DE2052665A1 - - Google Patents

Info

Publication number
DE2052665A1
DE2052665A1 DE19702052665 DE2052665A DE2052665A1 DE 2052665 A1 DE2052665 A1 DE 2052665A1 DE 19702052665 DE19702052665 DE 19702052665 DE 2052665 A DE2052665 A DE 2052665A DE 2052665 A1 DE2052665 A1 DE 2052665A1
Authority
DE
Germany
Prior art keywords
turbine
blades
stator
nozzle
gas
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
Application number
DE19702052665
Other languages
German (de)
English (en)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE2052665A1 publication Critical patent/DE2052665A1/de
Pending 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
DE19702052665 1969-10-27 1970-10-27 Pending DE2052665A1 (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB52558/69A GB1275970A (en) 1969-10-27 1969-10-27 Turbine nozzle guide or stator vane assembly

Publications (1)

Publication Number Publication Date
DE2052665A1 true DE2052665A1 (zh) 1971-05-13

Family

ID=10464377

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19702052665 Pending DE2052665A1 (zh) 1969-10-27 1970-10-27

Country Status (3)

Country Link
DE (1) DE2052665A1 (zh)
FR (1) FR2066634A5 (zh)
GB (1) GB1275970A (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0161203A1 (en) * 1984-05-11 1985-11-13 United Technologies Corporation First stage turbine vane support structure

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2110306B (en) * 1981-11-26 1985-02-13 Roll Royce Limited Turbomachine housing
US4553386A (en) * 1982-02-04 1985-11-19 Martin Berg Combustion chamber for dual turbine wheel engine
US5486091A (en) * 1994-04-19 1996-01-23 United Technologies Corporation Gas turbine airfoil clocking
GB2420157B (en) * 2003-05-14 2006-06-28 Rolls Royce Plc A stator vane assembly for a turbomachine
DE102012001678A1 (de) 2012-01-28 2013-08-01 Yakiv Blyumin Verfahren und Vorrichtung zur Erhöhung der Arbeitsfähigkeit der Arbeitsschaufeln von Hochdruckgasturbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0161203A1 (en) * 1984-05-11 1985-11-13 United Technologies Corporation First stage turbine vane support structure

Also Published As

Publication number Publication date
FR2066634A5 (zh) 1971-08-06
GB1275970A (en) 1972-06-01

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