DE3419713A1 - Combustion engine with rotating drums - Google Patents

Combustion engine with rotating drums

Info

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Withdrawn
Application number
DE19843419713
Other languages
German (de)
Inventor
Jakob Dr. 8542 Roth Ulrich
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DE19843419713 priority Critical patent/DE3419713A1/en
Publication of DE3419713A1 publication Critical patent/DE3419713A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/04Charge admission or combustion-gas discharge
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
    • F01C11/004Combinations 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

This relates to a combustion engine with rotating drums. The drums (T2 to T5 sheet 1) have wedge-shaped recesses (a). At each explosion in the ignition chamber Z one flap (K1 and K2 sheet 1) is forced into each of these recesses. The surface with the 3 arrows is thereby freed for the explosion pressure and the other surface protected. The pressure can therefore only result in one rotation of the drums. The drums (T1 and T6 sheet 1) form the swept volumes HU. Due to their rotation the content is forced into the ignition chamber with the aid of the flap KL. The exhaust gases at B fig. 1 are expelled and forced out by rotation of the drums. All axes A are connected to one another by gears. The height of the drums and the size of the recesses and the ignition chamber/swept volume ratio are variable. This engine may be used like any conventional combustion engine. <IMAGE>

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)

P A T E N T A N S P R U F ( H E Verbrennungsmotor mit- rotierenden Trommeln, dadurch gekennzeichnet, daß ½) die Trommeln keilförmige Aussparunaen mit abgerundeten Ecken haben. In diese Ausspart ng wird durch den Explosionsdruck ein Ende einer Klappe gedrückt, wodurch eine Fläche dieser Aussparung für den Druck freigegeben, die zweite Fläche geschützt wird. P A T E N T A N S P R U F (H E Combustion engine co-rotating Drums, characterized in that ½) the drums have wedge-shaped cutouts have rounded corners. The explosion pressure enters this recess The end of a flap is pressed, creating an area of this recess for printing released, the second surface is protected. 2.) drei KLappen den Verbrennungsraum bilden. 2.) three flaps form the combustion chamber. 3.) der Hubraum von Trommeln gebildet wird. 3.) the cylinder capacity is formed by drums. A.) die Kompression von rotierenden ovalen Trommeln, mit Hilfe einer Klappe, bewirkt wird. A.) The compression of rotating oval drums, with the help of a Flap, is effected. 5.) bei gegenüberliegender Anordnung der Aussparungen tind der Hubräume, bei einer Umdrehung zweimal gezi:tndet werden kann. 5.) with opposing arrangement of the recesses and the displacements, can be struck twice with one revolution. 6. die Abgase sowohl herausgeschleudert, wie auch herausgeblasen werden können. 6. The exhaust gases are both thrown out and blown out can be. 7.) im Moment der Zündung der Zündraum vom Hubraum getrennt ist. 7.) At the moment of ignition, the ignition space is separated from the displacement.
DE19843419713 1984-05-26 1984-05-26 Combustion engine with rotating drums Withdrawn DE3419713A1 (en)

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

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Family Applications (1)

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DE19843419713 Withdrawn DE3419713A1 (en) 1984-05-26 1984-05-26 Combustion engine with rotating drums

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DE (1) DE3419713A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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