EP3283732A2 - Dispositif de réglage d'aubes directrices et turbomachine - Google Patents

Dispositif de réglage d'aubes directrices et turbomachine

Info

Publication number
EP3283732A2
EP3283732A2 EP16716553.9A EP16716553A EP3283732A2 EP 3283732 A2 EP3283732 A2 EP 3283732A2 EP 16716553 A EP16716553 A EP 16716553A EP 3283732 A2 EP3283732 A2 EP 3283732A2
Authority
EP
European Patent Office
Prior art keywords
vane
control ring
transmission lever
ring
drive shaft
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.)
Granted
Application number
EP16716553.9A
Other languages
German (de)
English (en)
Other versions
EP3283732B1 (fr
Inventor
Lennart Leopold
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.)
Everllence SE
Original Assignee
MAN Diesel and Turbo SE
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 MAN Diesel and Turbo SE filed Critical MAN Diesel and Turbo SE
Publication of EP3283732A2 publication Critical patent/EP3283732A2/fr
Application granted granted Critical
Publication of EP3283732B1 publication Critical patent/EP3283732B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • 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
    • 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
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
    • F03B3/16—Stators
    • F03B3/18—Stator blades; Guide conduits or vanes, e.g. adjustable
    • F03B3/183—Adjustable vanes, e.g. wicket gates
    • 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
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
    • 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
    • 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
    • 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
    • F04D29/566—Fluid-guiding means, e.g. diffusers adjustable specially adapted for liquid pumps
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/24—Three-dimensional ellipsoidal
    • F05D2250/241—Three-dimensional ellipsoidal spherical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position

Definitions

  • the invention relates to a Leitschaufelverstellvortechnische for a turbomachine and a turbomachine with such Leitschaufelverstellvorrich- device.
  • Turbomachines known from practice have a rotor and a stator.
  • the rotor of a turbomachine comprises a shaft and a plurality of rotating together with the rotor blades, wherein the blades form at least one blade ring.
  • the stator of a turbomachine comprises a housing and a plurality of stationary vanes, wherein the vanes form at least one vane ring.
  • Leitschaufelverstellvoriquesen known from practice in this case have a drive shaft to which a drive motor can be coupled and which is drivable via the drive motor.
  • the rotation of the drive shaft via the drive motor with the aid of a control ring on all vanes of a vane ring is transferred, so therefore all the vanes of a vane ring indirectly adjusted or rotated with the interposition of the control ring, starting from the drive shaft.
  • the control ring of guide vane adjusting devices known from practice can be rotated in the circumferential direction, but can not be displaced in the axial direction and in the radial direction.
  • Leitschaufelverstellvorettien From the practice known Leitschaufelverstellvoroplastyen have the disadvantage that incurred relatively much friction on the same. Furthermore, they are designed for a high torsional load. Therefore, known from practice Leitschaufelverstellvorierien must be sized accordingly large. However, this is disadvantageous in view of the limited installation space available on turbomachines.
  • the object of the invention is to provide a novel guide vane adjusting device for a turbomachine and a turbomachine with such a vane adjusting device.
  • the drive shaft is directly coupled to one of the vanes of the vane ring, such that this vane ring of the vane ring is directly rotatable, starting from the drive shaft without the interposition of the control ring.
  • the drive shaft or the vane directly driven by the drive shaft is pivotally coupled to the control ring via a transmission lever.
  • the drive shaft is indirectly coupled to the other vanes of the vane ring such that the other vanes of the vane ring are rotatable indirectly from the drive shaft with the interposition of the control ring.
  • the indirectly drivable by the drive shaft vanes are pivotally coupled to the control ring via other transmission lever.
  • Control ring is displaceable in the circumferential direction and in the axial direction, so that forces at coupling points between the control ring and the coupling arms articulated to the control ring perpendicular to the transmission levers.
  • the guide vanes of the vane ring that are indirectly rotatable or indirectly coupled to the drive shaft are articulated to the control ring via a transmission lever.
  • the control ring is displaceable in the circumferential direction and in the axial direction and guided only displaceable in the radial direction. In this way, it can ultimately be ensured that forces at the coupling points between the control ring and the transmission levers pivotally coupled to the control ring are always perpendicular to the transmission levers so that bearings of the guide vanes are not loaded by parasitic force components.
  • a Leitschaufelverstellvor- direction can be dimensioned smaller so that the same has a smaller space requirement.
  • the drive shaft or directly driven by the drive shaft guide vane is pivotally coupled to the control ring via a multi-part transmission lever, wherein a first segment of the multi-part transmission lever is rigidly coupled to the drive shaft or with the directly driven by the drive shaft vane, and wherein a second segment of the multi-piece transmission lever is pivotally coupled to the control ring.
  • the first segment of the multi-part transmission lever is pivotally coupled to the second segment of the multi-part transmission lever to form a two-part transmission lever. This allows a particularly advantageous coupling of the drive shaft or the directly from the drive shaft driven vane with the control ring.
  • the indirectly drivable by the drive shaft guide vanes with the control ring via one-piece, elastically deformable transmission lever are articulated coupled.
  • the indirectly driven by the drive shaft vanes with the control ring articulated via multi-part transmission lever wherein a first segment of each of these multi-part transmission lever is rigidly coupled to the respective vane, and wherein a second segment of each of these multi-part transmission lever articulated is coupled to the control ring.
  • the first segment of the respective multi-part transmission lever is then preferably articulated to the second segment of the respective multi-part transmission lever to form a two-part transmission lever.
  • the two variants allow an advantageous coupling of the indirectly rotatable vanes with the control ring.
  • the first variant with the one-piece transmission levers between the control ring and indirectly driven by the drive shaft guide vanes is structurally simpler than the second variant with the multi-part transmission levers.
  • the second variant with the multi-part transmission levers builds more compact.
  • the turbomachine is defined in claim 10.
  • Fig. 1 shows a perspective section of a turbomachine in
  • Fig. 2 is a plan view of the arrangement of Figure 1 in a first state.
  • Fig. 3 is a fragmentary side view of Fig. 2;
  • Fig. 4 is a plan view of the arrangement of Figure 1 in a second state.
  • Fig. 5 is a fragmentary side view of Fig. 4;
  • FIG. 6 shows a partial cross section through an alternative Leitschaufelverstell- device.
  • FIG. 7 shows a partial cross-section, offset by 90 ° with respect to FIG. 1, through the vane adjusting device of FIG. 6;
  • FIG. 7 shows a partial cross-section, offset by 90 ° with respect to FIG. 1, through the vane adjusting device of FIG. 6;
  • FIG. 8 shows the arrangement of FIG. 7 without housing in a perspective view
  • Fig. 9 is a detail of Fig. 8.
  • Fig. 10 is a detail of the vane adjusting devices; Fig. 1 1 an alternative to the detail of Fig. 10;
  • Fig. 12 shows an alternative to the arrangement of Fig. 8;
  • Fig. 13 is a detail of Fig. 12;
  • FIG. 14 shows an alternative to the detail of FIG. 13.
  • the present invention relates to a Leitschaufelverstellvortechnische for a turbomachine and a turbomachine with at least one such Leitschaufelverstellvortechnisch.
  • a turbomachine comprises a rotor with rotor-side rotor blades and a stator with stator-side stator blades.
  • the blades of the rotor form at least one blade ring, wherein the or each blade ring rotates together with a shaft of the rotor.
  • the vanes of the stator form at least one vane ring which is connected to a stator-side housing.
  • 1 shows a section of a turbomachine in the region of a guide vane ring 20 comprising a plurality of stator blades 21.
  • Each of the guide vanes 21 has a blade root or blade journal 22 and an airfoil blade 23, wherein the blade journal 22 of the respective stator blade 21 is positioned radially outward and acts on a housing structure 24 of the turbomachine.
  • the present invention now relates to a vane adjusting device for the guide vanes 21 of such a vane ring 20, by means of which the guide vanes 21 can be rotated about extending in the radial direction of the rotor, not shown, the stator blades 25 of the guide vanes 20.
  • the blade roots 22 of the vanes 21 are thus rotatably mounted in the housing structure 24, namely such that each of the vanes 21 can be rotated about the respective radially extending vane axis 25.
  • the vane adjusting device for rotating the guide vanes 21 of the vane ring 20 about their radially extending Leitschaufel- axes 25 includes a drive shaft 26 which is coupled to a drive motor, not shown, and which is driven by the drive motor.
  • the drive shaft 26 is directly coupled to one of the vanes 21 of the vane ring 20, namely such that this vane 21 of the Leitschaufelkran- zes 20, starting from the drive shaft 26 is directly rotatable.
  • the drive shaft 26 preferably runs coaxially with the blade journal 22 of this directly rotatable guide blade 21 or coaxially with the blade axis 25 of this directly rotatable guide blade 21.
  • the vane adjusting device further comprises a control ring 27.
  • the drive shaft 26 or the directly from the drive shaft 26 driven vane 21 is pivotally coupled to the control ring 27 via a transmission lever 28.
  • the drive shaft 26 is indirectly coupled to the other vanes 21 of the vane ring 20 via the control ring 27, so that the remaining vanes 21 of the vane ring 20 of the drive shaft 26 are indirectly rotatable, namely with the interposition of the control ring 27, the rotation of the drive shaft 26 on the remaining vanes 21 of the vane ring 20 transmits.
  • This indirectly by the drive shaft 26 driven or rotatable vanes 21 of the vane ring 20 are coupled to the control ring 27 via other transmission lever 29 articulated.
  • the control ring 27, on which on the one hand the directly adjustable from the drive shaft 26 from the guide vane 21 via the transmission lever 28 and on the other hand indirectly from the drive shaft 26 rotatable vanes 21 are connected via the transmission lever 29, in the circumferential direction U and in the axial direction A can be displaced.
  • This displaceability of the control ring 27 in the circumferential direction U and in the axial direction A and by the articulated connection of the transmission levers 28 and 29 to the control ring 27 extend forces during rotation of the vanes 21 at the coupling points between the control ring 27 and the articulated to the control ring 27 coupled transmission levers 28, 29 attack, always perpendicular to the transmission levers 27, 28th
  • This multi-part transmission lever 28 has at least one first segment 31 which is rigidly coupled to the drive shaft 26 or to the guide vane 21 which can be driven directly by the drive shaft 26, and a second segment 32 which is pivotally coupled to the control ring 27.
  • two spherical spherical plain bearings 33 are formed between the first segment 31 of the two-part transmission lever 28 and the second segment 32 thereof. Further, between the second segment 32 of this transmission lever 28 and the control ring 27, a further spherical spherical plain bearing 34 is formed.
  • the indirectly driven by the drive shaft 26 of the guide vanes 21 are coupled to the control ring 27 via the transmission lever 29, which in the embodiments of FIGS. 1 to 9 also as a multi-part transmission lever 29th are executed.
  • Each of these transmission levers 29 has a first segment 35 which is rigidly coupled to the respective vane 21, and a second segment 36 which is pivotally coupled to the control ring 27, wherein in the embodiments of Figs. 1 to 9, this transmission - Lever 29 as well as the transmission lever 28 are formed as a two-part transmission lever 29.
  • the first segment 35 of the respective transmission lever 29 is then articulated to the second segment 36, wherein according to the illustrated embodiments of FIGS.
  • FIGS. 10 and 11 show such a control ring 27 in a sole view, wherein an inner running surface 39 of the control ring 27 of FIG. 10 is preferably coated with anti-friction varnish or a PTFE fabric in order to reduce the friction thereon.
  • Fig. 1 1 shows an alternative embodiment of the control ring 27, which in contrast to FIG. 10 is not formed in one piece, but rather in several parts and comprises a plurality of so-called sliding pads 40 which detachable with a main body 41 of the control ring 27 of FIG are connected.
  • the sliding pads 40 prevent tilting of the control ring 27 in the movement of the same in the axial direction and circumferential direction and allow a backlash-free mounting of the control ring 27 on the housing structure 24.
  • the sliding pads 40 are interchangeable and preferably made of a material with good sliding properties and thus low coefficients of friction.
  • the sliding pads 40 are hingedly connected to the base body 41 via sliding pad holders 40a, such that they are each mounted rotatably about an axis which are tangent to the circumference and perpendicular to the axis of rotation of the control ring 27.
  • the transmission levers 29, which serve to couple the guide vanes 21 indirectly driven by the drive shaft 26 to the control ring 27, are designed as one-piece, elastically deformable transmission levers 29.
  • the one-piece, elastically deformable transmission lever 29 at one end fixed to the respective vane 21 and at an opposite end via a spherical pivot bearing 42 with the
  • Control ring 27 coupled.
  • the same bending elastic is deformable to compensate for a changing in the circumferential displacement and axial displacement of the control ring 27 between the control ring 27 and the indirectly displaceable vanes 21 height offset or radial offset.
  • FIG. 14 differs from the embodiment of FIGS. 12 and 13 by the specific embodiment of the transmission lever 28 and 29th
  • a guide blade 21 of the guide blade ring 20 can be driven directly by a drive shaft 26.
  • the drive shaft 26 or the directly driven vane 21 is coupled to a control ring 27.
  • This coupling is preferably carried out via a two-part pivot lever 28 with preferably three spherical plain bearings.
  • All other vanes 21 of the vane ring 20 are indirectly driven by the drive shaft 26 via the control ring 27, said vanes 21 are coupled via further transmission lever 29 to the control ring 27.
  • the control ring 27 is mounted radially coaxial with the axis of rotation of a rotor, not shown, and can perform an axial linear movement and a rotational movement superimposed in the circumferential direction.
  • the transmission levers 29, which serve to couple the indirectly adjustable guide vanes to the control ring 27, can, like the transmission lever 28, which serves to connect the directly adjustable guide vane 21 to the control ring 27, be made in several parts or alternatively in one piece.
  • hinge joints can also be used.
  • the transmission levers 28, 29 engage outside the housing structure 24 at the radially outer ends of the blade roots.
  • the transmission levers 28, 29 engage between the bearing stems 30 of the transmission levers 28, 29.
  • the vane adjuster of the present invention provides efficient kinematics for relocating the guide scooping a vane ring at low component loads, which high suction pressures can be used in a turbomachine, which uses the Leitschaufelverstellvorraum.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'invention concerne un dispositif de réglage d'aubes directrices pour une turbomachine, permettant notamment la rotation de plusieurs aubes directrices, groupées pour former une couronne directrice, autour d'un axe d'aube directrice s'étendant dans la direction radiale d'un rotor de la turbomachine, lequel dispositif comprend un arbre d'entraînement (26), auquel un moteur d'entraînement peut être accouplé et qui peut être entraîné par ledit moteur d'entraînement, et une bague de commande (27) qui transmet une rotation de l'arbre d'entraînement (26) pour permettre la rotation d'aubes directrices (21) de la couronne directrice (20) sur celui-ci. L'arbre d'entraînement (38) est accouplé directement à une des aubes directrices (21) de la couronne directrice (20), de sorte que cette aube directrice de la couronne directrice peut tourner en étant sollicitée directement par l'arbre d'entraînement (38) sans insertion de la bague de commande (27). L'arbre d'entraînement (26) ou l'aube directrice (21) pouvant être entraînée directement par l'arbre d'entraînement (26) est accouplé(e) à la bague de commande (27) de manière articulée par l'intermédiaire d'un levier de transmission (28). L'arbre d'entraînement (26) est accouplé indirectement aux autres aubes directrices (21) de la couronne directrice (20), de sorte que les autres aubes directrices de la couronne directrice peuvent tourner en étant sollicitées indirectement par l'arbre d'entraînement (26) avec insertion de la bague de commande (27). Les aubes directrices (21) pouvant être entraînées indirectement par l'arbre d'entraînement (26) sont accouplées à la bague de commande (27) de manière articulée par l'intermédiaire de leviers de transmission (29) supplémentaires; et la bague de commande (27) peut se déplacer dans la direction périphérique et dans la direction axiale, de sorte que des forces s'appliquent aux points d'accouplement entre la bague de commande (27) et les leviers de transmission (28, 29) accouplés à la bague de commande (27) de manière articulée, perpendiculairement aux leviers de transmission (28, 29).
EP16716553.9A 2015-04-15 2016-04-14 Dispositif de réglage d'aubes directrices et turbomachine Active EP3283732B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102015004648.9A DE102015004648A1 (de) 2015-04-15 2015-04-15 Leitschaufelverstellvorrichtung und Strömungsmaschine
PCT/EP2016/058181 WO2016166191A2 (fr) 2015-04-15 2016-04-14 Dispositif de réglage d'aubes directrices et turbomachine

Publications (2)

Publication Number Publication Date
EP3283732A2 true EP3283732A2 (fr) 2018-02-21
EP3283732B1 EP3283732B1 (fr) 2020-07-29

Family

ID=57043699

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16716553.9A Active EP3283732B1 (fr) 2015-04-15 2016-04-14 Dispositif de réglage d'aubes directrices et turbomachine

Country Status (8)

Country Link
US (1) US10774673B2 (fr)
EP (1) EP3283732B1 (fr)
JP (1) JP6683730B2 (fr)
KR (1) KR20170136632A (fr)
CN (1) CN107429572B (fr)
DE (1) DE102015004648A1 (fr)
RU (1) RU2675948C1 (fr)
WO (1) WO2016166191A2 (fr)

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US10774673B2 (en) 2020-09-15
EP3283732B1 (fr) 2020-07-29
WO2016166191A3 (fr) 2017-01-26
CN107429572B (zh) 2020-03-06
WO2016166191A4 (fr) 2017-03-16
JP6683730B2 (ja) 2020-04-22
US20180100407A1 (en) 2018-04-12
RU2675948C1 (ru) 2018-12-25
DE102015004648A1 (de) 2016-10-20
JP2018511735A (ja) 2018-04-26
WO2016166191A2 (fr) 2016-10-20
KR20170136632A (ko) 2017-12-11
CN107429572A (zh) 2017-12-01

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