CH405015A - Multi-stage axial turbine, in particular axial gas turbine - Google Patents

Multi-stage axial turbine, in particular axial gas turbine

Info

Publication number
CH405015A
CH405015A CH1222263A CH1222263A CH405015A CH 405015 A CH405015 A CH 405015A CH 1222263 A CH1222263 A CH 1222263A CH 1222263 A CH1222263 A CH 1222263A CH 405015 A CH405015 A CH 405015A
Authority
CH
Switzerland
Prior art keywords
turbine
axial
stage
gas turbine
axial gas
Prior art date
Application number
CH1222263A
Other languages
German (de)
Inventor
Wittstock Gerhard
Original Assignee
Licentia Gmbh
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 Licentia Gmbh filed Critical Licentia Gmbh
Publication of CH405015A publication Critical patent/CH405015A/en

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
    • 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
    • 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
    • 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)
CH1222263A 1962-10-09 1963-10-03 Multi-stage axial turbine, in particular axial gas turbine CH405015A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1962L0043154 DE1296877B (en) 1962-10-09 1962-10-09 Housing of a multi-stage axial turbine, in particular a gas turbine

Publications (1)

Publication Number Publication Date
CH405015A true CH405015A (en) 1965-12-31

Family

ID=7270180

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1222263A CH405015A (en) 1962-10-09 1963-10-03 Multi-stage axial turbine, in particular axial gas turbine

Country Status (3)

Country Link
CH (1) CH405015A (en)
DE (1) DE1296877B (en)
GB (1) GB1051244A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007059220A1 (en) * 2007-12-07 2009-06-10 Rolls-Royce Deutschland Ltd & Co Kg Guide vane ring for thermal fluid flow engine of aircraft, has hooks inserted into recesses of housing parts, and grooves arranged laterally near hooks, where each hook is angularly attached at radial outer guide vane base of guide vane

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH633346A5 (en) * 1978-03-29 1982-11-30 Bbc Brown Boveri & Cie GUIDE BLADE SUPPORT ON A GAS TURBINE.
GB8724537D0 (en) * 1987-10-20 1987-11-25 Rolls Royce Plc Interturbine duct
US5131811A (en) * 1990-09-12 1992-07-21 United Technologies Corporation Fastener mounting for multi-stage compressor
US5297932A (en) * 1990-09-12 1994-03-29 United Technologies Corporation Fastener for multi-stage compressor
EP2184445A1 (en) 2008-11-05 2010-05-12 Siemens Aktiengesellschaft Axial segmented vane support for a gas turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE969599C (en) * 1943-05-27 1958-06-19 Holzwarth Gasturbinen G M B H Cooled nozzle body for centrifugal machines, especially exhaust gas turbines
FR957575A (en) * 1946-10-02 1950-02-23
FR965713A (en) * 1947-05-07 1950-09-20
DE974589C (en) * 1951-12-13 1961-02-23 Siemens Ag Steam or gas turbine with an inner housing which is installed centrally in an outer housing so that it can move in heat to accommodate guide disks
US2858104A (en) * 1954-02-04 1958-10-28 A V Roe Canada Ltd Adjustable gas turbine shroud ring segments
FR1301686A (en) * 1960-09-28 1962-08-17 Licentia Gmbh Multistage axial type gas or steam turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007059220A1 (en) * 2007-12-07 2009-06-10 Rolls-Royce Deutschland Ltd & Co Kg Guide vane ring for thermal fluid flow engine of aircraft, has hooks inserted into recesses of housing parts, and grooves arranged laterally near hooks, where each hook is angularly attached at radial outer guide vane base of guide vane

Also Published As

Publication number Publication date
DE1296877B (en) 1969-06-04
GB1051244A (en)

Similar Documents

Publication Publication Date Title
CH417837A (en) Auxiliary blading on the turbomachine
CH411463A (en) Gas turbine plant
CH439334A (en) Multi-stage axial flow turbine
AT241913B (en) Gas turbine plant
CH390948A (en) Gas turbine
CH369250A (en) Axial turbo compressor
CH413500A (en) Countercurrent gas turbine engine
CH395142A (en) Multi-stage, axially loaded steam or gas turbine
NL146578B (en) COMPRESSOR ROTOR.
CH405015A (en) Multi-stage axial turbine, in particular axial gas turbine
BE613415A (en) Turbomachinery reactor
FR1326037A (en) Turbine
FR1319432A (en) Turbo extractor
CH385633A (en) Turbo machine
CH427415A (en) Axial turbine machine stator, in particular axial gas turbine stator
CH355327A (en) Axial turbine, in particular gas turbine
CH411462A (en) Gas turbine system
CH380753A (en) Multi-stage, axially loaded impulse turbine
BE587418A (en) Turbine.
DK104769C (en) Gas turbine plant.
AT245716B (en) Multi-stage axial compressor
CH402268A (en) Axial compressor
FR1336676A (en) Radial compressor
FR1275985A (en) Equi-pressure, multi-stage turbine, axially fed
AT250398B (en) Large capacity steam or gas turbine