FR996476A - Cylinder for gas turbines - Google Patents

Cylinder for gas turbines

Info

Publication number
FR996476A
FR996476A FR996476DA FR996476A FR 996476 A FR996476 A FR 996476A FR 996476D A FR996476D A FR 996476DA FR 996476 A FR996476 A FR 996476A
Authority
FR
France
Prior art keywords
cylinder
gas turbines
turbines
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.)
Expired
Application number
Other languages
French (fr)
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.)
Compagnie Electro Mecanique SA
Original Assignee
Compagnie Electro Mecanique SA
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 Compagnie Electro Mecanique SA filed Critical Compagnie Electro Mecanique SA
Application granted granted Critical
Publication of FR996476A publication Critical patent/FR996476A/en
Expired 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
    • F01D9/042—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
    • 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
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR996476D 1949-10-01 1949-10-01 Cylinder for gas turbines Expired FR996476A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR996476T 1949-10-01

Publications (1)

Publication Number Publication Date
FR996476A true FR996476A (en) 1951-12-19

Family

ID=9557898

Family Applications (1)

Application Number Title Priority Date Filing Date
FR996476D Expired FR996476A (en) 1949-10-01 1949-10-01 Cylinder for gas turbines

Country Status (1)

Country Link
FR (1) FR996476A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4199300A (en) * 1977-03-17 1980-04-22 Rolls-Royce Limited Shroud ring aerofoil capture
EP0186389A1 (en) * 1984-12-14 1986-07-02 The Garrett Corporation Turbocharger system and method of controlling heat transfer
EP1508673A2 (en) * 2003-08-18 2005-02-23 General Electric Company Methods for fabricating gas turbine engines
EP2159377A1 (en) * 2008-08-27 2010-03-03 Siemens Aktiengesellschaft Stator vane support for a gas turbine and corresponding gas turbine plant
EP2194235A1 (en) * 2008-12-05 2010-06-09 Siemens Aktiengesellschaft Housing component for an axial turbo engine with passive seam control, gas turbine with the housing component and method for retrofitting an existing housing component

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4199300A (en) * 1977-03-17 1980-04-22 Rolls-Royce Limited Shroud ring aerofoil capture
EP0186389A1 (en) * 1984-12-14 1986-07-02 The Garrett Corporation Turbocharger system and method of controlling heat transfer
EP1508673A2 (en) * 2003-08-18 2005-02-23 General Electric Company Methods for fabricating gas turbine engines
EP1508673A3 (en) * 2003-08-18 2007-06-13 General Electric Company Methods for fabricating gas turbine engines
EP2159377A1 (en) * 2008-08-27 2010-03-03 Siemens Aktiengesellschaft Stator vane support for a gas turbine and corresponding gas turbine plant
EP2194235A1 (en) * 2008-12-05 2010-06-09 Siemens Aktiengesellschaft Housing component for an axial turbo engine with passive seam control, gas turbine with the housing component and method for retrofitting an existing housing component

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