DE1293784B - Rotary piston internal combustion engine - Google Patents
Rotary piston internal combustion engineInfo
- Publication number
- DE1293784B DE1293784B DEC26419A DEC0026419A DE1293784B DE 1293784 B DE1293784 B DE 1293784B DE C26419 A DEC26419 A DE C26419A DE C0026419 A DEC0026419 A DE C0026419A DE 1293784 B DE1293784 B DE 1293784B
- Authority
- DE
- Germany
- Prior art keywords
- combustion engine
- internal combustion
- rotary piston
- piston internal
- partition walls
- 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.)
- Pending
Links
- 238000002485 combustion reaction Methods 0.000 title claims description 8
- 238000005192 partition Methods 0.000 claims description 9
- 239000007789 gas Substances 0.000 description 5
- 230000002349 favourable effect Effects 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000007906 compression Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/36—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having both the movements defined in sub-groups F01C1/22 and F01C1/24
-
- 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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- 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
- F02B2730/00—Internal-combustion engines with pistons rotating or oscillating with relation to the housing
- F02B2730/05—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with pistons intermeshing as gear wheels; with helicoidal rotors
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
Die Erfindung bezieht sich auf eine innenachsige Rotationskolben-Brennkraftmaschine mit einem Mantel, der in radialer Richtung nach innen sich erstreckende Trennwände aufweist, die Arbeitskammern begrenzen und mit zwei an einer Nabe exzentrisch angeordneten, drehbar gelagerten Kolben, die achsnahe und achsferne Zonen aufweisen.The invention relates to an internal-axis rotary piston internal combustion engine with a jacket, the partition walls extending inward in the radial direction has, limit the working chambers and with two eccentrically arranged on a hub, rotatably mounted pistons, which have zones close to and away from the axis.
Soweit solche Maschinen bereits bekannt geworden sind, z. B. durch die USA.-Patentschrift 2 478 924, haben jedoch die Arbeitskammern eine komplizierte Form, und es entstehen zerklüftete Verbrennungs-und Expansionsräume. Aufgabe der Erfindung ist es nun, eine solche Maschine so auszubilden, daß die Form der Arbeitskammern möglichst einfach wird und gleichzeitig dafür zu sorgen, daß bei einer für den Wirkungsgrad möglichst günstigen Ausbildung der Kolben gleichzeitig eine hinreichende Dichtung bei möglichst geringer Reibung erzielt wird.As far as such machines are already known, z. B. by U.S. Patent 2,478,924, however, the working chambers are complicated Form, and jagged combustion and expansion spaces are created. Task of The invention is now to design such a machine so that the shape of the working chambers is as simple as possible and at the same time to ensure that one for the efficiency as favorable as possible design of the piston at the same time an adequate seal is achieved with the lowest possible friction.
Diese Aufgabe wird dadurch gelöst, daß jeder Kolben im Querschnitt doppel-T-förmig ausgebildet ist, daß die Arbeitskammern im Querschnitt kreissektorförmig ausgebildet sind und daß die die Arbeitskammern begrenzenden Flächen der Trennwände in die Mittelachse der Rotationskolben-Brennkraftmaschine schneidenden Axialebenen liegen.This object is achieved in that each piston in cross section Is designed double-T-shaped that the working chambers in cross-section in the shape of a sector of a circle are formed and that the working chambers delimiting surfaces of the partition walls Axial planes intersecting the central axis of the rotary piston internal combustion engine lie.
Im folgenden ist an Hand der Zeichnung ein Ausführungsbeispiel für eine Rotationskolben-Brennkraftmaschine gemäß der Erfindung beschrieben. Die Zeichnung zeigt die Maschine im Querschnitt.In the following, an exemplary embodiment for described a rotary piston internal combustion engine according to the invention. The drawing shows the machine in cross section.
Innerhalb des Mantels 1 ist um dessen Mittelachse 10 die Nabe 2 drehbar gelagert, in der zwei Ausnehmungen 11,12 vorgesehen sind. In den Ausnehmungen 11,12 sind die doppel-T-förmigen Kolben 3, 4 gleichfalls drehbar angeordnet, deren Durchmesser gerade halb so groß ist, wie der Innendurchmesser des Mantels 1. Der von dem Mantel 1 umschlossene Innenraum ist durch die Trennwände 5, 5' in vier Sektoren geteilt, deren jeder eine Arbeitskammer 9 bildet. Die Trennwände 5, 5' schließen den Auslaßkanal 7 ein, wobei die Trennwand 5' in der Mitte etwas kürzer ist als seitlich, so daß ein Durchlaß 13 für die verbrannten Gase entsteht, der die Arbeitskammer 9 mit dem Auslaßkanal verbindet. Die Flächen der die Kammern 9 begrenzenden Trennwände 5, 5' liegen in Achsialebenen, die sich in der Mittelachse 10 der Maschine schneiden. Da sich die Kanten der doppel-T-förmigen Kolben 3, 4 gleichfalls in solchen Ebenen bewegen, ist auf diese Weise eine weitgehende Dichtung der Arbeitskammern 9 bei geringster Reibung gewährleistet, während gleichzeitig die Arbeitskammern eine einfache, nicht zerklüftete Form aufweisen. Auch wird sowohl für den Kompressionsvorgang als auch für die Entspannung der verbrannten Gase eine besonders günstige Angriffsrichtung der auftretenden Kräfte an der Nabe erreicht.Within the shell 1 , the hub 2 is rotatably mounted about its central axis 10, in which two recesses 11, 12 are provided. In the recesses 11, 12 the double-T-shaped pistons 3, 4 are also rotatably arranged, the diameter of which is just half as large as the inner diameter of the jacket 1 'Divided into four sectors, each of which forms a working chamber 9. The partition walls 5, 5 'enclose the outlet channel 7, the partition wall 5' being slightly shorter in the middle than on the side, so that a passage 13 for the burned gases is created which connects the working chamber 9 to the outlet channel. The surfaces of the partition walls 5, 5 ′ delimiting the chambers 9 lie in axial planes which intersect in the central axis 10 of the machine. Since the edges of the double-T-shaped pistons 3, 4 also move in such planes, this ensures extensive sealing of the working chambers 9 with minimal friction, while at the same time the working chambers have a simple, non-jagged shape. A particularly favorable direction of attack of the forces occurring on the hub is also achieved both for the compression process and for the expansion of the burnt gases.
In der Nabe 2 sind die Einlaßkanäle 6 vorgesehen, durch die das explosive Gasgemisch den Arbeitskammern 9 zugeführt werden kann; der öffnungs-und Schließungszeitpunkt für den Gaseintritt werden beispielsweise selbsttätig durch die Nabe 2 gesteuert. Die Bohrungen 8 dienen zum Einsetzen der Zündkerzen. An Stelle eines Gasgemisches kann auch Luft zugeführt werden, die alsdann in den Arbeitskammern 9 komprimiert wird und in die mittels in den Bohrungen 8 an Stelle von Zündkerzen eingesetzter Einspritzdüsen ein beispielsweise flüssiger Brennstoff eingespritzt wird.In the hub 2, the inlet channels 6 are provided through which the explosive Gas mixture can be fed to the working chambers 9; the opening and closing times for the gas inlet are controlled automatically by the hub 2, for example. The holes 8 are used to insert the spark plugs. Instead of a gas mixture Air can also be supplied, which then compresses in the working chambers 9 is and inserted into the means in the bores 8 instead of spark plugs Injection nozzles, for example, a liquid fuel is injected.
Claims (2)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7117A FR1407651A (en) | 1961-03-22 | 1961-03-22 | Rotary combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1293784B true DE1293784B (en) | 1969-04-30 |
Family
ID=8572051
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEC26419A Pending DE1293784B (en) | 1961-03-22 | 1962-03-06 | Rotary piston internal combustion engine |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE1293784B (en) |
FR (1) | FR1407651A (en) |
GB (1) | GB992126A (en) |
SE (1) | SE308427B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4274374A (en) * | 1979-01-10 | 1981-06-23 | Lee Choong G | Air-cooled rotary internal combustion engine |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR343064A (en) * | 1904-05-11 | 1904-09-24 | Jean Dautheville | Rotary motor |
FR443334A (en) * | 1912-04-27 | 1912-09-21 | Henri Auguste Pruvost | Four-stroke rotary explosion engine |
US1047357A (en) * | 1912-10-19 | 1912-12-17 | Silas S Williams | Rotary engine. |
AT85773B (en) * | 1917-05-19 | 1921-10-10 | Charles Bruce And Company Ltd | Internal combustion engine with a rotating housing provided with piston vanes. |
US2478924A (en) * | 1946-09-19 | 1949-08-16 | Getty S Johnson | Rotary internal-combustion engine |
CH321163A (en) * | 1953-11-11 | 1957-04-30 | Bopp & Reuther Gmbh | Rotary piston machine |
US2958312A (en) * | 1957-06-25 | 1960-11-01 | Shimomura Kenji | Rotary internal combustion engine |
DE1094269B (en) * | 1959-02-11 | 1960-12-08 | Arno Fischer | Volumetric power machine or device |
-
1961
- 1961-03-22 FR FR7117A patent/FR1407651A/en not_active Expired
-
1962
- 1962-03-06 DE DEC26419A patent/DE1293784B/en active Pending
- 1962-03-19 SE SE3014/62A patent/SE308427B/xx unknown
- 1962-03-19 GB GB10410/62A patent/GB992126A/en not_active Expired
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR343064A (en) * | 1904-05-11 | 1904-09-24 | Jean Dautheville | Rotary motor |
FR443334A (en) * | 1912-04-27 | 1912-09-21 | Henri Auguste Pruvost | Four-stroke rotary explosion engine |
US1047357A (en) * | 1912-10-19 | 1912-12-17 | Silas S Williams | Rotary engine. |
AT85773B (en) * | 1917-05-19 | 1921-10-10 | Charles Bruce And Company Ltd | Internal combustion engine with a rotating housing provided with piston vanes. |
US2478924A (en) * | 1946-09-19 | 1949-08-16 | Getty S Johnson | Rotary internal-combustion engine |
CH321163A (en) * | 1953-11-11 | 1957-04-30 | Bopp & Reuther Gmbh | Rotary piston machine |
US2958312A (en) * | 1957-06-25 | 1960-11-01 | Shimomura Kenji | Rotary internal combustion engine |
DE1094269B (en) * | 1959-02-11 | 1960-12-08 | Arno Fischer | Volumetric power machine or device |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4274374A (en) * | 1979-01-10 | 1981-06-23 | Lee Choong G | Air-cooled rotary internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
FR1407651A (en) | 1965-08-06 |
SE308427B (en) | 1969-02-10 |
GB992126A (en) | 1965-05-19 |
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