WO2015003818A2 - Turbines brinkmann à joints actifs, à pré-compression, à post-expansion et à fonctionnement à deux temps wankel - Google Patents

Turbines brinkmann à joints actifs, à pré-compression, à post-expansion et à fonctionnement à deux temps wankel Download PDF

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Publication number
WO2015003818A2
WO2015003818A2 PCT/EP2014/001932 EP2014001932W WO2015003818A2 WO 2015003818 A2 WO2015003818 A2 WO 2015003818A2 EP 2014001932 W EP2014001932 W EP 2014001932W WO 2015003818 A2 WO2015003818 A2 WO 2015003818A2
Authority
WO
WIPO (PCT)
Prior art keywords
rotors
housing
turbines
wankel
rotating
Prior art date
Application number
PCT/EP2014/001932
Other languages
German (de)
English (en)
Other versions
WO2015003818A3 (fr
Inventor
Wilhelm Brinkmann
Original Assignee
Wilhelm Brinkmann
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 Wilhelm Brinkmann filed Critical Wilhelm Brinkmann
Publication of WO2015003818A2 publication Critical patent/WO2015003818A2/fr
Publication of WO2015003818A3 publication Critical patent/WO2015003818A3/fr

Links

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
    • F01C1/22—Rotary-piston machines or engines of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth- equivalents than the outer member
    • 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
    • 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
    • F01C13/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • 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
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F01C19/005—Structure and composition of sealing elements such as sealing strips, sealing rings and the like; Coating of these elements
    • 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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • 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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/10—Outer members for co-operation with rotary pistons; Casings
    • 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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/06—Heating; Cooling; Heat insulation

Definitions

  • a third object are rotary steam turbines for driving
  • the pressure should first be at least ninefold. In total, the pressure should be at least 24 bar before the explosions. Furthermore, should after the
  • the purpose of the invention is thus to be achieved by the fuel injection under high pressure from the inside via cams on the crankshaft. This should then, for example, diesel fuel in the
  • Fuels, as well as cooling and lubricants for reducing friction in the engine via the rotors allows.
  • the predominant engine mass will also act as their own flywheel mass, when doing the crankshaft fixed as a crank shaft stands still. Not only fuels, coolants and lubricants can be supplied via this central tube, but ultimately exhaust gases can be discharged as well
  • Compression phase of the engine through a catalyst through is sprayed.
  • These motors can also be equipped with active seals and a more efficient rotor principle, namely asymmetric symmetrical rotors.
  • the exhaust gas then consists of oxygen and distilled water.
  • Fig. 4 is a front view of the main rotor (9) which rotates about the cam crank shaft (0) on its eccentric (10). He sweeps over the cam (18), each with a ball bearing (21) which is mounted on a slide (22) and in the main rotor (9) which is designed there as a guide, can move to the outside and inside.
  • the slider has at the other end a small piston (23) attached, which moves in the cylinder (24) to the outside and inside, while the fuel is under high pressure, which in turn by one or more nozzles in the
  • the Z-combustion chamber mold (26) advantageously distributes the force vectors of the explosions in the direction of the desired direction of travel, mainly at the beginning of the respective explosion, since these vectors are always perpendicular to surfaces.
  • Fig. 7 is an isometric view of a set in front of the Brinkmann turbine
  • Exhaust valves (14) visible from which the exhaust-steam mixture flows into the rotating around the center of the Brinkmann turbine turbocharger (30). These generate a highly compressed fresh air stream which serves to blow out the expansion chambers of the main rotor housing (8) and which is generated in the cylinders of the compressor (31) by its rotating double-acting pistons on rotating connecting rods which rotate about the cam crankshaft (0) in this part resembles a normal crankshaft, though the part of course stands still. After this "crankshaft part" of the cam crank shaft (0) goes back into its central arch form around which rotates the entire Brinkmann turbine housing in the last central part of the
  • Fig. 10 is an isometric general view and concurrent overview of the Brinkmann turbine showing that this closed combustion process with multiple energy recirculation is an extremely useful way of generating torque because from the front to the rear 3 compression processes 3
  • Fig. 13 is a front view of a Wankel turbine (47) where steam or other releasable gas or fluid under pressure enters the lower left to exit to the right, continuing to rotate the rotor.
  • the SZ shape of the wankel-like rotor will increase the overall efficiency, because the pressure as a fundamental fact of physics always acts perpendicular to a wall with a corresponding resulting vector fraction. Which, of course, has to be done taking into account the adequate direction of rotation of the rotor, since this is now asymmetrically symmetrical.
  • Fig. 14 is a front view of the Wankel turbine (47) where steam or other relaxable gas or fluid under pressure enters from the right and exits the left as soon as the rotor has arrived in its home position before frictional engagement on the other side is, so now by a simple with the Wankel turbine (47)

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • General Electrical Machinery Utilizing Piezoelectricity, Electrostriction Or Magnetostriction (AREA)

Abstract

D'un point de vue philosophique, le présent ensemble turbine Brinkmann producteur d'énergie est une machine ramenée au minimum de pièces pour le moment nécessaire, dans laquelle les principes de la symétrie universelle sont entièrement applicables et permettant pour cette raison une rotation du type turbine. Cela entraîne automatiquement un gain de puissance immense, mais économique, sur un espace des plus réduits. Les points fixes peuvent également se limiter à trois en tant que conditions préalables minimales de symétrie centrale, après quoi le fait de se demander si le reste de l'univers tourne autour du derviche ou si c'est celui-ci qui tourne dans l'univers n'a pour ainsi dire plus aucune importance. Des pièces asymétriques faisant office de corps rotatifs sont éliminées autant que possible. C'est surtout le vilebrequin qui n'est utilisé en tant que pour des applications particulières relativement à faible vitesse. L'espace avant résiduel dans la turbine Brinkmann est occupé par les pièces asymétriques également fixes, la pompe à carburant, la pompe à huile et la pompe à eau, lesquelles sont accouplées à la transmission à roue planétaire fixe avant, ainsi que le conduit d'air. Il ne reste donc guère qu'un tout petit déséquilibre agissant dans le sens radial. Les cycles thermodynamiques de la récupération d'énergie sont amenés, dans la turbine Brinkmann, à un premier maximum provisoire, ce qui peut également être rattaché au principe de la conception symétrique et par la même occasion garantit la marche la plus silencieuse de la turbine Brinkmann, y compris en cas de régimes très élevés. Et tout ceci y compris lors de l'utilisation non seulement de carburants diesel à auto-allumage, car une compression très importante est à présent disponible et peut également être maintenue sans frottement grâce à une technologie d'étanchéité active, mais également de combinaisons de carburants ou d'agents propulseurs, lesquels peuvent être produits à partir d'un courant, ce qui permet ainsi le transport de courant en tant que liquide pouvant être facilement stocké, mais présentent respectivement une densité énergétique élevée. L'invention concerne le principe classique de piston rotatif de turbines et de pompes pour des milieux ou liquides sous pression pouvant être détendus. Les améliorations constituent également principalement les meilleures possibilités d'étanchéification actives, mais concernent également la disposition des éléments d'admission et d'échappement en combinaison avec les rotors du type Wankel asymétriquement symétriques décrits ici en particulier. L'invention concerne également l'utilisation de la combustion catalytique au moyen du H202 dans de telles turbines.
PCT/EP2014/001932 2013-07-11 2014-07-10 Turbines brinkmann à joints actifs, à pré-compression, à post-expansion et à fonctionnement à deux temps wankel WO2015003818A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013012052.7 2013-07-11
DE201310012052 DE102013012052A1 (de) 2013-07-11 2013-07-11 Brinkmann-Turbinen mit aktiven Dichtungen, Vorverdichtung, Nachexpansion sowie Wankelzweitaktfunktion

Publications (2)

Publication Number Publication Date
WO2015003818A2 true WO2015003818A2 (fr) 2015-01-15
WO2015003818A3 WO2015003818A3 (fr) 2015-07-02

Family

ID=51585062

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2014/001932 WO2015003818A2 (fr) 2013-07-11 2014-07-10 Turbines brinkmann à joints actifs, à pré-compression, à post-expansion et à fonctionnement à deux temps wankel

Country Status (2)

Country Link
DE (1) DE102013012052A1 (fr)
WO (1) WO2015003818A2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210285441A1 (en) * 2020-03-11 2021-09-16 Borgwarner Inc. Rotary piston compressor and system for temperature conditioning with rotary piston compressor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1194636B (de) * 1962-03-24 1965-06-10 Beteiligungs & Patentverw Gmbh Kreiskolbenmaschine
DE2355728A1 (de) * 1973-11-08 1975-05-15 Gerhard Noeltner Motorgenerator
DE2946457A1 (de) * 1979-11-17 1981-05-27 Fritz 6000 Frankfurt Opel Hochverdichtende rotationskolben- brennkraftmaschine
CA2607700A1 (fr) * 2006-11-03 2008-05-03 General Electric Company Systeme et methode de scellement mecanique pour machines rotatives
DE102006057003A1 (de) * 2006-12-02 2008-06-05 GÜNTHER, Eggert Prinzip und System zur Abdichtung des Kolbens von Rotationskolbenmaschinen
DE102013000919A1 (de) * 2012-05-09 2013-11-14 Wilhelm Brinkmann Wankel Turbinen und Wankel Dampf Turbinen mit Aktiven Dichtungen

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20210285441A1 (en) * 2020-03-11 2021-09-16 Borgwarner Inc. Rotary piston compressor and system for temperature conditioning with rotary piston compressor
US11841019B2 (en) * 2020-03-11 2023-12-12 Borgwarner Inc. Rotary piston compressor and system for temperature conditioning with rotary piston compressor

Also Published As

Publication number Publication date
DE102013012052A1 (de) 2015-01-15
WO2015003818A3 (fr) 2015-07-02

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