US1976286A - Cam gear for internal combustion engines - Google Patents
Cam gear for internal combustion engines Download PDFInfo
- Publication number
- US1976286A US1976286A US600517A US60051732A US1976286A US 1976286 A US1976286 A US 1976286A US 600517 A US600517 A US 600517A US 60051732 A US60051732 A US 60051732A US 1976286 A US1976286 A US 1976286A
- Authority
- US
- United States
- Prior art keywords
- compression
- internal combustion
- cam gear
- piston
- combustion engines
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title description 14
- 238000007906 compression Methods 0.000 description 27
- 230000006835 compression Effects 0.000 description 26
- 239000000446 fuel Substances 0.000 description 9
- 230000002269 spontaneous effect Effects 0.000 description 8
- 239000000203 mixture Substances 0.000 description 7
- 230000007704 transition Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 241000218652 Larix Species 0.000 description 1
- 235000005590 Larix decidua Nutrition 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000002000 scavenging effect Effects 0.000 description 1
Images
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
- F02B75/00—Other engines
- F02B75/28—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
- F02B75/282—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders the pistons having equal strokes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F01B3/04—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis the piston motion being transmitted by curved surfaces
- F01B3/045—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis the piston motion being transmitted by curved surfaces by two or more curved surfaces, e.g. for two or more pistons in one cylinder
-
- 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
- F02B75/26—Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18056—Rotary to or from reciprocating or oscillating
- Y10T74/18296—Cam and slide
- Y10T74/18304—Axial cam
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18056—Rotary to or from reciprocating or oscillating
- Y10T74/18296—Cam and slide
- Y10T74/18304—Axial cam
- Y10T74/18312—Grooved
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18056—Rotary to or from reciprocating or oscillating
- Y10T74/18296—Cam and slide
- Y10T74/18304—Axial cam
- Y10T74/18312—Grooved
- Y10T74/1832—Multiple screw
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2101—Cams
Definitions
- the invention relates to internal combustion engines (for I example explosion-Diesel twostroke cycle or multi-fstroke cycle engines) in which the piston movement is converted into the rotary motion of the driving shaft not by crank gear but by cam gear.
- internal combustion engines for I example explosion-Diesel twostroke cycle or multi-fstroke cycle engines
- cam gear It is a particular advantage of cam gear that the course of the piston movement is not confined to that determined bythe crank gear, but that it is possible by suitable configuration of the cam tracks to move the piston as desired during one revolution of the engine shaft, for example, to accelerate the movement of the piston, to retard it or even temporarily to stop it entirely.
- the invention utilizes this advantage, in such internal combustion engines, in which the fuel is supplied during or before the compression of the air for combustion for the purpose of securing spontaneous ignition of the fuel mixture at the correct instant instead of by electrical ignition or by the incandescent method of ignition.
- This is effected by appropriate configuration of the cam track (compression cam curve) provided on the cam, which cam track effects the compression of the mixture.
- This compression cam curve is so constructed according to the invention that the piston moved thereby first of all precompresses the fuel mixture to an extentsuch that spontaneous ignition does not yet occur, while the compression curve rises very steeply towards its end, thereby effecting 'such rapid and high compression of the fuel mixture that spontaneous ignition of the latter occurs.
- the new type of compression process just described is also applicable in the case of a Diesel engine in which the fuel is only admitted at the end of the high compression of the fresh air. In this case, fresh air is precompressed. first of all, but the rapid and high compression of the fresh air occurring towards the end of the compression curve then brings the said air intensively to a state of incandescence, hence considerably promoting the spontaneous ignition of the fuel which is now admitted.
- Figure- 1 shows in axial section the cam gear applied to a multi-cylinder tw -stroke cycle internal combustion engine with pistons running counter to one another.
- Figure 2 shows on a larger scale a compression and a working curve in development after and the position of the working piston spontaneous ignition of the fuel has occurred.
- 1 and 2 are the pistons
- 3 is the cam mounted on the driving shaft 4.
- the pistons run on the tracks of the said cam by means of rollers '7 or slide shoes.
- the admission and exhaust ports are shown at 5 and 6 respectively.
- a piston operated cam gear for internal combustion engines of the Diesel two-stroke cycle and multi-stroke cycle type including a cam track having compression and working portions
- the part of the compression portion immediately adjacent the working portion having a steeper inclination than the remaining compression portion whereby to effect a sudden increase of pressure at a more rapid rate than at the beginning of the compression period.
- a piston operated cam gear for internal vided with a substantially rectilinear transition portion between the compression and working portions.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Valve Device For Special Equipments (AREA)
Description
Oct. 9, 1934. A. KREIDLER 1,976,236
CAM GEAR FOR INTERNAL COMBUSTION ENGINES A Filed larch 22, 1932 2 Sheets-Sheet l Z? flreiquew Jzwezziar:
Oct. 9, 1934. KREIDLER 1,976,286
CAM GEAR FOR INTERNAL COMBUSTION ENGINES Filed March 22, 1932 2 Sheets-Sheet 2 Registered Oct. 9, 1934 UNITED STATES CAM GEAR FOR INTERNAL COMBUSTION ENGINES Anton Kreidler, Stuttgart, Germany Application March 22,1932, Serial No. 600,517 In Austria April 15, 1931 2 Claims.
The invention relates to internal combustion engines (for I example explosion-Diesel twostroke cycle or multi-fstroke cycle engines) in which the piston movement is converted into the rotary motion of the driving shaft not by crank gear but by cam gear.
It is a particular advantage of cam gear that the course of the piston movement is not confined to that determined bythe crank gear, but that it is possible by suitable configuration of the cam tracks to move the piston as desired during one revolution of the engine shaft, for example, to accelerate the movement of the piston, to retard it or even temporarily to stop it entirely.
The invention utilizes this advantage, in such internal combustion engines, in which the fuel is supplied during or before the compression of the air for combustion for the purpose of securing spontaneous ignition of the fuel mixture at the correct instant instead of by electrical ignition or by the incandescent method of ignition. This is effected by appropriate configuration of the cam track (compression cam curve) provided on the cam, which cam track effects the compression of the mixture. This compression cam curve is so constructed according to the invention that the piston moved thereby first of all precompresses the fuel mixture to an extentsuch that spontaneous ignition does not yet occur, while the compression curve rises very steeply towards its end, thereby effecting 'such rapid and high compression of the fuel mixture that spontaneous ignition of the latter occurs.
The new type of compression process just described is also applicable in the case of a Diesel engine in which the fuel is only admitted at the end of the high compression of the fresh air. In this case, fresh air is precompressed. first of all, but the rapid and high compression of the fresh air occurring towards the end of the compression curve then brings the said air intensively to a state of incandescence, hence considerably promoting the spontaneous ignition of the fuel which is now admitted.
Whereas in crank engines the piston only slowly increases compression towards the end of thecompression stroke, and the resulting heat of compression is partly absorbed unused by the cylinder walls, the latter occurrence is considerably diminished according to the invention by the rapid high compression at the end of the compression stroke.
Since, in the case of the cam gear, the transition from the compression curve to the working curve is very rapid, there is the disadvantage, particularly in the case of high speed engines, that this change of curve proceeds more rapidly than the time taken for combustion to develop Consequently, the working piston and hence the working curve is not under the desired working pressure from the beginning of the said curve. This disadvantage is obviated according to the invention by providing between the end of the compression curve and the beginning of the working curve on the cam a substantially rectilinear transition portion which practically stops the working piston until the combustion initiated by the spontaneous ignition has been fully developed. This arrangement corresponds to the known pro-ignition in internal combustion engines. 7
One' constructional example of a cam gear according to the invention as applied to an internal combustion engine is shown in the accom-' panying drawings, wherein:
Figure- 1 shows in axial section the cam gear applied to a multi-cylinder tw -stroke cycle internal combustion engine with pistons running counter to one another.
Figure 2shows on a larger scale a compression and a working curve in development after and the position of the working piston spontaneous ignition of the fuel has occurred.
Referring to the drawings, 1 and 2 are the pistons, 3 is the cam mounted on the driving shaft 4. The pistons run on the tracks of the said cam by means of rollers '7 or slide shoes. The admission and exhaust ports are shown at 5 and 6 respectively.
In Figure 2, the compression curve is shown at 15, 16 being its steeply rising portion at the end, d-e the connection portion between compression and working curve and 1'? the working curve.
In Figure 1, the pistons 1 and 2 are at the instant at which spontaneous ignition has occurred. (See also Figure 2.) The pistons in moving outwardly run along the connecting distance H and by their pressure upon the steep working curve 17 situated opposite them set the driving shaft 4 in rotation. The piston. 1, now 1a passes the exhaust port 6 and uncovers it for the most part, and the combustion residues escape. Piston 2 at this instant still covers the inlet. Both pistons move further. Piston 1 passes the exhaust port and piston 2 uncovers the inlet port, so that the fresh gas mixture or the scavenging air can enter the cylinder. During the further course of the rotation of the cam, pistol 1 closes the exhaust 6 and then piston 2 closes the inlet 5. Both pistons are now on the compression curves 15, Fig. 2, which move them towards the middle of the cylinder to compress the contents of the cylinder. On passing over the steep end portion 16 of the compression curve, a rapid compression of the fuel mixture takes place in cooperation with the piston 2, which is rapidly moved forward at the same time from the other end, thereby eflecting spontaneous ignition of the fuel mixture, whereupon the working of the pistons is repeated in the manner described in the foregoing.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is: p
1. A piston operated cam gear for internal combustion engines of the Diesel two-stroke cycle and multi-stroke cycle type including a cam track having compression and working portions,
the part of the compression portion immediately adjacent the working portion having a steeper inclination than the remaining compression portion whereby to effect a sudden increase of pressure at a more rapid rate than at the beginning of the compression period.
2. A piston operated cam gear for internal vided with a substantially rectilinear transition portion between the compression and working portions.
ANTON KRElDLER.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT377614X | 1931-04-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1976286A true US1976286A (en) | 1934-10-09 |
Family
ID=3673076
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US600517A Expired - Lifetime US1976286A (en) | 1931-04-15 | 1932-03-22 | Cam gear for internal combustion engines |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US1976286A (en) |
| FR (1) | FR732629A (en) |
| GB (1) | GB377614A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2532106A (en) * | 1946-12-06 | 1950-11-28 | Korsgren Theodore Yngve | Multiple opposed piston engine |
| US3314403A (en) * | 1964-02-07 | 1967-04-18 | Participations Soc Et | Autogenerators |
| US5031581A (en) * | 1988-08-29 | 1991-07-16 | Powell Brian L | Crankless reciprocating machine |
| US5743220A (en) * | 1996-07-29 | 1998-04-28 | Guarner-Lans; Enrique Eduardo | Internal combustion engine with central chamber |
| US6899065B2 (en) | 2002-04-30 | 2005-05-31 | Thomas Engine Company | Radial-valve gear apparatus for barrel engine |
| US6986342B2 (en) | 1999-03-23 | 2006-01-17 | Thomas Engine Copany | Homogenous charge compression ignition and barrel engines |
| AT501400A1 (en) * | 2004-12-22 | 2006-08-15 | Walter Ing Falkinger | INCREASING EFFICIENCY IN HUB PISTON ENGINES |
| US7469662B2 (en) | 1999-03-23 | 2008-12-30 | Thomas Engine Company, Llc | Homogeneous charge compression ignition engine with combustion phasing |
| US8046299B2 (en) | 2003-10-15 | 2011-10-25 | American Express Travel Related Services Company, Inc. | Systems, methods, and devices for selling transaction accounts |
| US20200141312A1 (en) * | 2018-11-07 | 2020-05-07 | Hts Llc | Opposed piston engine |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2376719A (en) * | 2001-04-27 | 2002-12-24 | Martin Leonard Stanley Flint | Engine with two wave barrel cam having dwell periods between rise and return and return and rise profiles |
| GB2477272B (en) | 2010-01-27 | 2014-06-25 | Two Stroke Developments Ltd | Internal combustion engine comprising piston dwell mechanism |
| GB2511781A (en) * | 2013-03-12 | 2014-09-17 | Two Stroke Developments Ltd | Improved opposed piston engine |
-
1932
- 1932-03-04 FR FR732629D patent/FR732629A/en not_active Expired
- 1932-03-10 GB GB7235/32A patent/GB377614A/en not_active Expired
- 1932-03-22 US US600517A patent/US1976286A/en not_active Expired - Lifetime
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2532106A (en) * | 1946-12-06 | 1950-11-28 | Korsgren Theodore Yngve | Multiple opposed piston engine |
| US3314403A (en) * | 1964-02-07 | 1967-04-18 | Participations Soc Et | Autogenerators |
| US5031581A (en) * | 1988-08-29 | 1991-07-16 | Powell Brian L | Crankless reciprocating machine |
| US5743220A (en) * | 1996-07-29 | 1998-04-28 | Guarner-Lans; Enrique Eduardo | Internal combustion engine with central chamber |
| US6986342B2 (en) | 1999-03-23 | 2006-01-17 | Thomas Engine Copany | Homogenous charge compression ignition and barrel engines |
| US7469662B2 (en) | 1999-03-23 | 2008-12-30 | Thomas Engine Company, Llc | Homogeneous charge compression ignition engine with combustion phasing |
| US6899065B2 (en) | 2002-04-30 | 2005-05-31 | Thomas Engine Company | Radial-valve gear apparatus for barrel engine |
| US8046299B2 (en) | 2003-10-15 | 2011-10-25 | American Express Travel Related Services Company, Inc. | Systems, methods, and devices for selling transaction accounts |
| AT501400A1 (en) * | 2004-12-22 | 2006-08-15 | Walter Ing Falkinger | INCREASING EFFICIENCY IN HUB PISTON ENGINES |
| US20200141312A1 (en) * | 2018-11-07 | 2020-05-07 | Hts Llc | Opposed piston engine |
| US10947846B2 (en) * | 2018-11-07 | 2021-03-16 | Hts Llc | Opposed piston engine |
| US11401812B2 (en) | 2018-11-07 | 2022-08-02 | Hts Llc | Opposed piston engine |
Also Published As
| Publication number | Publication date |
|---|---|
| FR732629A (en) | 1932-09-23 |
| GB377614A (en) | 1932-07-28 |
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