DE3419713A1 - Combustion engine with rotating drums - Google Patents
Combustion engine with rotating drumsInfo
- Publication number
- DE3419713A1 DE3419713A1 DE19843419713 DE3419713A DE3419713A1 DE 3419713 A1 DE3419713 A1 DE 3419713A1 DE 19843419713 DE19843419713 DE 19843419713 DE 3419713 A DE3419713 A DE 3419713A DE 3419713 A1 DE3419713 A1 DE 3419713A1
- Authority
- DE
- Germany
- Prior art keywords
- drums
- flap
- combustion engine
- recesses
- ignition
- 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- Withdrawn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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/04—Charge admission or combustion-gas discharge
-
- 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
- F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
- F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
- F01C11/004—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
-
- 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
Abstract
Description
BESCHREIBUNG DESCRIPTION
DES VERBRENNUNGSMOTORS MIT ROTIERENDEN TROMMELN Zwei oder mehrere Trommeln (Tl bis T10 Abb. 1 und 2) drehen sich mit dann Achsen (A Abb. 1 + 2). Die Trommeln haben keilförmige Aussparungen (a). Bei jeder Trommel ist eine Klappe (Kl und K2). OF THE COMBUSTION ENGINE WITH ROTATING DRUMS Two or more Drums (Tl to T10 Fig. 1 and 2) then turn with axes (A Fig. 1 + 2). the Drums have wedge-shaped recesses (a). Each drum has a flap (cl and K2).
Diese Klappen bilden mit der Klappe (KL) in geschlossenem Zustand dtn Raum, in dem die Zündung erfolgt (Z Abb. 1 + 2). Oben und unten schliesst je eine Abdeckplatte (Abb. 3 Ab) ab. In den Abdeckplatten laufen die Achsen aller beweglichen Teile (Abb. 4).These flaps form with the flap (KL) in the closed state dtn room in which the ignition takes place (Z Fig. 1 + 2). Above and below each close a cover plate (Fig. 3 Ab). The axes of all movable ones run in the cover plates Parts (Fig. 4).
Der Zündstoff kommt bi M Abb. 1 in den Hubraum (HU Abb. 1), also dann, wenn dieser geschlossen ist. Dreht sich die ovale Trommel (T9 Abb. 2 ) in Pfeilrichtung, ird der Zündstoff in die Zündkammer (Z) gepresst, wobei die Klappe KL Abb. 2 dadurch, daß ein Ende ständig auf die ovale Trommel gedrückt wird, die Richtung weist. Der Druck auf die Trommel kann durch eine Spiralfeder (Fe Abb. 3 + 4), die an der Abdeckplatte im Oelraum (Oel bei C) befestigt ist. Der Spalt in der Abdeckplatte, in dem sich der Zapfen der Klappe KL bewegt, wird mit einer kleinen Platte (d Abb. 4) zugedeckt. Diese Platte bewegt sich mit der Klappe (KL Abb. 3) Abb. 3 zeigt den Querschnitt wie in Abb. 2 schraffiert zwischen O und 01 angezeigt ist.The explosive comes into the cylinder capacity in M Fig. 1 (HU Fig. 1), so then, when this is closed. If the oval drum (T9 Fig. 2) rotates in the direction of the arrow, If the ignition material is pressed into the ignition chamber (Z), the flap KL Fig. 2 thereby, that one end is constantly pressed onto the oval drum, which shows the direction. Of the Pressure on the drum can be done by a spiral spring (Fe Fig. 3 + 4) attached to the cover plate is fixed in the oil room (oil at C). The gap in the cover plate in which the pin of the flap KL moves, is covered with a small plate (d Fig. 4). This plate moves with the flap (KL Fig. 3) Fig. 3 shows the cross section as indicated by hatching between O and 01 in Fig. 2.
In Abb. 1 ist die Kompression zu Ende, die Zündung erfolgt. In diesem Moment ist der Hubraum vom Zündraum getrennt. Die Klappen Kl +K42 werden durch den Explosionsdruck in die Aussparungen (a) gedrückt und geben die Fläche der Aussparung frei auf der der Druck die Trommeln in der Drehrichtung (Pfeilrichtung) bewegt.In Fig. 1 the compression has ended and the ignition takes place. In this At the moment, the displacement is separated from the ignition chamber. The flaps Kl + K42 are through the Explosion pressure is pressed into the recesses (a) and enter the area of the recess freely on which the pressure moves the drums in the direction of rotation (arrow direction).
Die andere Fläche von a wird durch die Klappen geschützt (verhindert Gegendruck). Die Trommeln drehen sich und schleudern die abgase bei B aus. Man kann zusetzlich durch eine Oeffnung in der Abdeckplatte (Oe Ahb. 4) durch Luftdruck nachhelfen.The other face of a is protected by the flaps (prevented Counter pressure). The drums rotate and throw the exhaust gases out at B. One can additionally help through an opening in the cover plate (Oe Fig. 4) with air pressure.
Abb. 4 zeigt die Abdeckplatte. Alle beweglichen Teile des Motors drehen sich mit ihren Achsen in die>.n Platten (KI, K2, KL und alle A sowie die Hauptachse Ha). Sie sind deshalb durch den O<l -raum (Oel Abb. 3) leicht zu schmieren. Die Achsen A, die O@@fnungen für die Zündung, die Oeffnungen ne fir das Durchblasen der Luft, sowie die Hauptachst (Ha) werden durch den Oel-und Wasserraum durchgeführt. Die Achsen A sind mit Hauptachse durch Zahnräder so verbunden, dass sich alle gleichmässig und in gewünschter Richtung drehen. Fig. 4 shows the cover plate. All moving parts of the engine rotate with their axes in the> .n plates (KI, K2, KL and all A as well as the Main axis Ha). They are therefore easy to lubricate through the oil space (oil Fig. 3). The axes A, the O @@ openings for the ignition, the openings ne for the blowing the air, as well as the main axes (Ha) are carried through the oil and water space. The axes A are connected to the main axis by gears in such a way that they all move evenly and turn in the desired direction.
Es besteht die Möglichkeit durch entgegengesetzte Aussparungen (a) bei den Trommeln T2, T3, T4 und T5 Abb. 1, einen besseren Gewichtsausgleich und durch zwei Hubräume bci Tl, bei einer Umdrehung 2 Zündungen zu erhalten. There is the possibility through opposing recesses (a) with drums T2, T3, T4 and T5 Fig. 1, a better weight compensation and by two cubic capacities bci Tl, to get 2 ignitions with one revolution.
Eine kleine Ausbuchtung (Abb. 1) bei den Trommeln T2 und T3 bei k bewirkt, dass der Zündraum etwas erweitert wird. Dadurch kann mehr Brennstoff in den Zündraum aufgenommen werden, der dann durch die Höcker h, unmittelbar vor der Zündung komprimiert wird. A small bulge (Fig. 1) on drums T2 and T3 at k causes the ignition space to be expanded somewhat. This allows more fuel to be put in the ignition chamber are added, which then through the hump h, immediately before the Ignition is compressed.
Die Ecken der Aussparungen (a) können abgerundet werden. so daß die Klappen (K1 + Y2 Abb. 1 + 2). wenn sie in die Aussparungen gedrückt werden, auf eine schiefe Ebene prallen und dadurch beschleunigend und lärmmindernd wirken. The corners of the recesses (a) can be rounded. So that the Flaps (K1 + Y2 Fig. 1 + 2). when they are pushed into the recesses crashing down an incline and thereby have an accelerating and noise-reducing effect.
In Abb. 1 ist der fehlende untere Teil gleich dem oberen. In Fig. 1 the missing lower part is the same as the upper one.
- Leerseite -- blank page -
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843419713 DE3419713A1 (en) | 1984-05-26 | 1984-05-26 | Combustion engine with rotating drums |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19843419713 DE3419713A1 (en) | 1984-05-26 | 1984-05-26 | Combustion engine with rotating drums |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3419713A1 true DE3419713A1 (en) | 1985-04-18 |
Family
ID=6236935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19843419713 Withdrawn DE3419713A1 (en) | 1984-05-26 | 1984-05-26 | Combustion engine with rotating drums |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3419713A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2777943A1 (en) * | 1998-04-22 | 1999-10-29 | Andre Louis Kovacs | Thermodynamic motor for converting heat into mechanical energy |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1189115A (en) * | 1915-12-06 | 1916-06-27 | Thomas J Jameson | Rotary internal-combustion engine. |
GB135778A (en) * | 1919-05-23 | 1919-12-04 | David Hercules Robertson | Improvements in Rotary Internal Combustion Engines. |
DE1526412A1 (en) * | 1965-10-12 | 1970-04-23 | Rolls Royce | Rotary piston internal combustion engine |
DE1904202A1 (en) * | 1969-01-29 | 1970-08-06 | Gerhard Kapolke | Internal combustion engine with piston disks rotating in annular spaces |
DE1963377A1 (en) * | 1969-10-06 | 1971-04-22 | Antioco Lampis | Rotary piston engine |
-
1984
- 1984-05-26 DE DE19843419713 patent/DE3419713A1/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1189115A (en) * | 1915-12-06 | 1916-06-27 | Thomas J Jameson | Rotary internal-combustion engine. |
GB135778A (en) * | 1919-05-23 | 1919-12-04 | David Hercules Robertson | Improvements in Rotary Internal Combustion Engines. |
DE1526412A1 (en) * | 1965-10-12 | 1970-04-23 | Rolls Royce | Rotary piston internal combustion engine |
DE1904202A1 (en) * | 1969-01-29 | 1970-08-06 | Gerhard Kapolke | Internal combustion engine with piston disks rotating in annular spaces |
DE1963377A1 (en) * | 1969-10-06 | 1971-04-22 | Antioco Lampis | Rotary piston engine |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2777943A1 (en) * | 1998-04-22 | 1999-10-29 | Andre Louis Kovacs | Thermodynamic motor for converting heat into mechanical energy |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
OAV | Applicant agreed to the publication of the unexamined application as to paragraph 31 lit. 2 z1 | ||
OM8 | Search report available as to paragraph 43 lit. 1 sentence 1 patent law | ||
Q161 | Has additional application no. |
Ref document number: 3440030 Country of ref document: DE |
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8139 | Disposal/non-payment of the annual fee |