IT1201062B - Perfezionamento nelle palette di statore per motori a turbina a gas - Google Patents

Perfezionamento nelle palette di statore per motori a turbina a gas

Info

Publication number
IT1201062B
IT1201062B IT4853076A IT4853076A IT1201062B IT 1201062 B IT1201062 B IT 1201062B IT 4853076 A IT4853076 A IT 4853076A IT 4853076 A IT4853076 A IT 4853076A IT 1201062 B IT1201062 B IT 1201062B
Authority
IT
Italy
Prior art keywords
palette
stator
improvement
gas turbine
turbine engines
Prior art date
Application number
IT4853076A
Other languages
English (en)
Original Assignee
Rolls Royce 1971 Ltd
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 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1201062B publication Critical patent/IT1201062B/it

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT4853076A 1975-03-14 1976-03-11 Perfezionamento nelle palette di statore per motori a turbina a gas IT1201062B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1064675A GB1605309A (en) 1975-03-14 1975-03-14 Stator blade for a gas turbine engine

Publications (1)

Publication Number Publication Date
IT1201062B true IT1201062B (it) 1989-01-27

Family

ID=9971682

Family Applications (1)

Application Number Title Priority Date Filing Date
IT4853076A IT1201062B (it) 1975-03-14 1976-03-11 Perfezionamento nelle palette di statore per motori a turbina a gas

Country Status (4)

Country Link
DE (1) DE2609702C1 (it)
FR (1) FR2624555A1 (it)
GB (1) GB1605309A (it)
IT (1) IT1201062B (it)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1073827B1 (de) * 1998-04-21 2003-10-08 Siemens Aktiengesellschaft Turbinenschaufel
EP1329593B1 (de) 2002-01-17 2005-03-23 Siemens Aktiengesellschaft Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform
US20050220622A1 (en) * 2004-03-31 2005-10-06 General Electric Company Integral covered nozzle with attached overcover
DE102005013794A1 (de) * 2005-03-24 2006-09-28 Alstom Technology Ltd. Leitschaufel für eine Strömungsrotationsmaschine
EP2422052A4 (en) * 2009-04-23 2013-01-02 Volvo Aero Corp METHOD FOR MANUFACTURING GAS TURBINE ENGINE COMPONENT AND COMPONENT FOR GAS TURBINE ENGINE

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2264877A (en) * 1940-11-15 1941-12-02 Gen Electric Elastic fluid turbine diaphragm
US2919891A (en) * 1957-06-17 1960-01-05 Gen Electric Gas turbine diaphragm assembly
DE1080352B (de) * 1957-10-21 1960-04-21 Bmw Triebwerkbau Ges M B H Kuehleinrichtung fuer Gasturbinen, insbesondere fuer mit Schweroel betriebene Gasturbinen
GB938189A (en) * 1960-10-29 1963-10-02 Ruston & Hornsby Ltd Improvements in the construction of turbine and compressor blade elements

Also Published As

Publication number Publication date
GB1605309A (en) 1989-02-01
FR2624555A1 (fr) 1989-06-16
DE2609702C1 (de) 1989-05-03

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