FR1246176A - Axial compressor - Google Patents

Axial compressor

Info

Publication number
FR1246176A
FR1246176A FR783219A FR783219A FR1246176A FR 1246176 A FR1246176 A FR 1246176A FR 783219 A FR783219 A FR 783219A FR 783219 A FR783219 A FR 783219A FR 1246176 A FR1246176 A FR 1246176A
Authority
FR
France
Prior art keywords
axial compressor
compressor
axial
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
FR783219A
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.)
ENTWICKLUNGSBAU PIRNA VEB
Original Assignee
ENTWICKLUNGSBAU PIRNA VEB
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 ENTWICKLUNGSBAU PIRNA VEB filed Critical ENTWICKLUNGSBAU PIRNA VEB
Priority to FR783219A priority Critical patent/FR1246176A/en
Application granted granted Critical
Publication of FR1246176A publication Critical patent/FR1246176A/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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR783219A 1959-01-03 1959-01-03 Axial compressor Expired FR1246176A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR783219A FR1246176A (en) 1959-01-03 1959-01-03 Axial compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR783219A FR1246176A (en) 1959-01-03 1959-01-03 Axial compressor

Publications (1)

Publication Number Publication Date
FR1246176A true FR1246176A (en) 1960-11-18

Family

ID=8709860

Family Applications (1)

Application Number Title Priority Date Filing Date
FR783219A Expired FR1246176A (en) 1959-01-03 1959-01-03 Axial compressor

Country Status (1)

Country Link
FR (1) FR1246176A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439317A1 (en) * 1978-10-16 1980-05-16 United Technologies Corp METHOD AND DEVICE FOR CONTROLLING THE ANGLE OF TILTING OF THE BLADES OF A GAS TURBINE
EP0310851A1 (en) * 1987-09-30 1989-04-12 Siemens Aktiengesellschaft Adjusting mechanism
WO2003014532A1 (en) * 2001-08-03 2003-02-20 Honeywell International Inc. Actuator crank arm design for variable nozzle turbocharger
EP1672180A1 (en) * 2004-12-16 2006-06-21 Snecma Nozzle stage of a distributor actuated by a rotatable ring moved by electric motors
FR2982653A1 (en) * 2011-11-14 2013-05-17 Snecma CANNELE SHAFT TRANSMISSION SYSTEM.
EP4148236A1 (en) * 2021-09-14 2023-03-15 MTU Aero Engines AG Adjusting assembly for pivotable vanes of a turbomachine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439317A1 (en) * 1978-10-16 1980-05-16 United Technologies Corp METHOD AND DEVICE FOR CONTROLLING THE ANGLE OF TILTING OF THE BLADES OF A GAS TURBINE
EP0310851A1 (en) * 1987-09-30 1989-04-12 Siemens Aktiengesellschaft Adjusting mechanism
WO2003014532A1 (en) * 2001-08-03 2003-02-20 Honeywell International Inc. Actuator crank arm design for variable nozzle turbocharger
EP1672180A1 (en) * 2004-12-16 2006-06-21 Snecma Nozzle stage of a distributor actuated by a rotatable ring moved by electric motors
FR2879687A1 (en) * 2004-12-16 2006-06-23 Snecma Moteurs Sa STATOR TURBOMACHINE COMPRISING A RECTIFIER AUBES STAGE ACTED BY A ROTATING CROWN DISPLACED BY ELECTRIC MOTOR MEANS
US7393178B2 (en) 2004-12-16 2008-07-01 Snecma Stator vane stage actuated by a rotary actuator ring moved by electric motor means
FR2982653A1 (en) * 2011-11-14 2013-05-17 Snecma CANNELE SHAFT TRANSMISSION SYSTEM.
EP4148236A1 (en) * 2021-09-14 2023-03-15 MTU Aero Engines AG Adjusting assembly for pivotable vanes of a turbomachine
US11891918B2 (en) 2021-09-14 2024-02-06 MTU Aero Engines AG Adjustment assembly for adjustable blades or vanes of a turbomachine

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