FR1399924A - Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine - Google Patents

Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine

Info

Publication number
FR1399924A
FR1399924A FR979514A FR979514A FR1399924A FR 1399924 A FR1399924 A FR 1399924A FR 979514 A FR979514 A FR 979514A FR 979514 A FR979514 A FR 979514A FR 1399924 A FR1399924 A FR 1399924A
Authority
FR
France
Prior art keywords
axial
turbine
suppressing
loss
radial gap
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
FR979514A
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.)
Licentia Patent Verwaltungs GmbH
Original Assignee
Licentia Patent Verwaltungs 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
Priority claimed from DE1963L0045236 external-priority patent/DE1239889B/en
Application filed by Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Priority to FR979514A priority Critical patent/FR1399924A/en
Application granted granted Critical
Publication of FR1399924A publication Critical patent/FR1399924A/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
    • F01D11/005—Sealing means between non relatively rotating elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR979514A 1963-06-28 1964-06-24 Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine Expired FR1399924A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR979514A FR1399924A (en) 1963-06-28 1964-06-24 Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1963L0045236 DE1239889B (en) 1963-06-28 1963-06-28 Inlet guide vane ring for axial turbines, in particular axial gas turbines, with radially resiliently pressed ring segments
FR979514A FR1399924A (en) 1963-06-28 1964-06-24 Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine

Publications (1)

Publication Number Publication Date
FR1399924A true FR1399924A (en) 1965-05-21

Family

ID=25985701

Family Applications (1)

Application Number Title Priority Date Filing Date
FR979514A Expired FR1399924A (en) 1963-06-28 1964-06-24 Device for suppressing a loss of radial gap in an axial turbine, in particular an axial gas turbine

Country Status (1)

Country Link
FR (1) FR1399924A (en)

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