FR1238098A - Axial turbo-machine, preferably axial compressor, comprising at least two crowns of adjustable blades, in particular guide blades - Google Patents

Axial turbo-machine, preferably axial compressor, comprising at least two crowns of adjustable blades, in particular guide blades

Info

Publication number
FR1238098A
FR1238098A FR807897A FR807897A FR1238098A FR 1238098 A FR1238098 A FR 1238098A FR 807897 A FR807897 A FR 807897A FR 807897 A FR807897 A FR 807897A FR 1238098 A FR1238098 A FR 1238098A
Authority
FR
France
Prior art keywords
blades
axial
crowns
machine
turbo
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
FR807897A
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
Application filed by Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Application granted granted Critical
Publication of FR1238098A publication Critical patent/FR1238098A/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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
FR807897A 1958-10-30 1959-10-19 Axial turbo-machine, preferably axial compressor, comprising at least two crowns of adjustable blades, in particular guide blades Expired FR1238098A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1238098X 1958-10-30

Publications (1)

Publication Number Publication Date
FR1238098A true FR1238098A (en) 1960-08-05

Family

ID=7735756

Family Applications (1)

Application Number Title Priority Date Filing Date
FR807897A Expired FR1238098A (en) 1958-10-30 1959-10-19 Axial turbo-machine, preferably axial compressor, comprising at least two crowns of adjustable blades, in particular guide blades

Country Status (1)

Country Link
FR (1) FR1238098A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3508839A (en) * 1968-01-15 1970-04-28 Sulzer Ag Plural-stage axial compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3508839A (en) * 1968-01-15 1970-04-28 Sulzer Ag Plural-stage axial compressor

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