DE1128706B - Gas turbine system with a drive shaft of the power turbine extending through the compressor drive turbine - Google Patents
Gas turbine system with a drive shaft of the power turbine extending through the compressor drive turbineInfo
- Publication number
- DE1128706B DE1128706B DEA28822A DEA0028822A DE1128706B DE 1128706 B DE1128706 B DE 1128706B DE A28822 A DEA28822 A DE A28822A DE A0028822 A DEA0028822 A DE A0028822A DE 1128706 B DE1128706 B DE 1128706B
- Authority
- DE
- Germany
- Prior art keywords
- turbine
- compressor drive
- power
- extending
- power turbine
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
- F02C3/145—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chamber being in the reverse flow-type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Gasturbinenanlage mit einer sich durch die Verdichterantriebsturbine erstreckenden Antriebswelle der Nutzleistungsturbine Bekannt ist eine Gasturbinenanlage mit einer Nutzleistungsturbine und einer Verdichterantriebsturbine, mit einer die Turbinen umgebenden ringförmigen Brennkammer und mit einer sich durch die Verdichterantriebsturbine erstreckenden Abtriebswelle der Nutzleistungsturbine. Bei dieser bekannten Anlage sind das Laufrad der Nutzleistungsturbine und die Abtriebswelle fest miteinander verbunden.Gas turbine system with a through the compressor drive turbine extending drive shaft of the power turbine A gas turbine system is known with a power turbine and a compressor drive turbine, with a die Turbines surrounding annular combustion chamber and with a through the compressor drive turbine extending output shaft of the power turbine. In this known system the impeller of the power turbine and the output shaft are fixed to one another tied together.
Aufgabe der Erfindung ist es, eine Gasturbinenanlage zu erstellen, bei der für Kontrollzwecke und für Reparaturarbeiten ein. leichter Zugang zum Inneren der Nutzleistungsturbine, der Verdichterantriebsturbine und der Brennkammer möglich ist.The object of the invention is to create a gas turbine system, at the for control purposes and for repair work. easy access to the interior the power turbine, the compressor drive turbine and the combustion chamber possible is.
Diese Aufgabe wird gemäß der Erfindung dadurch gelöst, daß eine leicht trennbare Verbindung zwischen dem Läufer der Nutzleistungsturbine und ihrer Abtriebswelle vorhanden ist. Durch diese Maßnahme ist es möglich, den kompletten Nutzleistungsturbinenabschnitt von der Abtriebswelle und damit von dem übrigen Anlagenteil leicht zu lösen und von dem an die Verdichterantriebsturbine angrenzenden Bereich zu entfernen, ohne daß die Nutzleistungsturbine in ihre Einzelteile zerlegt werden muß.This object is achieved according to the invention in that one easily separable connection between the rotor of the power turbine and its output shaft is available. This measure makes it possible to use the entire power turbine section easily detachable from the output shaft and thus from the rest of the system from the area adjacent to the compressor drive turbine without that the power turbine must be disassembled into its individual parts.
Eine beispielsweise Ausführungsform der Erfindung ist in der Zeichnung dargestellt, und zwar zeigt Fig. 1 eine zusammengebaute Gasturbinenanlage im Längsschnitt und Fig.2 eine auseinandergenommene Gasturbinenanlage in perspektivischer Ansicht, zum Teil geschnitten.An exemplary embodiment of the invention is shown in the drawing shown, namely Fig. 1 shows an assembled gas turbine plant in longitudinal section and FIG. 2 shows a disassembled gas turbine plant in a perspective view, partially cut.
Die Nutzleistungsturbine 1 und die Verdichterantriebsturbine 2 sind von einer ringförmigen Brennkammer 3 umgeben. Durch die Verdichterantriebsturbine 2 erstreckt sich die Abtriebswelle 4 der Nutzleistungsturbine 1. Gemäß der Erfindung ist eine leicht trennbare Verbindung 5 zwischen dem Läufer der Nutzleistungsturbine 1 und ihrer Abtriebswelle 4 vorhanden, um einen einfachen Zugang zum Inneren der Nutzleistungsturbine 1, der Verdichterantriebsturbine 2 und der Brennkammer 3 zu erreichen.The power turbine 1 and the compressor drive turbine 2 are surrounded by an annular combustion chamber 3. Through the compressor drive turbine 2 extends the output shaft 4 of the power turbine 1. According to the invention is an easily separable connection 5 between the rotor of the power turbine 1 and its output shaft 4 available for easy access to the interior of the Power turbine 1, the compressor drive turbine 2 and the combustion chamber 3 to reach.
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1128706XA | 1957-05-01 | 1957-05-01 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1128706B true DE1128706B (en) | 1962-04-26 |
Family
ID=22346282
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEA28822A Pending DE1128706B (en) | 1957-05-01 | 1958-02-04 | Gas turbine system with a drive shaft of the power turbine extending through the compressor drive turbine |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE1128706B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2364431A1 (en) * | 1972-12-26 | 1974-06-27 | Gen Electric | GAS TURBINE ENGINE WITH POWER TURBINE SYSTEM |
DE2507695A1 (en) * | 1974-02-25 | 1975-08-28 | Gen Electric | METHOD OF BALANCING A GAS TURBINE ENGINE |
US4989421A (en) * | 1987-06-19 | 1991-02-05 | Schmidt Walter R | Process for producing a patterned plush fabric as well as a multisystem circular knitting machine for carrying out the process |
US5167133A (en) * | 1987-06-19 | 1992-12-01 | Schmidt Walter R | Process for producing a patterned plush fabric as well as a multisystem circular knitting machine for carrying out the process |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH270945A (en) * | 1948-01-28 | 1950-09-30 | Rolls Royce | Gas turbine plant. |
US2638745A (en) * | 1943-04-01 | 1953-05-19 | Power Jets Res & Dev Ltd | Gas turbine combustor having tangential air inlets for primary and secondary air |
-
1958
- 1958-02-04 DE DEA28822A patent/DE1128706B/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2638745A (en) * | 1943-04-01 | 1953-05-19 | Power Jets Res & Dev Ltd | Gas turbine combustor having tangential air inlets for primary and secondary air |
CH270945A (en) * | 1948-01-28 | 1950-09-30 | Rolls Royce | Gas turbine plant. |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2364431A1 (en) * | 1972-12-26 | 1974-06-27 | Gen Electric | GAS TURBINE ENGINE WITH POWER TURBINE SYSTEM |
DE2507695A1 (en) * | 1974-02-25 | 1975-08-28 | Gen Electric | METHOD OF BALANCING A GAS TURBINE ENGINE |
US4989421A (en) * | 1987-06-19 | 1991-02-05 | Schmidt Walter R | Process for producing a patterned plush fabric as well as a multisystem circular knitting machine for carrying out the process |
US5167133A (en) * | 1987-06-19 | 1992-12-01 | Schmidt Walter R | Process for producing a patterned plush fabric as well as a multisystem circular knitting machine for carrying out the process |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE2849747A1 (en) | CERAMIC MATERIALS CONSTRUCTION AXIAL VANE FURNITURE FOR GAS TURBINES | |
DE1128706B (en) | Gas turbine system with a drive shaft of the power turbine extending through the compressor drive turbine | |
DE768041C (en) | Hot jet engine, in particular for propelling aircraft | |
DE582193C (en) | Device for adjusting the blades of turbines | |
DE2257076B2 (en) | Drum rotor for axial compressors | |
DE580853C (en) | Device for securing the connection of rotor parts of centrifugal machines | |
DE2616565C3 (en) | Centering support of a stack of several ceramic components of a gas turbine engine | |
DE829685C (en) | Attachment of the blades in the wheel disc, especially of exhaust gas turbines | |
DE3500447C2 (en) | Gas turbine jet engine | |
DE423310C (en) | Guide disc machined on all sides | |
DE514438C (en) | Piston compressor driven by an internal combustion engine | |
DE474936C (en) | Anchoring of cast housing walls through cast-in struts, especially for steam turbine housings | |
DE849328C (en) | Axial turbo expansion valve for gas turbines | |
DE858204C (en) | Screw ship or wheel ship driven by internal combustion engines | |
DE527499C (en) | Light alloy pistons | |
DE569806C (en) | Device for cooling gas turbine blades and vanes | |
DE460791C (en) | Multiple turbine made up of single turbines with radial inlet and outlet on a common shaft | |
DE906845C (en) | Runner for axially flowed through turbomachines, especially for multi-stage axial compressors and axial turbines of aircraft engines or the like. | |
DE603689C (en) | Steam chamber for counter-rotating turbines | |
DE559553C (en) | Construction of welded turbo blowers and compressors | |
DE852856C (en) | Single axle drive of vehicles, in particular locomotives, by a steam or gas turbine each | |
CH219485A (en) | Constant pressure gas turbine system. | |
AT94320B (en) | Turbine for elastic propellants. | |
DE1092730B (en) | Housing training for gas turbine engines | |
DE453079C (en) | Control device for radial steam or gas turbines |