CH395142A - Multi-stage, axially loaded steam or gas turbine - Google Patents
Multi-stage, axially loaded steam or gas turbineInfo
- Publication number
 - CH395142A CH395142A CH1048161A CH1048161A CH395142A CH 395142 A CH395142 A CH 395142A CH 1048161 A CH1048161 A CH 1048161A CH 1048161 A CH1048161 A CH 1048161A CH 395142 A CH395142 A CH 395142A
 - Authority
 - CH
 - Switzerland
 - Prior art keywords
 - stage
 - gas turbine
 - axially loaded
 - loaded steam
 - steam
 - Prior art date
 
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
 - F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
 - F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
 - F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
 - F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
 
 - 
        
- 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
 - F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
 - F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
 - F01D25/246—Fastening of diaphragms or stator-rings
 
 - 
        
- 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
 - F01D9/00—Stators
 - F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
 - F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
 - F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
 
 - 
        
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
 - F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
 - F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
 - F05D2240/00—Components
 - F05D2240/10—Stators
 - F05D2240/11—Shroud seal segments
 
 
Landscapes
- Engineering & Computer Science (AREA)
 - Mechanical Engineering (AREA)
 - General Engineering & Computer Science (AREA)
 - Turbine Rotor Nozzle Sealing (AREA)
 
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title | 
|---|---|---|---|
| DEL37127A DE1138071B (en) | 1960-09-28 | 1960-09-28 | Multi-stage axial turbine | 
| DEL38097A DE1140945B (en) | 1960-09-28 | 1961-02-01 | Multi-stage, axially loaded constant pressure or overpressure turbine | 
| DEL38385A DE1140946B (en) | 1960-09-28 | 1961-03-07 | Multi-stage, axially loaded constant pressure or overpressure turbine | 
Publications (1)
| Publication Number | Publication Date | 
|---|---|
| CH395142A true CH395142A (en) | 1965-07-15 | 
Family
ID=27211396
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date | 
|---|---|---|---|
| CH1048161A CH395142A (en) | 1960-09-28 | 1961-09-07 | Multi-stage, axially loaded steam or gas turbine | 
Country Status (5)
| Country | Link | 
|---|---|
| BE (1) | BE608497A (en) | 
| CH (1) | CH395142A (en) | 
| DE (3) | DE1138071B (en) | 
| GB (1) | GB953931A (en) | 
| NL (1) | NL269161A (en) | 
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| US4643636A (en) * | 1985-07-22 | 1987-02-17 | Avco Corporation | Ceramic nozzle assembly for gas turbine engine | 
| EP0608080A1 (en) * | 1993-01-21 | 1994-07-27 | General Electric Company | Positioning means for a turbo engine liner | 
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| DE1239889B (en) * | 1963-06-28 | 1967-05-03 | Licentia Gmbh | Inlet guide vane ring for axial turbines, in particular axial gas turbines, with radially resiliently pressed ring segments | 
| US4247248A (en) * | 1978-12-20 | 1981-01-27 | United Technologies Corporation | Outer air seal support structure for gas turbine engine | 
| FR2683851A1 (en) * | 1991-11-20 | 1993-05-21 | Snecma | TURBOMACHINE EQUIPPED WITH MEANS TO FACILITATE THE ADJUSTMENT OF THE GAMES OF THE STATOR INPUT STATOR AND ROTOR. | 
| GB0319002D0 (en) * | 2003-05-13 | 2003-09-17 | Alstom Switzerland Ltd | Improvements in or relating to steam turbines | 
| US8021103B2 (en) * | 2008-10-29 | 2011-09-20 | General Electric Company | Pressure activated flow path seal for a steam turbine | 
| USD873874S1 (en) | 2012-09-28 | 2020-01-28 | Dürr Systems Ag | Axial turbine housing for a rotary atomizer for a painting robot | 
| EP3339581A1 (en) * | 2016-12-22 | 2018-06-27 | Ansaldo Energia S.p.A. | Sealing system for a rotating machine | 
| CN109555564B (en) * | 2019-01-25 | 2023-08-29 | 沈阳航空航天大学 | Brush type sealing structure with magnet and adjustable radial gap between brush filament bundle and rotor surface | 
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| FR392896A (en) * | 1907-08-09 | 1908-12-08 | George Westinghouse | Improvements in turbines operated by the pressure of an elastic fluid | 
| DE1055548B (en) * | 1956-06-08 | 1959-04-23 | Siemens Ag | Overpressure axial turbine with pot housing | 
- 
        0
        
- NL NL269161D patent/NL269161A/xx unknown
 
 - 
        1960
        
- 1960-09-28 DE DEL37127A patent/DE1138071B/en active Pending
 
 - 
        1961
        
- 1961-02-01 DE DEL38097A patent/DE1140945B/en active Pending
 - 1961-03-07 DE DEL38385A patent/DE1140946B/en active Pending
 - 1961-09-07 CH CH1048161A patent/CH395142A/en unknown
 - 1961-09-25 BE BE608497A patent/BE608497A/xx unknown
 - 1961-09-27 GB GB3467261A patent/GB953931A/en not_active Expired
 
 
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title | 
|---|---|---|---|---|
| US4643636A (en) * | 1985-07-22 | 1987-02-17 | Avco Corporation | Ceramic nozzle assembly for gas turbine engine | 
| EP0608080A1 (en) * | 1993-01-21 | 1994-07-27 | General Electric Company | Positioning means for a turbo engine liner | 
Also Published As
| Publication number | Publication date | 
|---|---|
| DE1140945B (en) | 1962-12-13 | 
| DE1138071B (en) | 1962-10-18 | 
| DE1140946B (en) | 1962-12-13 | 
| NL269161A (en) | |
| BE608497A (en) | 1962-01-15 | 
| GB953931A (en) | 1964-04-02 | 
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