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US2058528A - Internal combustion engine - Google Patents

Internal combustion engine Download PDF

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Publication number
US2058528A
US2058528A US652896A US65289633A US2058528A US 2058528 A US2058528 A US 2058528A US 652896 A US652896 A US 652896A US 65289633 A US65289633 A US 65289633A US 2058528 A US2058528 A US 2058528A
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United States
Prior art keywords
cylinder
scavenging air
frame
passages
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 - Lifetime
Application number
US652896A
Inventor
Thege Edvin Ossian Parcival
Angkvist Per Olof
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Atlas Copco AB
Original Assignee
Atlas Diesel AB
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 Atlas Diesel AB filed Critical Atlas Diesel AB
Application granted granted Critical
Publication of US2058528A publication Critical patent/US2058528A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • F02B33/44Passages conducting the charge from the pump to the engine inlet, e.g. reservoirs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/18Other cylinders
    • F02F1/22Other cylinders characterised by having ports in cylinder wall for scavenging or charging
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two

Definitions

  • 'Ihe present invention relates to internal combustion engines and has particular reference to such engines of the two stroke cycle type to which scavenging airis delivered from a receiver situated at the side of the engine.
  • the cylinder structure and frame are madeV separately, with the scavenging air passages located partly in the frame and partly in the cylinder structure, with the transverse portions of the scavenging air passages, leading from the side of the engine, situated in the frame and with the vertically extending portions of vsuch passages situated in the cylinder structure.
  • the vertically extending portions, the discharge ends of which control the direction of flow of scavenging air into the cylinders 5 0l may readily and reliably be machined or otherwise accurately formed, in a manner which is not practically possible from a manufacturing standpoint when the cylinder and frame structure is integrally cast.
  • Fig. 3 is a section taken on the line A-B of Fig. l; and 50 Fig. 3a is a section taken on the line C-D of Fig. 1.
  • reference numeral I designates the outer cylinder part having the cylinder liner 2 and the cooling jacket space 3 between the liner and the outer wall of the cylinder part I.
  • the liner 2 extends downwardly beyond the lower face of the outer cylinder part I sufcently to guide the piston 4.
  • the cylinder part I is cast separately fromand supported by a frame 5.
  • the line of partition between these parts is indicated at 6 and these parts are bolted together by bolts (not shown).
  • the frame carries the bearings I and the crank shaft 8, the latter being connected to piston 4 by means of the connecting rod 9.
  • the scavenging air passes from a receiver pipe IU through an automatic admission valve II, for example, of the kind disclosed in U. S. Patent No. 1,672,436, and from this valve to the scavenging air passages indicated generally at I2.
  • an automatic admission valve II for example, of the kind disclosed in U. S. Patent No. 1,672,436, and from this valve to the scavenging air passages indicated generally at I2.
  • the passages I2 are formed partly in the frame 5 and partly in the cylinder structure.
  • the parts of the channels located in the cylinder structure extend in substantially vertical direction while the parts of the passages I2 located in the frame extend transversely thereof.
  • the vertical and transverse parts of the passages. communicate with each other at the line of partition 6 between the cylinder and frame parts.
  • the vertical portions of the scavenging air passages are disposed at the opposite transverse side portions of the cylinder, as seen more clearly in Fig. 2, and at their upper ends terminate in the oblique and oppositely disposed ports I3.
  • These ports are advantageously arranged in groups as shown in Fig. 3 so that the air delivered therefrom will be deflected upwardly in the lateral side portion of the cylinder opposite the exhaust ports I4 which communicate with the exhaust pipe I5, the direction of ilow of the scavenging air in the cylinder being indicated by the arrows in Fig. 1.
  • the lower ends of the scavenging air passages in the cylinder communicate with the inner end of a transverse passage in the frame which communicates at its outer end with the receiver pipe I0.
  • the outer cylinder part I and the liner 2 may be and preferably are of cast iron having suicient strength to withstand the combustion chamber pressures.
  • the frame may be cast of the same or a different metal, for example, some light alloy, or may be fabricated of welded plate structure. The latter can readily be done since there is no cooling jacket structure necessary in the frame. By this arrangement the engine construction as a whole may be made comparatively very light.
  • cylinder structure providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of the cylinder, a series of scavenging air ports distributed in and limited to the transverse side portions of the cylinder, said ports being arranged to direct scavenging air in a path of upward flow substantially confined to the lateral half of the cylinder opposite the lateral half in which said exhaust ports are located, upwardly extending scavenging air passages in said cylinder structure at the transverse sides thereof, said passages communicating at their upper ends with said scavenging ports and a transversely extending passage in said frame for said scavenging air, said transversely extending passage having an inlet end at one lateral side of the engine and having its outlet end registering with the lower ends of said scavenging air passages in said cylinder structure.
  • cylinder structure comprising an outer cylinder part and a separable cylinder liner providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of said liner, a series of scavenging air ports distributed in and limited to the transverse side portions of the liner, said scavenging air ports being arranged in mutually opposed groups for directing the scavenging air in a substantially vertical upward path of flow substantially confined to the lateral half of the cylinder opposite the lateral side in which the exhaust ports are located, separate scavenging air passages formed in said outer cylinder part in the opposite transverse side portions of said part, said air passages registering at their upper ends with said scavenging air ports, and a transverse scavenging air passage formed in said frame and extending inwardly from one lateral side of the frame, the inner end of said transverse air passage registering with the lower ends of the air passages in
  • cylinder structure comprising an outer cylinder part and a separable cylinder liner providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of said liner, an exhaust conduit secured to said outer cylinder part at the same lateral side thereof as that of said exhaust ports, there being an exhaust passage in said cylinder part for placing said exhaust pipe in communication with said exhaust ports, a series of scavenging air ports distributed in and limited to the transverse side portions of said liner, said scavenging air ports being arranged to direct scavenging air in a generally vertical upward path of now in and substantially limited to the lateral half of the cylinder opposite the side where said exhaust ports are located, separate scavenging air passages formed in said outer cylinder part and extending upwardly in each of the transverse side portions of said cylinder part, said passages registering at their upper ends with said scavenging ports, and a transverse scavenven

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

Oct. 21, 1936, Er P. THEGE ET A1. 2,058,528 INTERNAL coMBU's'TIoN ENGINE Fild Jan.r 21, 14935 Patented Get. 27, 1936 UNiTso srnrss sArsNr ori-*ics INTERNAL coMBUsTIoN ENGINE poration of Sweden Application January 21, 1933, Serial No. 652,896 In Sweden December 29, 1932 4 claims.
'Ihe present invention relates to internal combustion engines and has particular reference to such engines of the two stroke cycle type to which scavenging airis delivered from a receiver situated at the side of the engine.
In engines having this general form of construction, it is dicult to secure proper dimensions and curvature of the scavenging air passages when the cylinder and frame structure oi' the engine are cast integrally, and this is particularly true with multiple cylinder engines.
It is a principal object of the present invention to improve upon prior forms of construction of engines of this kind so as to readily and reliably secure the desired accuracy of direction of flow of the scavenging air into the engine cylinders, with a construction that is relatively cheap and provides for ease of manufacture.
To thisend the cylinder structure and frame are madeV separately, with the scavenging air passages located partly in the frame and partly in the cylinder structure, with the transverse portions of the scavenging air passages, leading from the side of the engine, situated in the frame and with the vertically extending portions of vsuch passages situated in the cylinder structure. By this means, the vertically extending portions, the discharge ends of which control the direction of flow of scavenging air into the cylinders 5 0l may readily and reliably be machined or otherwise accurately formed, in a manner which is not practically possible from a manufacturing standpoint when the cylinder and frame structure is integrally cast.
`The above general object and other and more detailed objects of the invention may best be understood from a consideration ofthe ensuing portion of this specification in which is described by way of example a preferred form of` of Fig. 1;
Fig. 3 is a section taken on the line A-B of Fig. l; and 50 Fig. 3a is a section taken on the line C-D of Fig. 1.
Referring now to the drawing, reference numeral I designates the outer cylinder part having the cylinder liner 2 and the cooling jacket space 3 between the liner and the outer wall of the cylinder part I. The liner 2 extends downwardly beyond the lower face of the outer cylinder part I sufcently to guide the piston 4.
The cylinder part I is cast separately fromand supported by a frame 5. The line of partition between these parts is indicated at 6 and these parts are bolted together by bolts (not shown).
The frame carries the bearings I and the crank shaft 8, the latter being connected to piston 4 by means of the connecting rod 9.
In the embodiment of the invention illustrated,` the scavenging air passes from a receiver pipe IU through an automatic admission valve II, for example, of the kind disclosed in U. S. Patent No. 1,672,436, and from this valve to the scavenging air passages indicated generally at I2.
The passages I2 are formed partly in the frame 5 and partly in the cylinder structure. The parts of the channels located in the cylinder structure extend in substantially vertical direction while the parts of the passages I2 located in the frame extend transversely thereof. The vertical and transverse parts of the passages. communicate with each other at the line of partition 6 between the cylinder and frame parts.
In the preferred arrangement shown, the vertical portions of the scavenging air passages are disposed at the opposite transverse side portions of the cylinder, as seen more clearly in Fig. 2, and at their upper ends terminate in the oblique and oppositely disposed ports I3. These ports are advantageously arranged in groups as shown in Fig. 3 so that the air delivered therefrom will be deflected upwardly in the lateral side portion of the cylinder opposite the exhaust ports I4 which communicate with the exhaust pipe I5, the direction of ilow of the scavenging air in the cylinder being indicated by the arrows in Fig. 1.
The lower ends of the scavenging air passages in the cylinder communicate with the inner end of a transverse passage in the frame which communicates at its outer end with the receiver pipe I0.
With the constructions illustrated, the outer cylinder part I and the liner 2 may be and preferably are of cast iron having suicient strength to withstand the combustion chamber pressures. The frame may be cast of the same or a different metal, for example, some light alloy, or may be fabricated of welded plate structure. The latter can readily be done since there is no cooling jacket structure necessary in the frame. By this arrangement the engine construction as a whole may be made comparatively very light.
Further with the arrangment shown, it will be evident that the provision of scavenging air passages in the cylinder structure having the required degree of accuracy to introduce the scavenging air in precisely the direction desired may readily be accomplished since these passages may be finished before the engine is assembled and while the portions of the passages which are controlling as to the direction of introduction of the scavenging air are readily accessible for machining or other operations that may be desired.
While for purposes of illustration only a single cylinder engine has been shown, it will be appreciated that the invention is equally applicable to multiple cylinder engines and that changes and modilications in the form of construction shown by way of illustration can be made without departing from the invention, the scope of which is defined in the appended claims.
We claim:
l. In an internal combustion engine of the two stroke cycle type, cylinder structure providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of the cylinder, a series of scavenging air ports distributed in and limited to the transverse side portions of the cylinder, said ports being arranged to direct scavenging air in a path of upward flow substantially confined to the lateral half of the cylinder opposite the lateral half in which said exhaust ports are located, upwardly extending scavenging air passages in said cylinder structure at the transverse sides thereof, said passages communicating at their upper ends with said scavenging ports and a transversely extending passage in said frame for said scavenging air, said transversely extending passage having an inlet end at one lateral side of the engine and having its outlet end registering with the lower ends of said scavenging air passages in said cylinder structure.
2. In an internal combustion engine of the two stroke cycle type, cylinder structure providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of the cylinder, a series of scavenging air ports arranged in and limited to the transverse side wall portions of the cylinder, said scavenging air ports being arranged in mutually opposed groups for directing the air in a substantially vertical path of flow upwardly in the lateral half of the cylinder opposite the lateral side in which the exhaust ports are located, scavenging air passages in the cylinder structure at the transverse sides of the cylinder, said passages terminating at their upper ends at said scavenging ports, and a transversely extending scavenging air passage in said frame registering at its inner end with the lower ends of the scavenging air passages in the cylinder, and at its outer end terminating at the lateral side of the engine.
3. In an internal combustion engine of the two stroke cycle type, cylinder structure comprising an outer cylinder part and a separable cylinder liner providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of said liner, a series of scavenging air ports distributed in and limited to the transverse side portions of the liner, said scavenging air ports being arranged in mutually opposed groups for directing the scavenging air in a substantially vertical upward path of flow substantially confined to the lateral half of the cylinder opposite the lateral side in which the exhaust ports are located, separate scavenging air passages formed in said outer cylinder part in the opposite transverse side portions of said part, said air passages registering at their upper ends with said scavenging air ports, and a transverse scavenging air passage formed in said frame and extending inwardly from one lateral side of the frame, the inner end of said transverse air passage registering with the lower ends of the air passages in said cylinder part.
4. In an internal combustion engine of the two stroke cycle type, cylinder structure comprising an outer cylinder part and a separable cylinder liner providing a working cylinder, a frame separate from and supporting said cylinder structure, a series of exhaust ports located in one lateral side portion of said liner, an exhaust conduit secured to said outer cylinder part at the same lateral side thereof as that of said exhaust ports, there being an exhaust passage in said cylinder part for placing said exhaust pipe in communication with said exhaust ports, a series of scavenging air ports distributed in and limited to the transverse side portions of said liner, said scavenging air ports being arranged to direct scavenging air in a generally vertical upward path of now in and substantially limited to the lateral half of the cylinder opposite the side where said exhaust ports are located, separate scavenging air passages formed in said outer cylinder part and extending upwardly in each of the transverse side portions of said cylinder part, said passages registering at their upper ends with said scavenging ports, and a transverse scavenging air passage in said frame, the last mentioned passage extending inwardly from the lateral side of the engine at which said exhaust pipe is located and registering at its inner end With the lower ends of the scavenging air passages in said cylinder part.
EDVIN OSSIAN PARCIVAL THEGE. PER OLOF NGKVIST.
US652896A 1932-12-29 1933-01-21 Internal combustion engine Expired - Lifetime US2058528A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2728333A (en) * 1950-04-22 1955-12-27 Gen Motors Corp Engine exhausting, scavenging, and charging system
US2736302A (en) * 1950-01-11 1956-02-28 Kloeckner Humboldt Deutz Ag Air-cooled two-cycle internal-combustion engines
US2760469A (en) * 1953-07-31 1956-08-28 Kremser Johann Fluid-cooled two-stroke cycle internal combustion engine with individually mounted cylinders
US4515112A (en) * 1981-10-28 1985-05-07 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder block

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2736302A (en) * 1950-01-11 1956-02-28 Kloeckner Humboldt Deutz Ag Air-cooled two-cycle internal-combustion engines
US2728333A (en) * 1950-04-22 1955-12-27 Gen Motors Corp Engine exhausting, scavenging, and charging system
US2760469A (en) * 1953-07-31 1956-08-28 Kremser Johann Fluid-cooled two-stroke cycle internal combustion engine with individually mounted cylinders
US4515112A (en) * 1981-10-28 1985-05-07 Toyota Jidosha Kabushiki Kaisha Aluminum alloy cylinder block

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