 1943-02-01 | 1951-02-06 | Honeywell Regulator Co | Pressure, temperature, and speed control apparatus for supercharged combustion engines |
US2477668A (en) * | 1943-02-22 | 1949-08-02 | Honeywell Regulator Co | Control apparatus |
US2444644A (en) * | 1943-07-31 | 1948-07-06 | Alfred Buchi | Speed responsive regulation of turbosupercharged engines |
US2480758A (en) * | 1944-01-10 | 1949-08-30 | Bendix Aviat Corp | Control mechanism for supercharged aircraft engines |
US2447388A (en) * | 1944-04-10 | 1948-08-17 | Honeywell Regulator Co | Control system and apparatus |
US2454424A (en) * | 1944-04-10 | 1948-11-23 | Honeywell Regulator Co | Compressor control system |
US2544852A (en) * | 1945-10-31 | 1951-03-13 | Honeywell Regulator Co | Exhaust gas turbine with variable nozzle area for maintaining constant pressure dropthrough the turbine |
US2581334A (en) * | 1947-01-18 | 1952-01-01 | Reggio Ferdinando Carlo | Engine air induction control system |
US2896598A (en) * | 1954-05-11 | 1959-07-28 | Reggio Ferdinando Carlo | Engine air induction control apparatus |
FR2435601A1 (en) * | 1978-09-07 | 1980-04-04 | Mtu Friedrichshafen Gmbh | INTERNAL COMBUSTION ENGINE HAVING ADDITIONAL CONTROL OF THE COMPRESSED GAS COMPRESSOR |
FR2441723A1 (en) * | 1978-11-16 | 1980-06-13 | Mtu Friedrichshafen Gmbh | INTERNAL COMBUSTION ENGINE WITH SUPPLY |
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