[go: up one dir, main page]

WO1997019255A2 - Power engine - working machine with turbine rotor - Google Patents

Power engine - working machine with turbine rotor Download PDF

Info

Publication number
WO1997019255A2
WO1997019255A2 PCT/DE1996/002191 DE9602191W WO9719255A2 WO 1997019255 A2 WO1997019255 A2 WO 1997019255A2 DE 9602191 W DE9602191 W DE 9602191W WO 9719255 A2 WO9719255 A2 WO 9719255A2
Authority
WO
WIPO (PCT)
Prior art keywords
engine
working machine
turbine
chamber volume
machine according
Prior art date
Application number
PCT/DE1996/002191
Other languages
German (de)
French (fr)
Other versions
WO1997019255A3 (en
Inventor
Dietmar Stope
Original Assignee
Dietmar Stope
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 Dietmar Stope filed Critical Dietmar Stope
Priority to AU17658/97A priority Critical patent/AU1765897A/en
Publication of WO1997019255A2 publication Critical patent/WO1997019255A2/en
Publication of WO1997019255A3 publication Critical patent/WO1997019255A3/en

Links

Classifications

    • 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
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-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
    • F01C1/34Rotary-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 the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • 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

Definitions

  • the invention relates to a power and working machine that can convert both compressive forces into mechanical forces and mechanical forces into compressive forces.
  • the combination of both machines results in an internal combustion engine.
  • a combustion chamber (9) is connected between the inlet duct (5) of the engine and the outlet duct (6) of the working machine, and the two axes (3) are connected to one another in a gearbox (10) so that the same turbines - rotor size rotates the axis of the engine faster.
  • Engines and machines with rotary pistons are known and internal combustion engines with rotary pistons are known.
  • the invention has for its object to produce pressure-resistant and wear-resistant sealing surfaces during the rotation of a turbine rotor.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Hydraulic Motors (AREA)
  • Hydraulic Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention concerns a power engine - working machine comprising a rotating turbine rotor which urges an annular chamber volume from the inlet duct into the outlet duct. The turbine rotor can be used as a power engine - working machine for liquids and gases. An internal combustion engine requires a driving engine and a working machine. A known combustion chamber is disposed between the two high-pressure ducts and the two shafts are connected to form a transmission such that the power engine shaft rotates more rapidly whilst the size of the turbine rotor is unchanged. The drive power is the difference between the rotational forces of the two shafts.

Description

K R A F T - U N D A R 3 E I T S M A S C H I N E M I T T U R B I N E N L Ä U F E RK R A F T - U N D A R 3 E I T S M A S C H I N E M I T T U R B I N E N LÄ U F E R

B e s c h r e i b u n g :Description :

Die Erfindung betrifft eine Kraft- und Arbeitsmaschine, die sowohl Druckkräfte in mechanische Kräfte, als auch mechani¬ sche Kräfte in Druckkräfte umwandeln kann. Die Kombination aus beiden Maschinen ergibt eine Brennkraftmaschine. Es wird eine Brennkammer (9) zwischen den Einlaßkanal (5) der Kraft¬ maschine und den Auslaßkanal (6) der Arbεitsmaschine ge¬ schaltet und die zwei Achsen (3) werden in einem Getriebe (1o) so miteinander verbunden, daß bei gleicher Turbinen- läufergröße die Achse der Kraftmaschine schneller dreht.The invention relates to a power and working machine that can convert both compressive forces into mechanical forces and mechanical forces into compressive forces. The combination of both machines results in an internal combustion engine. A combustion chamber (9) is connected between the inlet duct (5) of the engine and the outlet duct (6) of the working machine, and the two axes (3) are connected to one another in a gearbox (10) so that the same turbines - rotor size rotates the axis of the engine faster.

Es sind Kraft- und Arbeitsmaschinen mit Rotationskolben be¬ kannt und es sind Brennkraftmaschinen mit Rotationskolben bekannt.Engines and machines with rotary pistons are known and internal combustion engines with rotary pistons are known.

Die Nachteile der Dichtfähigkeit des Kammervolumens (4) bei hohen Drücken und bei Verschleiß sind nicht gelöst.The disadvantages of the sealability of the chamber volume (4) at high pressures and when worn are not solved.

Der Erfindung liegt die Aufgabe zugrunde, drucksichere und verschleißsichere Dichtflächen bei der Rotation eines Turbinenläufers herzustellen.The invention has for its object to produce pressure-resistant and wear-resistant sealing surfaces during the rotation of a turbine rotor.

Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß so¬ wohl die Dichtungsnocke (7), als auch die Dichtungsschau¬ feln (.'8) über genügend Dichtfläche verfügen und sich dem Verschleiß anpassen können.This object is achieved in that both the sealing cam (7) and the sealing blades (. ' 8) have sufficient sealing surface and can adapt to wear.

Die mit der Erfindung erzielten Vorteile bestehen insbeson¬ dere darin, daß durch eine einfache Mechanik ein hoher Wirkungsgrad erreicht wird. The advantages achieved by the invention are, in particular, that a high degree of efficiency is achieved by a simple mechanism.

Claims

P a t e n t a n s p r ü c h e : Patent claims: 1. Kraft- und Arbeitsmaschine mit Turbinenläufer, der aus ei¬ nem Turbinenring und einem Turbinenkern besteht, zwischen denen ein Kammervolumen ist, welches durch Rotation von dem Einlaßkanal zu dem Auslaßkanal gedrückt wird, d a d u r c h g e k e n n z e i c h n e t , daß der Turbinenring (1) und der Turbinenkern (2) in einer Achse (3) liegen. Entweder der Turbinenring dreht in der Achse um den Turbinenkern, oder der Turbinenkern dreht in der Achse in dem Turbinenring.1. Motor and working machine with turbine rotor, which consists of a turbine ring and a turbine core, between which there is a chamber volume which is pressed by rotation from the inlet channel to the outlet channel, characterized in that the turbine ring (1) and the turbine core ( 2) lie in one axis (3). Either the turbine ring rotates in the axis around the turbine core, or the turbine core rotates in the axis in the turbine ring. 2. Kraft- und Arbeitsmaschine nach Anspruch 1, d a d u r c h g e k e n n z e i c h n e t , daß zwischen dem Turbinenring und dem Turbinenkern ein ringförmiges Kammervolumen ('4) -ist.2. The power and working machine according to claim 1, which also has an annular chamber volume ('4) between the turbine ring and the turbine core. 3« Kraft- und Arbeitsmaschine nach Anspruch 1 oder 2, d a d u r c h g e k e n n z e i c h n e t , daß in das ringförmige Kammervolumen ein Einlaßkanal (5) und ein Auslaßkanal ('6) führen. Als Variante I führen die Kanäle durch den Turbinenring und als Variante II führen die Kanäle durch den Turbinenkern.3 «Power and working machine according to claim 1 or 2, characterized in that an inlet channel (5) and an outlet channel ( ' 6) lead into the annular chamber volume. As variant I the channels lead through the turbine ring and as variant II the channels lead through the turbine core. 4. Kraft- und Arbeitsmaschine nacn Anspruch 1 bis 3> d a d u r c h g e k e n n z e i c h n e t , daß zwischen dem Einlaßkanal und dem Auslaßkanal eine Dich- tungsnocke (7) in das Kammervolumen hineinragt. Sie trennt das ringförmige Kammervolumen so, daß zwischen dem Sinlaß- kanal und dem Auslaßkanal keine direkte Verbindung besteht. 4. Power and working machine according to claims 1 to 3 > characterized in that a sealing cam (7) protrudes into the chamber volume between the inlet channel and the outlet channel. It separates the annular chamber volume so that there is no direct connection between the inlet channel and the outlet channel. 5. Kraft- und Arbeitsmaschine nach Anspruch 1 bis 4, d a d u r c h g e k e n n z e i c h n e t , daß mindestens zwei Dichtungsschaufeln ('8) das ringförmige Kammervolumen von dem Einlaßkanal in den Auslaßkanal drü¬ cken. Die zwei Dichtungsschaufeln sind um 36° /zwei=18o versetzt. Sie dichten in dem ringförmigen Kammervolumen ei¬ nen Bereich von größer als 36o /zwei=18o° ab, der gegenüber der Dichtungsnocke liegt. Um bei Rotation an der Dichtungs- nocke vorbeizukommen, ziehen sich die Dichtungsschaufeln ein und übernehmen in diesem Bereich keine Dichtungsfunktion.5. Engine and machine according to claim 1 to 4, d a d u r c h g e k e n n z e i c h n t that at least two sealing blades ('8) press the annular chamber volume from the inlet channel into the outlet channel. The two sealing blades are offset by 36 ° / two = 18o. In the annular chamber volume, they seal a region of greater than 36o / two = 18o °, which lies opposite the sealing cam. In order to get past the sealing cam during rotation, the sealing blades retract and do not perform a sealing function in this area. 6. Kraft- und Arbeitsmaschine nach Anspruch 1 bis 5, d a d u r c h g e k e n n z e i c h n e t , daß die Kraftmaschine (Fig.1) durch das Drücken des Kammer¬ volumens von dem Einlaßkanal (Hochdruck) in den Auslaßkanal (Normaldruck) den Turbinenläufer zur Rotation bringt.6. Engine and working machine according to claim 1 to 5, d a d u r c h g e k e n n z e i c h n e t that the engine (Fig.1) by pressing the Kammer¬ volume of the inlet channel (high pressure) in the outlet channel (normal pressure) brings the turbine rotor to rotation. 7. Kraft- und Arbeitsmaschine nach Anspruch 1 bis 6, d a d u r c h g e k e n n z e i c h n e t , daß die Arbeitsmaschine (Fig.2) durch Rotation des Turbinen¬ läufers das Kammervolumen von dem Einlaßkanal (Normaldruck) in den Auslaßkanal (Hochdruck) drückt.7. Engine and machine according to claim 1 to 6, d a d u r c h g e k e n n z e i c h n e t that the machine (Fig.2) by rotating the Turbinen¬ rotor presses the chamber volume from the inlet channel (normal pressure) into the outlet channel (high pressure). 8. Kraft- und Arbeitsmaschine nach Anspruch 1 bis 7, d a d u r c h g e k e n n z e i c h n e t , daß die Brennkraftmaschine (Fig.3) aus einer Kraftmaschine und einer Arbeitsmaschine besteht. Zwischen dem Einlaßkanal der Kraftmaschine und dem Auslaßkanal der Arbeitsmaschine ist eine Brennkammer (9) geschaltet, in der komprimierte Luft mit Brennkraftstoff gemischt und verbrannt wird. Die Achsen der Kraftmaschine und der Arbeitsmaschine sind in einem Getriebe (1o) miteinander verbunden. Bei gleicher Tur¬ binenläufergroße dreht die Achse der Kraftmaschine schnelles als die Achse der Arbeitsmaschine. Die Differenz aus den Drehkräften ist die Antriebsleistung der Brennkraftmaschine. 8. Engine and working machine according to claim 1 to 7, d a d u r c h g e k e n n z e i c h n e t that the internal combustion engine (Fig.3) consists of an engine and a working machine. A combustion chamber (9), in which compressed air is mixed with fuel and burned, is connected between the inlet duct of the engine and the outlet duct of the machine. The axes of the engine and the working machine are connected to one another in a gearbox (1o). With the same turbine rotor size, the axis of the engine rotates faster than the axis of the working machine. The difference between the rotational forces is the drive power of the internal combustion engine.
PCT/DE1996/002191 1995-11-22 1996-11-20 Power engine - working machine with turbine rotor WO1997019255A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU17658/97A AU1765897A (en) 1995-11-22 1996-11-20 Power engine - working machine with turbine rotor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19543572.9 1995-11-22
DE1995143572 DE19543572A1 (en) 1995-11-22 1995-11-22 Power and work machine with turbine runner

Publications (2)

Publication Number Publication Date
WO1997019255A2 true WO1997019255A2 (en) 1997-05-29
WO1997019255A3 WO1997019255A3 (en) 1997-07-17

Family

ID=7778147

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE1996/002191 WO1997019255A2 (en) 1995-11-22 1996-11-20 Power engine - working machine with turbine rotor

Country Status (3)

Country Link
AU (1) AU1765897A (en)
DE (1) DE19543572A1 (en)
WO (1) WO1997019255A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8238879B2 (en) 2004-09-24 2012-08-07 Armstrong, Quinton Co. LLC Policy-based controls for wireless cameras

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2241122C2 (en) * 2002-08-19 2004-11-27 Леонид Аркадьевич Гурецкий Rotary machine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR66487E (en) * 1954-06-23 1957-03-08 Device usable as a torque converter, pump, compressor, engine counter, turbine, clutch and brake
GB1186345A (en) * 1966-04-27 1970-04-02 John Thomas Flitcroft A Rotary Fluid Motor or Pump
DE2147943A1 (en) * 1971-09-25 1973-03-29 August G Dipl Ing Dr In Monath CIRCULAR CHAMBER MOTOR
US4154208A (en) * 1975-07-05 1979-05-15 Eiichi Kunieda Rotary engine
DE8811623U1 (en) * 1988-09-14 1988-10-27 Bolle, Herta Combustion engine
DE4409212A1 (en) * 1994-03-18 1995-09-21 Christoph Stiller Double rotary piston IC engine for vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8238879B2 (en) 2004-09-24 2012-08-07 Armstrong, Quinton Co. LLC Policy-based controls for wireless cameras
US8660534B2 (en) 2004-09-24 2014-02-25 Armstrong, Quinton Co. LLC Policy based controls for wireless cameras

Also Published As

Publication number Publication date
DE19543572A1 (en) 1997-05-28
WO1997019255A3 (en) 1997-07-17
AU1765897A (en) 1997-06-11

Similar Documents

Publication Publication Date Title
DE19704786C1 (en) Device for compensating for alternating torques and vibrations in the drive train of a motor vehicle with an integrated starter generator
CH669428A5 (en)
DE3510492A1 (en) METHOD AND DEVICE FOR POWER TRANSFER
DE10223145B4 (en) Rotary engine
EP0532567A1 (en) Rotary piston internal combustion engine.
DE2207692C3 (en) Internal combustion engine assembly
DE102008026033B4 (en) Powertrain with a hydrodynamic machine
WO1997019255A2 (en) Power engine - working machine with turbine rotor
DE3717250A1 (en) SPIRAL-TYPE FLOWING MACHINE
EP0154205A1 (en) Explosions turbine
WO1995034750A1 (en) Internal-combustion engine, compressor or pump
EP1554496A1 (en) Compressor machine with two counter-rotating rotors
EP0087746A1 (en) Rotary piston supercharger driven by exhaust gases
DE3146782A1 (en) Rotary piston machine
EP2625427B1 (en) Fluid transmission
DE2226831A1 (en) DISPLACEMENT MACHINE
DE19837729A1 (en) Rotary piston machine working as pump, compressor, turbine or engine
DE29518546U1 (en) Power and work machine with turbine runner
DE19523736A1 (en) Internal combustion engine with rotary symmetrical cylinders - has cylinder cavity in form of even number of separate cylinder sectors each with its own piston
DE2607376A1 (en) Rotary piston IC engine - uses compression and work pistons on common shaft impelling compressed air into combustion chambers
DE69304310T2 (en) turbine
DE102018125624A1 (en) Rotary piston machine and method for producing a seal in a rotary piston machine
EP0556563A2 (en) Internal combustion engine
EP0530771A1 (en) Rotary engine
DE2129059A1 (en) Antnebsmotorsystem, especially with a rotary piston engine

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AL AM AU BA BB BG BR CA CN CU CZ EE FI GE HU IL IS JP KG KP KR LC LK LR LT LV MD MG MK MN MX NO NZ PL RO SG SI SK TR TT UA US UZ VN AM AZ BY KG KZ MD RU TJ TM

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): KE LS MW SD SZ UG AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN ML MR NE SN TD TG

AK Designated states

Kind code of ref document: A3

Designated state(s): AL AM AU BA BB BG BR CA CN CU CZ EE FI GE HU IL IS JP KG KP KR LC LK LR LT LV MD MG MK MN MX NO NZ PL RO SG SI SK TR TT UA US UZ VN AM AZ BY KG KZ MD RU TJ TM

AL Designated countries for regional patents

Kind code of ref document: A3

Designated state(s): KE LS MW SD SZ UG AT BE CH DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN ML MR NE SN TD TG

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: JP

Ref document number: 97519284

Format of ref document f/p: F

122 Ep: pct application non-entry in european phase
NENP Non-entry into the national phase

Ref country code: CA