DE2618075A1 - Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors - Google Patents

Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors

Info

Publication number
DE2618075A1
DE2618075A1 DE19762618075 DE2618075A DE2618075A1 DE 2618075 A1 DE2618075 A1 DE 2618075A1 DE 19762618075 DE19762618075 DE 19762618075 DE 2618075 A DE2618075 A DE 2618075A DE 2618075 A1 DE2618075 A1 DE 2618075A1
Authority
DE
Germany
Prior art keywords
rotors
engine
gastight
maltese cross
sliding contact
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
Application number
DE19762618075
Other languages
German (de)
Inventor
Gustav Sandvoss
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 DE19762618075 priority Critical patent/DE2618075A1/en
Publication of DE2618075A1 publication Critical patent/DE2618075A1/en
Pending legal-status Critical Current

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
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/08—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/12—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type
    • F01C1/123—Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of other than internal-axis type with tooth-like elements, extending generally radially from the rotor body cooperating with recesses in the other rotor, e.g. one tooth
    • 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
    • F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • 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)
  • Supercharger (AREA)

Abstract

The internal combustion engine with maltese cross main rotor actuates side members for generating compression. The engine has stable running characteristics when designed to run on a diesel engine cycle, and does not use flywheel for stabilisation. The rotating main body arms are in sliding and gastight contact with pref. four rotating auxiliary rotors. This arrangement ensures the four cyclic processes of a four stroke engine. Each full revolution ensures, on using four auxiliary rotors sixteen working pulses per revolution.

Description

Der Hauptkörper hat im Querschnitt die Form einesThe main body has the shape of a in cross section

Malteserkreuzes und ist aus diesem Grunde, wie auch der ganze Motor, als Malteser bezeichnet. Die Nebenkörper haken bei entsprechender Gestaltung die Kompression zu erzeugen und heißen Verdichter.Maltese cross and for this reason, like the whole engine, referred to as a Maltese. The secondary bodies hook the Generate compression and hot compressor.

Der Funktionsablauf des in Rede stehenden Viertels vom Malteserkörper gestaltet sich folgendermaßen: In Fig. 2 sowie im beigefügten Demonstrationsmodell sind der walzenartige Hauptkörper und ein Verdichter im Schnitt dargestellt. Aus dieser dargestellten Situation ist zwischen den beiden Körpern die matheniatisch geometrisch Resultierende entwickelt. An dieser Resultierenden wird durch gleitende und gasdichte Beruhrung der labile Füllungsraum mit seinen vier Phasen des Viertakters gebildet. Bei der Rotation des Malteserkörpers mit vorzugsweise 1 n und des Verdichters in entgegengesetzter Drehrichtung mit 2 n wird zunächst durch den Verdichter der Füllungsraum geschlossen und komprimiert, dann gezündet und nach erfolgten Expandieren durch Weiterdrehung die achsiale Auspufföffnung spontan freigegeben. Diese Auspufföffnung schließt sich dann sofort wieder spontan.The functional sequence of the quarter in question from the Maltese body is as follows: In Fig. 2 and in the attached demonstration model the roller-like main body and a compressor are shown in section. the end This situation shown is the mathematical one between the two bodies geometrically resultant developed. This resultant is followed by sliding and gas-tight contact with the unstable filling space with its four phases of the four-stroke engine educated. When rotating the Geneva body with preferably 1 n and the compressor in the opposite direction of rotation with 2 n, the compressor is initially the Filling space closed and compressed, then ignited and after expansion has taken place the axial exhaust port is released spontaneously by further turning. This exhaust port then closes again spontaneously.

Zur genauen uflrung und zur Ergänzung speziell dieser Voringe füge ich ein Demonstrationsmodell bei.For precise information and to supplement these items in particular I am providing a demonstration model.

Da sich der Malteser mit 1 n und der Verdichter mit 2 n dreht, sind die in Positionen dargestellten Kreisbogeneinteilungen so dargestellt, daß bei gleichen Positionszahlen beim Malteser 3,75 Grad vom Kreise liegen und bei denen des Verdichters je 7,5 Grad. Es sind daher zu Beginn, beide Körper auf 0 einzustellen, und bei der Weiterdrehung beider Körper auf je die gleichen Positionen sieht man dann von Pos. 1 - 6 bzw. 7 die Komprimierung, in 6 - 7 wird gezündet und in Pos. 7 - 8 erfolgt die Expandierung und der Auslass.Since the Maltese rotates with 1 n and the compressor with 2 n, are the arc divisions shown in positions shown so that with the same Position numbers for the Maltese are 3.75 degrees from the circle and for those of the compressor 7.5 degrees each. It is therefore at the beginning to set both bodies to 0, and at the Further rotation of both bodies to the same positions can be seen from pos. 1 - 6 or 7 the compression, in 6 - 7 it is ignited and in pos. 7 - 8 it takes place the expansion and the outlet.

An diesem Modell ist gut zu erkennen, daß in allen Positionen immer 2 Punkte gasdicht geschlossen sind und den labilen Füllungsraum oilden. Die Kühlung ist wie allgemein heute üblich und daher nicht d rgestellt.This model clearly shows that in all Positions 2 points are always closed gas-tight and oil the unstable filling space. the Cooling is common today and is therefore not shown.

Das frische Treibstoff-Luftgemisch bzw. beim Einspritzer und beim Diesel die reine Luft tritt wie bei jedem Exhaustor echsial in des Verdichtergehäuse ein und wird durch den mit 2 n laufenden Verdichter zusätzlich vorverdichtet.The fresh fuel-air mixture or with the injector and with Diesel, the pure air, enters the compressor housing echsially as with any exhaustor and is additionally pre-compressed by the compressor running at 2 n.

Bei seiner verblüffenden Einfachhiet und seiner stabilen Laufstarre ist dieser M-Motor vorzüglich als Diesel geeignet und zwar von den kleinsten bis zu den größten Dimensionen.With its amazing simplicity and its stable rigidity this M-engine is ideally suited as a diesel, from the smallest to to the largest dimensions.

Dank seines hohen Gleichförmigkeitgrades im Lauf, kann alles sehr leicht gehalten sein, sogar die Schwungscheibe fällt weg. Bei höheren Drehzahlen wird dieser M-Motor der Turbine immer ähnlicher.Thanks to its high degree of uniformity in the run, everything can be very good be held lightly, even the flywheel is omitted. At higher speeds this M-motor is becoming more and more similar to the turbine.

Claims (1)

Patentanspruch "M a l t e s e r m o t o r " Der Maltesermotor ist ein von mir erfundener Rotations/Verbrennungsmotor.Claim "M altesermotor" The Maltese engine is a rotary / internal combustion engine that I invented. Er ist gekennzeichnet dadurch, daß ein walzenartiger, rotierender Hauptkörper so gestaltet und so gelagert ist, daß durch seine gleitende und gasdichte Berührung mit einem bzw. mit mehreren, vorzugsweise mit vier, ebenfalls walzenartigen und rotierenden Nebenkörpern schon bei einer viertel Umdrehung die vier Funktionsvorgänge des Viertaktmotors erreicht werden.It is characterized in that a roller-like, rotating Main body is designed and mounted so that by its sliding and gas-tight Contact with one or with several, preferably four, also roller-like and rotating secondary bodies, the four functional processes are carried out in just a quarter of a turn of the four-stroke engine can be achieved. Es bedeutet dies, daß auf je eine volle Umdrehung vier, und bei vier Nebenkörpern zusammen sogar 16 Ärbeitsimpulse auf eine Umdrehung kommen.This means that for every full revolution four, and with four Secondary bodies together even produce 16 work impulses per rotation.
DE19762618075 1976-04-24 1976-04-24 Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors Pending DE2618075A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19762618075 DE2618075A1 (en) 1976-04-24 1976-04-24 Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762618075 DE2618075A1 (en) 1976-04-24 1976-04-24 Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors

Publications (1)

Publication Number Publication Date
DE2618075A1 true DE2618075A1 (en) 1978-01-05

Family

ID=5976195

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19762618075 Pending DE2618075A1 (en) 1976-04-24 1976-04-24 Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors

Country Status (1)

Country Link
DE (1) DE2618075A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993014314A1 (en) * 1992-01-07 1993-07-22 Snell (Hydro Design) Consultancy Limited Water turbines or pumps

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1993014314A1 (en) * 1992-01-07 1993-07-22 Snell (Hydro Design) Consultancy Limited Water turbines or pumps
US5468132A (en) * 1992-01-07 1995-11-21 Snell (Hydro Design) Consultancy Limited Water turbines

Similar Documents

Publication Publication Date Title
DE2141895A1 (en) Rotary piston engine with internal combustion
DE2618075A1 (en) Maltese cross engine with contacting rotors - has central rotor in gastight and sliding contact with auxiliary rotors
DE2256776A1 (en) PENDULUM PISTON ENGINE
DE339761C (en) Internal combustion engine with two pistons rotating in a ring cylinder
DE719397C (en) Rotary piston internal combustion engine
DE4427105C1 (en) Rotary IC engine with hinged segments
DE1086941B (en) Process for generating propellant gas and piston propellant gas generator for carrying out the process
DE2420296A1 (en) Supercharged rotary piston engine - with continuous ignition, power stroke lasting through 300o, and some turbine-like characteristics
DE808304C (en) Two-stroke engine
DE732374C (en) Two-stroke internal combustion engine
DE2154547A1 (en) COMBUSTION ENGINE AS ROTATING PISTON OR ROTARY CYLINDER MOTOR
DE2648395A1 (en) Rotary radial piston engine - has pistons guided by fingers which slide in circumferential slot of central elliptical members
DE842723C (en) Rotary piston machine with a fixed abutment and a rotatable member arranged on the piston disk
DE2217766A1 (en) Central flushing and charging process by means of swivel slide axles, especially for two-chamber two-stroke oscillating piston internal combustion engines
DE2315440A1 (en) TURBO ROTOR ENGINE - HRUMIN 72-93
DE709245C (en) Explosion turbine
DE212018000229U1 (en) Rotary engine
DE705628C (en) Four-stroke internal combustion piston engine system with water injection
DE2131966A1 (en) ROTARY LISTON COMBUSTION ENGINE
Le Roux Qualitative Analysis of Sealing Element Behavior in Various Types of Internal Combustion Engines.
DE3610703A1 (en) Disc rotor motor
DE1905321A1 (en) Trigonon gas and liquid compressor pump
DE1426067A1 (en) Rhomboid oscillating piston internal combustion engine
DE1451794A1 (en) Internal combustion engine with rotating combustion chamber piston
DE1902203A1 (en) Spherical rotary machine with six rotating pistonless motors

Legal Events

Date Code Title Description
OAP Request for examination filed
OD Request for examination
OHW Rejection