DE891165C - Turbine for gas and vapor propellants - Google Patents

Turbine for gas and vapor propellants

Info

Publication number
DE891165C
DE891165C DEH1936A DEH0001936A DE891165C DE 891165 C DE891165 C DE 891165C DE H1936 A DEH1936 A DE H1936A DE H0001936 A DEH0001936 A DE H0001936A DE 891165 C DE891165 C DE 891165C
Authority
DE
Germany
Prior art keywords
pressure
turbine
rotor
propellant
rotation
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.)
Expired
Application number
DEH1936A
Other languages
German (de)
Inventor
Alois Horner
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 DEH1936A priority Critical patent/DE891165C/en
Application granted granted Critical
Publication of DE891165C publication Critical patent/DE891165C/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/30—Non-positive-displacement machines or engines, e.g. steam turbines characterised by having a single rotor operable in either direction of rotation, e.g. by reversing of blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

Die Erfindung bezieht sich .auf Turbinen für gas-oder dampfförmige Treibmittel und . hat die Ausbildung diese Läufers ;als Druckmuldenläüfer und dessen Anordnung im Turbinengehäuse zum Gegenstand. , -Der Treibmittelerzeniger kann von beliebiger Bauart sein wind gehört nicht zur Erfindung.The invention relates .auf turbines for gas or vapor Propellant and. has the training of this runner; as a pressure sump runner and its Arrangement in the turbine housing to the subject. , -The propellant ore can from Any type of wind is not part of the invention.

In der Zeichnung ist die Turbine dargestellt,-Abb. -i zeigt einten Längsschnitt, Abb. 2 eine Ansicht, Abb.3 einen Querschnitt mit der Ansicht des Druek=uldenläufers für Linkslauf und Abb . 4 das gleiche wie Ab-b. 3, jedoch für Rechtslauf.In the drawing the turbine is shown, -Fig. -i shows one Longitudinal section, Fig. 2 a view, Fig. 3 a cross section with the view of the pressure runner for left-hand rotation and Fig. 4 the same as Ab-b. 3, but for clockwise rotation.

Das Gehäuse i der Turbine weist zwei -zylindrisiche Innenräume mit verschiedenen Durchmess ern iawf. Mit der Welle 6 fest verbunden ist der sbufenfiörmige Ro,tior 2, in .dessen Stufen mit ebenfalls unterschiedlichen Durchmiessern je zwei Reihen Druckmulden 5 für die zwei eingearbeitet sind. Die Form der Druckmulden sowie die Zuführung,der vom Treibstofferzeuger kommenden Rohrleitungen zeigen die Abb.3 und q.. Eine Rohrverbindung 7 (Abt. 3 und 4) dient zur weiteren Ausnutzung des auf die Druckmulden einströmenden Treibmittels bis zu .dessen völliger Entspannung durch die Überleitung 7 auf eine vorauseilende Druckmuldie 5. Der entspannte Betriebsstoff verläßt 'bei 8 ,die Turbine.The housing of the turbine has two cylindrical interiors with different diameters iawf. The stepped roof 2 is firmly connected to the shaft 6, with two rows of pressure troughs 5 for each of the two rows of pressure troughs also being incorporated in its steps with likewise different diameters. The shape of the pressure troughs as well as the supply of the pipes coming from the fuel generator are shown in Fig.3 and q .. A pipe connection 7 (section 3 and 4) is used to further utilize the propellant flowing into the pressure troughs until it is completely relaxed by the Transfer 7 to a leading pressure trough 5. The relaxed fuel leaves the turbine at 8.

Wird eines der in den vom Treibstofferzeuger kommenden Rohrleitungen liegendem, Äbisperrventile der gewünschten Drehrichtung geöffnet, so strömt das untere Druck im Treibstofferzeuger entwickelte Treibmittel biet 4 Uuf die Druckmuldien 5, wodurch der Rotor 2 in-Bewegung gebracht wird. Durch ,die Bewegung des Rcstdrs ä sichließt sich abwechslungsweise die Druckleitung 4 ab. Das auf die Druckmulden 5 einströmende Treibmittel wird seine Letzte Spannkraft mittels der Rohrleitung 7 (Abt.. 3 -und 4) auf eine vorauseilende, Druckmulde übertragen und nach Entspannwig bei 8 die Turbine verlassen.Becomes one of the pipes coming from the fuel producer horizontal shut-off valves opened in the desired direction of rotation, that's how it flows Propellant developed under pressure in the fuel generator offers 4 Uuf the pressure molds 5, whereby the rotor 2 is set in motion. By, the movement of the back door The pressure line 4 closes alternately. That on the pressure hollows 5 influx of propellant is its last tension by means of the pipeline 7 (Dept. 3 - and 4) transferred to a leading pressure depression and after Entspannwig leave the turbine at 8.

Claims (1)

PATENTANSPRÜCHE: i. Turbine für gas- Bader dampfförmige Treibmittel, @daduxch gekennzeichnet, daß das Turbinengehäuse (i) leinen stufenförmig abgesetzten zylindrischen Innenraum mit zwei verschiedenen Innendurchmessern ,aufweist, in welchem ein stufenförmiger Rotor (2) angeordnet ist, auf ,dessen einer Stute Druckmulden für die eine Drehrichtung Lund ,auf .dessen anderer Stufe Druckmulden für :die andere Direhrichtung in den Auißenkranz des Rotors eingearbeitet sind. z. Turbine für ;gas- Moder dampfförmige Treibmittel nach Anspruch i, ,dadurch gekennzeichnet, @daß idne TYeibmittelz@uleitung (4) infolge der Drehbewegung dies Rotors (2) und die sich zwischen zwei Druckmulden befindliche Fläche periodenweise schließt, und da,ßzur vollständigen Ausnutzung des einströmenden Treibmittels je Roriorstufe eine in seiner vorauseilenden Druckmulde endende Umführungslei:tung (7) angeordnet ist. Angezogene Dru_ks_@chriften: IDeuitsche Patentschriften Nr. ^63i 255, 587 255, 352 690, 223 986.
PATENT CLAIMS: i. Turbine for gas baths vaporous propellant, @daduxch characterized in that the turbine housing (i) has a stepped cylindrical interior with two different inner diameters, in which a stepped rotor (2) is arranged, one of which has pressure hollows for one Direction of rotation Lund, on the other stage of which pressure hollows for: the other direction of rotation are incorporated into the outer rim of the rotor. z. Turbine for; gaseous and vaporous propellants according to claim 1, characterized in that the idne TYeibmittelz @ uleitung (4) as a result of the rotary movement of the rotor (2) and the area between two pressure troughs periodically closes, and there, ß for full utilization of the inflowing propellant per Roriorstufe a bypass line (7) ending in its leading pressure trough is arranged. Dru_ks_ @ fonts attracted: European patent specifications No. ^ 63i 255, 587 255, 352 690, 223 986.
DEH1936A 1950-03-09 1950-03-09 Turbine for gas and vapor propellants Expired DE891165C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEH1936A DE891165C (en) 1950-03-09 1950-03-09 Turbine for gas and vapor propellants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEH1936A DE891165C (en) 1950-03-09 1950-03-09 Turbine for gas and vapor propellants

Publications (1)

Publication Number Publication Date
DE891165C true DE891165C (en) 1953-09-24

Family

ID=7142846

Family Applications (1)

Application Number Title Priority Date Filing Date
DEH1936A Expired DE891165C (en) 1950-03-09 1950-03-09 Turbine for gas and vapor propellants

Country Status (1)

Country Link
DE (1) DE891165C (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2446924A1 (en) * 1979-01-19 1980-08-14 Brenier Maurice IC engine with cylindrical rotor - has stator and a rotor with grooves for gas ignition and expansion and chambers in rotor to contain gas
WO2001098633A1 (en) * 2000-06-23 2001-12-27 Vincent Huret Fluid-propelled motor
WO2004025085A1 (en) * 2002-09-12 2004-03-25 Vicus William Smith Flow actuated drive means
WO2016020742A1 (en) * 2014-08-06 2016-02-11 Mariani Augusto Pressurized air engine for electric power generators
CN106930825A (en) * 2016-05-13 2017-07-07 谭智 Without compression engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE223986C (en) *
DE352690C (en) * 1919-11-25 1922-05-03 Edward Louis Girard Control for explosion turbines
DE587255C (en) * 1928-07-05 1933-11-01 Hermann Nitzsche Internal combustion turbine for liquid or gaseous fuels
DE631255C (en) * 1936-06-16 Heinrich Mangels Combustion gas turbine for operation with an oxygen-fuel mixture

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE223986C (en) *
DE631255C (en) * 1936-06-16 Heinrich Mangels Combustion gas turbine for operation with an oxygen-fuel mixture
DE352690C (en) * 1919-11-25 1922-05-03 Edward Louis Girard Control for explosion turbines
DE587255C (en) * 1928-07-05 1933-11-01 Hermann Nitzsche Internal combustion turbine for liquid or gaseous fuels

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2446924A1 (en) * 1979-01-19 1980-08-14 Brenier Maurice IC engine with cylindrical rotor - has stator and a rotor with grooves for gas ignition and expansion and chambers in rotor to contain gas
WO2001098633A1 (en) * 2000-06-23 2001-12-27 Vincent Huret Fluid-propelled motor
FR2810699A1 (en) * 2000-06-23 2001-12-28 Vincent Huret Air driven low torque motor includes compressed air injector acting on teeth around edge of driven wheel
WO2004025085A1 (en) * 2002-09-12 2004-03-25 Vicus William Smith Flow actuated drive means
US7229244B2 (en) 2002-09-12 2007-06-12 William Vicus Smith Fluid flow actuated drive means
WO2016020742A1 (en) * 2014-08-06 2016-02-11 Mariani Augusto Pressurized air engine for electric power generators
CN106930825A (en) * 2016-05-13 2017-07-07 谭智 Without compression engine

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