FR1208697A - Turbomachine à diffuseur radial - Google Patents

Turbomachine à diffuseur radial

Info

Publication number
FR1208697A
FR1208697A FR1208697DA FR1208697A FR 1208697 A FR1208697 A FR 1208697A FR 1208697D A FR1208697D A FR 1208697DA FR 1208697 A FR1208697 A FR 1208697A
Authority
FR
France
Prior art keywords
turbomachine
radial diffuser
diffuser
radial
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
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.)
Sulzer AG
Original Assignee
Sulzer AG
Sulzer Freres 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 Sulzer AG, Sulzer Freres SA filed Critical Sulzer AG
Application granted granted Critical
Publication of FR1208697A publication Critical patent/FR1208697A/fr
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
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1208697D 1957-12-13 1958-11-17 Turbomachine à diffuseur radial Expired FR1208697A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1208697X 1957-12-13

Publications (1)

Publication Number Publication Date
FR1208697A true FR1208697A (fr) 1960-02-25

Family

ID=4563093

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1208697D Expired FR1208697A (fr) 1957-12-13 1958-11-17 Turbomachine à diffuseur radial

Country Status (2)

Country Link
CH (1) CH353837A (fr)
FR (1) FR1208697A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4544325A (en) * 1980-10-22 1985-10-01 Teledyne Industries, Inc. Variable geometry device for turbine compressor outlet

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5116197A (en) * 1990-10-31 1992-05-26 York International Corporation Variable geometry diffuser

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4544325A (en) * 1980-10-22 1985-10-01 Teledyne Industries, Inc. Variable geometry device for turbine compressor outlet

Also Published As

Publication number Publication date
CH353837A (de) 1961-04-30

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