GB2183730A - Charging internal combustion reciprocating piston engine - Google Patents
Charging internal combustion reciprocating piston engine Download PDFInfo
- Publication number
- GB2183730A GB2183730A GB08625750A GB8625750A GB2183730A GB 2183730 A GB2183730 A GB 2183730A GB 08625750 A GB08625750 A GB 08625750A GB 8625750 A GB8625750 A GB 8625750A GB 2183730 A GB2183730 A GB 2183730A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- internal combustion
- cylinder
- cylinders
- 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.)
- Withdrawn
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
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/02—Engines with reciprocating-piston pumps; Engines with crankcase pumps
- F02B33/06—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps
- F02B33/22—Engines with reciprocating-piston pumps; Engines with crankcase pumps with reciprocating-piston pumps other than simple crankcase pumps with pumping cylinder situated at side of working cylinder, e.g. the cylinders being parallel
Abstract
A first piston 11 in a cylinder 10 compresses air admitted through a valve 16, a combustion chamber 12 receives the compressed air through a valve 17 and fuel from an injector 21 and a second piston 14 is driven in a cylinder 13 by expansion of the products of combustion supplied from the combustion chamber 12 through a valve 18, the exhaust gas passing out through a valve 20. The combustion chamber 12 may be provided in a slide valve 25 (Fig 4). The pistons 11, 14 may be connected to a common crankpin on a crankshaft 28 whose axis lies between the axes of the cylinders 10 and 13 (Figure 5). <IMAGE>
Description
SPECIFICATION
Internal combustion reciprocating piston engine
This invention relates to an internal combustion reciprocating piston engine and particularly to a compression ignition engine.
According to the present invention there is provided an internal combustion reciprocating piston engine comprising a first piston and cylinder for compressing gas admitted thereto, a combustion chamber for receiving gas compressed in said first piston and cylinder, meansforsupplying fuel to said combustion chamberfor combustion therein, a second piston and cylinderfor receiving the products of combustion from the combustion chamber and in which said products are expanded, and valve meansfor controlling theflow of gases into and out ofthe cylinders and the combustion chamber.
Preferably the piston of said first piston and cylinder is arranged to reach its top dead centre position in advance of the piston ofthesecond piston and cylinder.
The diameter of the second piston and cylinder is preferably largerthan that ofthe first piston and cylinder.
Some embodiments ofthe invention will now be described, by way of examples, with reference to the accompanying drawings, in which Figure 1 is a diagrammatic illustration of a first embodiment of an internal combustion engine according to the present invention, Figure2is a diagram showingtheopening and closing ofthevalves relativetothe position ofthe crankshaft angle,
Figure3 illustrates diagrammatically one form of valve means,
Figure 4illustrates diagrammatically a slide valve constituting the valve means, and
FigureS illustrates one particular arrangement of the two pistons and cylinders connected to a common crankpin.
The internal combustion reciprocating piston engine consists of a first cylinder 10 in which is
reciprocated a piston 11,a combustion chamber 12 and a second cylinder 13 in which is reciprocated a
piston 14. Air is admitted to the cylinder 10 from an air intake duct 1 via a valve 16 and the cylinder 10 communicates with the combustion chamber 12 via a valve 17. The combustion chamber 12 communicates with the cylinder 13via a valve 18and the cylinder 13 communicates with an exhaust duct 19via avalve20.
The internal combustion engine may be provided with a plurality of pairs ofcylinders 10 and 13.
The combustion chamber 12 is provided with a fuel injector 21.
Figure 2 shows the opening and closing ofthe valves 16, 17, 18, 20 relative to the position of crankshaft angle. At the starting point 00 the piston 14
is at top dead centre.
During operation of the engine air is drawn into the
cylinder 10thorough the open valve 16, with the valve
17 closed, as the piston 11 moves downwardly towards its bottom dead centre position. On the piston 11 reaching BDC the valve 16 is closed.
Upward movement of the piston 11 then compresses the change of air in the cylinder 10. The valve 17 is opened when the engine crankshaft has rotated 1800to allow the compressed airtoflow into the combustion chamber 12 and the valve 17 remains open until the piston 11 reaches its top dead centre position. The valve 18 is closed atthistime.
When the valves 17 and 18 are closed fuel is injected into the combustion chamber 12 bythe injector 21 and combustion takes place in the combustion chamber 12. The valve 18 is opened when the crankshaft has rotated 360" at which time the piston 14 is atTDC and the products of combustion are admitted into the cylinder 13. The piston 14 is driven down the cylinder 13 by the expanding gases, the valve 20 being closed at this time. When the piston 14 reaches its bottom dead centre position the valve 20 is opened so that the expanded gases are passed to the exhaust duct 19 as the piston 14 rises towards its top dead centre position. The opening and closing of the valves 16,17,18,20 relativetothecrankshaft angle and the position ofthe pistons 11 and 14is shown in figure 2.
Preferably the diameter of the cylinder 13 and piston 14 is greaterthan that of the cylinder 10 and piston 11.
The pistons 11 and 14 do not reach their top dead centre position at the same time. Piston 11 is in advance of piston 14. The amount of advance can be chosen to suit the particular application of use of the engine. This angle of advance is shown at 'A' in
Figure 2. The timing of the fuel injection will depend upon the design and will be controlled in accordance with the desired engine speed.
The angle of advance 'A' allowsforignition and combustion time. It may be possible to have an angle of ignition advance greaterthan that of a conventional internal combustion piston engine and this is desirable to give a more complete combustion before admitting the products of combustion into the cylinder 13, buttheir is a limitation on the size of the angle. Valve 17 must remain closed until the power stroke isfinished and can only be openforthetime between the end of the power stroke of piston 14 and the end of the compression stroke of piston 11, that is 1800-A0.Thistime cannot betoo small and thusA cannotbetoo large.
With the present invention the hot gases are expanded in the cylinder 13 having a largervolume than the cylinder 10 in which compression takes place and therefore they can be expanded almost to atmospheric pressure and the whole of the energy released on expansion of the gases acts on the piston
1 4thus giving good thermal efficiency and a quieter exhaust compared with conventional internal combustion reciprocating piston engines. Ignition can be timed to be before the top dead centre position of the piston 14without having to be before the top dead centre position ofthe compression piston 11. This has the advantage that the normal
loss in power of conventional engines caused by
back pressure due to ignition before top dead centre
is eliminated and smoother operation results withoutthe "knock" of conventional compression ignition engines.
In conventional engines a slight loss of power at the end ofthe power stroke is tolerated in orderto achieve better scavenging of the gases when the exhaust valve is opened before bottom dead centre ofthe piston. This is unnecessary with an engine according to the present invention.
It is possible to advance the ignition furtherthan can be done in conventional engines so as to give a longer combustion time resulting in more complete combustion, a higherfuel efficiency and less pollution oftheatmosphere.
The engine according to the preset invention is a two cylinder basicunit having a powerstrokefor each revolution of the crankshaft and therefore is comparable with a two cylinderfour stroke engine of conventional design.
As each valve 16,17, 18 and 20 operates once each revolution of the crankshaftthere is no need fora separate camshaft. The cams operating the valves can be directly on the crankshaft. This will reduce the cost of the engine, give fewer working parts, produce less friction and less mechanical noise.
The inletand outlet manifolds or ducts 15 and 19 can be simple in design as only one inlet and one outletduct is required for a two cylinder unit. Only one fuel injector is required for two cylinders and the fuel injector pump can besimple.
Thevalves 17 and 18 may have valve stemswhich pass through the combustion chamber 12 and as shown in Figure 3 they may be provided with piston ring type seals 22 and be acted upon by springs 23, the stems having recesses 24 which can be contacted by forks provided on push rods. The valve stem may be hollow and cooled by oil flowing into the valve stems.
Alternatively, as shown in Figure 4, the valve means may consist of a slide valve member 25 which incorporates the combustion chamber 12, the cylinder 10 having a port 26 and the cylinder 13 having a port 27 which are controlled by the slide valve member25. Asimple lever system may be provided to drive the slide valve 25. Also, a simple injection pump may be driven from the same lever system.
The cylinders 10 and 13 may be disposed in-line one behind the other or they may be disposed side-by-side. When the cylinders 10 and 13 are disposed side-by-side the sideways force produced by the power piston 14 and the friction and wear produced by such force can be reduced if the axis of rotation ofthe crankshaft 28 is offset, as shown in
Figure 5, so that during the power stroke ofthe piston 14the connecting rod 29 is nearly in line with the axis ofthe cylinder 13. As shown in Figure Sthe cylinders 11 and 14 are arranged in a V-shape and the connecting rods 29 and 30 are connected to the same crankpin which gives the required angle of advance, i.e. the angle of advance is the angle between the arms ofthe V-shape.
In a conventional V-engine the cylinder heads are far apart and if a narrow V-shape is chosen to bring the cylinder heads close togetherthen very long connecting rods are required if the axis ofthe crankshaft is located at the intersection of the axes of the cylinders. However with the design shown in
Figure 5 shortening ofthe connecting rods and a reduction ofthe side loading on both pistons is achieved by offsetting the axes of the crankshaft 28 from the axes ofthe cylinders 11 and 14to a point withintheV-shapeformed bythe axes ofthe cylinders.
Claims (10)
1. An internal combustion reciprocating piston engine comprising a first piston and cylinderfor compressing gas admitted thereto, a combustion chamber for receiving gas compressed in said first piston and cylinder, means for supplying fuel to said combustion chamberfor combustion therein, a second piston and cylinderfor receiving the products of combustion from the combustion chamber and in which the products are expanded, and valve means for controlling the flow of gases into and out of the cylinders and combustion chamber.
2. An internal combustion engine as claimed in claim 1, in which the piston of the first piston and cylinder is arranged to reach its top dead centre position in advance of the piston ofthe second piston and cylinder.
3. An internal combustion engine as claimed in claim 1 orclaim 2, in which the diameter ofthe second piston and cylinder is larger than that ofthe first piston and cylinder.
4. An internal combustion engine as claimed in any preceding claim in which said valve means comprise spring loaded valves having stems connected to push rods.
5. An internal combustion engine as claimed in any one of claims 1 to 3, in which said valve means comprises a slide valve in which said combustion chamber isformed.
6. An internal combustion engine as claimed in any preceding claim, in which the cylinders are disposed side-by-side in a V-shaped arrangement.
7. An internal combustion engine as claimed in claim 6, in which the connecting rods of both pistons are connected to a common crankpin.
8. An internal combustion engine as claimed in claim 6 or claim 7, in which the axis ofthecrankshaft is offset from the axes of the cylinders to a point within theV-shapeformed by the axes ofthe cylinders.
9. An internal combustion engine as claimed in any one of claims 1 to 5, in which the cylinders are disposed in-line one behind the other.
10. An internal combustion reciprocating piston engine substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB858529102A GB8529102D0 (en) | 1985-11-26 | 1985-11-26 | Dual cylinder i c engine |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8625750D0 GB8625750D0 (en) | 1986-12-03 |
GB2183730A true GB2183730A (en) | 1987-06-10 |
Family
ID=10588802
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB858529102A Pending GB8529102D0 (en) | 1985-11-26 | 1985-11-26 | Dual cylinder i c engine |
GB08625750A Withdrawn GB2183730A (en) | 1985-11-26 | 1986-10-28 | Charging internal combustion reciprocating piston engine |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB858529102A Pending GB8529102D0 (en) | 1985-11-26 | 1985-11-26 | Dual cylinder i c engine |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB8529102D0 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2413361A (en) * | 2004-04-20 | 2005-10-26 | Leslie Maidment | Fixed-displacement i.c. engine with expansion ratio greater than compression ratio |
GB2469939A (en) * | 2009-05-01 | 2010-11-03 | Keith Gordon Hall | Split-cycle engines |
RU2631179C1 (en) * | 2016-11-23 | 2017-09-19 | Анатолий Александрович Рыбаков | Method for ensuring operation of tandem two-stroke engine with energy of combustion products from common external combustion chamber |
RU2638242C1 (en) * | 2016-12-12 | 2017-12-12 | Анатолий Александрович Рыбаков | Method of providing functionment of tandemic two-total engine with energy of combustion products from general external combustion chamber and compressed air energy from general pneumatic accumulator |
RU2641998C1 (en) * | 2016-11-23 | 2018-01-23 | Анатолий Александрович Рыбаков | Method of controlling the level of charging the pneumatic accumulator of a two-motor engine with external combustion chamber |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB227467A (en) * | ||||
GB402256A (en) * | ||||
GB145329A (en) * | 1919-10-20 | 1920-07-02 | Henry Davey | Improvements in two-stroke internal combustion engines |
GB166234A (en) * | 1919-07-18 | 1921-07-11 | Allen M Rossman | Improvements relating to internal combustion engines |
GB177507A (en) * | 1921-03-24 | 1923-04-26 | Eugene Gabriel Gendreau | Improvements in or relating to internal combustion engines |
GB276453A (en) * | 1926-06-07 | 1927-09-01 | Charles Henry Thomas Alston | Improvements in or relating to two-stroke-cycle internal-combustion engines |
GB369751A (en) * | 1931-03-27 | 1932-03-31 | Bernard Stanley Maher | Improvements in compression ignition engines |
GB1300603A (en) * | 1969-03-11 | 1972-12-20 | Glenn Barton Warren | Reciprocating combustion product engine with substantially constant pressure combustion |
-
1985
- 1985-11-26 GB GB858529102A patent/GB8529102D0/en active Pending
-
1986
- 1986-10-28 GB GB08625750A patent/GB2183730A/en not_active Withdrawn
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB227467A (en) * | ||||
GB402256A (en) * | ||||
GB166234A (en) * | 1919-07-18 | 1921-07-11 | Allen M Rossman | Improvements relating to internal combustion engines |
GB145329A (en) * | 1919-10-20 | 1920-07-02 | Henry Davey | Improvements in two-stroke internal combustion engines |
GB177507A (en) * | 1921-03-24 | 1923-04-26 | Eugene Gabriel Gendreau | Improvements in or relating to internal combustion engines |
GB276453A (en) * | 1926-06-07 | 1927-09-01 | Charles Henry Thomas Alston | Improvements in or relating to two-stroke-cycle internal-combustion engines |
GB369751A (en) * | 1931-03-27 | 1932-03-31 | Bernard Stanley Maher | Improvements in compression ignition engines |
GB1300603A (en) * | 1969-03-11 | 1972-12-20 | Glenn Barton Warren | Reciprocating combustion product engine with substantially constant pressure combustion |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2413361A (en) * | 2004-04-20 | 2005-10-26 | Leslie Maidment | Fixed-displacement i.c. engine with expansion ratio greater than compression ratio |
GB2469939A (en) * | 2009-05-01 | 2010-11-03 | Keith Gordon Hall | Split-cycle engines |
RU2631179C1 (en) * | 2016-11-23 | 2017-09-19 | Анатолий Александрович Рыбаков | Method for ensuring operation of tandem two-stroke engine with energy of combustion products from common external combustion chamber |
RU2641998C1 (en) * | 2016-11-23 | 2018-01-23 | Анатолий Александрович Рыбаков | Method of controlling the level of charging the pneumatic accumulator of a two-motor engine with external combustion chamber |
RU2638242C1 (en) * | 2016-12-12 | 2017-12-12 | Анатолий Александрович Рыбаков | Method of providing functionment of tandemic two-total engine with energy of combustion products from general external combustion chamber and compressed air energy from general pneumatic accumulator |
Also Published As
Publication number | Publication date |
---|---|
GB8625750D0 (en) | 1986-12-03 |
GB8529102D0 (en) | 1986-01-02 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4860716A (en) | Multi-cylinder diesel internal combustion engine with low compression ratio in the cylinders | |
US5224460A (en) | Method of operating an automotive type internal combustion engine | |
US5265564A (en) | Reciprocating piston engine with pumping and power cylinders | |
EP1866530B1 (en) | Double piston cycle engine | |
US5431130A (en) | Internal combustion engine with stroke specialized cylinders | |
US6668809B2 (en) | Stationary regenerator, regenerated, reciprocating engine | |
US5694890A (en) | Internal combustion engine with sliding valves | |
US6065440A (en) | Internal combustion engine with binary cylinder sizing for variable power output | |
US4987864A (en) | Two cycle engine with valved pressure scavenging | |
AU638720B2 (en) | Reciprocating piston engine with pumping and power cylinders | |
US6250263B1 (en) | Dual piston cylinder configuration for internal combustion engine | |
US5596955A (en) | Internal combustion engine | |
JP2820793B2 (en) | Reciprocating engine with pump cylinder and power cylinder | |
GB2183730A (en) | Charging internal combustion reciprocating piston engine | |
US20040035377A1 (en) | Two-stroke cycle, free piston, shaft power engine | |
US5314314A (en) | Two-cycle engine compressor | |
WO1987005073A1 (en) | Supercharged two-stroke engine | |
EP0342893A1 (en) | Internal combustion engine | |
GB2264333A (en) | Compound expansion i.c.piston engine. | |
EP1230472B1 (en) | Z-engine | |
US4955333A (en) | Variable volume crankcase scavenge control | |
US3043283A (en) | Internal combustion engines | |
US20230044154A1 (en) | T-scavenged opposed piston engine | |
EP0057591A2 (en) | Internal combustion engine | |
RU2139431C1 (en) | Internal combustion engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |