EP0780544B1 - Palier d'extrémité interne d'aube pivotante - Google Patents
Palier d'extrémité interne d'aube pivotante Download PDFInfo
- Publication number
- EP0780544B1 EP0780544B1 EP96402807A EP96402807A EP0780544B1 EP 0780544 B1 EP0780544 B1 EP 0780544B1 EP 96402807 A EP96402807 A EP 96402807A EP 96402807 A EP96402807 A EP 96402807A EP 0780544 B1 EP0780544 B1 EP 0780544B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- ring
- socket
- bearing
- axis
- journal
- 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 - Lifetime
Links
- 239000007789 gas Substances 0.000 description 2
- 239000003831 antifriction material Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000011796 hollow space material Substances 0.000 description 1
- 210000004417 patella Anatomy 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
Images
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
Definitions
- the subject of the invention is a level inner end of pivoting vane.
- Modern turbomachines include often stator blades with variable setting, that is to say the orientation of which can be changed by a pivoting movement to modify the recovery of the gases they cause and optimize machine performance at different speeds of it.
- the blades 1 with variable setting are arranged in stages circulars which also alternate with floors circular vanes 2 fixed to the rotor 3; the vanes 1 have an outer end pivot 4, engaged in a bearing 5 of the stator and protruding at the outside to finish in a head 7 grabbed by a control lever 8, and control levers 8 of blades 1 of the same stage are articulated to their other end to a control ring 9 which surrounds the stator: the rotation of the control ring 9 around of its axis therefore produces the tilting of the levers 8 and the pivoting of the blades 1.
- the internal end of the blades 1 comprises a internal pivot 10 engaged in an internal bearing 11, in cylindrical socket shape in this design classic and housed in a common link ring 12 to all the vanes 1 on the same stage and whose role is to strengthen the mounting of the blades 1 while helping to define the gas flow stream 13 with platforms 14 movable vanes 2 and wear a labyrinth seal 15 with the rotor 3.
- the internal bearings 11 are the most often a substantially cylinder-shaped socket hollow and antifriction material, which therefore allows internal pivots 10 to turn easily.
- the internal bearings 11 must be replaced frequently, as a result of efforts aerodynamics exerted on the blades 1, which drive their deformation and the displacement of the ring of link 12: the internal pivots 10 are then oriented obliquely in the internal bearings 11 and wear them out by expanding them.
- the internal bearings 11 are mounted with a clamp in the connecting ring 12 and with a just sliding fit around the pivot internal 10. Wear therefore almost immediately a significant change in the adjustment.
- the invention is based on the idea that wear and tear of the bearing part can be prevented without it should give him the freedom of movement of a patella.
- the rectifier composed of vanes 1 and link ring 12 had low overall inertia rotating around the axis X of the machine and of the connecting ring 12, while its inertia in translation along this axis was much stronger, which explains why the movements of the internal pivots 10 and the wear they cause on the bearing parts are much more important in transverse direction than in direction longitudinal.
- the level of the invention therefore has as characteristic that it can rotate in the ring of link only when the pivot he wears inflate a transverse rotation, around an axis parallel to the X axis of the machine.
- the invention relates to an end bearing internal pivoting blade, engaged in a ring of connection of pivoting vanes on the same stage and comprising a socket surrounding the pivot, characterized in that it includes a revolving pin in a drilling of the axis ring parallel to the axis of the ring, and in that the sleeve, integral with the pin, is free to play in the ring.
- the bearing part 18, that is to say that which connects each of the internal pivots 10 to the ring of link 12, is composed of a socket 19, cylindrical like known socket 11, and two portions of pin 20 in extension and located on each side of the socket 19, which forms a single piece with them.
- the journal portions 20 therefore have an axis of common rotation X 'parallel to the machine axis X and of the connecting ring 12. As in Figures 2 and 3 the show, the journal portions 20 are engaged in bore portions 21 of the connecting ring 12 so that it can rotate freely around this axis X '.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Support Of The Bearing (AREA)
Description
- la figure déjà décrite illustre le lieu d'utilisation de l'invention dans une turbomachine et une conception de l'art antérieur ;
- la figure 2 illustre un palier complet selon l'invention,
- la figure 3 représente les paliers vus en direction longitudinale,
- et la figure 4 représente la pièce de palier en perspective.
Claims (3)
- Palier (18) d'extrémité interne (10) d'aube pivotante (1), engagé dans un anneau de liaison (12) d'aubes pivotantes (1) d'un même étage et comprenant une douille (19) entourant le pivot (10), caractérisé en ce qu'il comprend un tourillon (20) tournant dans un perçage (21) de l'anneau (12) d'axe (X') parallèle à l'axe de l'anneau (X), et en ce que la douille (19), solidaire du tourillon (20), est libre de jouer dans l'anneau (12).
- Palier selon la revendication 1, caractérisé en ce que le tourillon (20) est composé de deux parties entre lesquelles se trouve la douille (19).
- Palier selon l'une quelconque des revendications 1 ou 2, caractérisé en ce que la douille (19) est engagée entre des faces (22) de l'anneau (21) qui forment des butées de limitation de jeu.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR9515120 | 1995-12-20 | ||
| FR9515120A FR2742799B1 (fr) | 1995-12-20 | 1995-12-20 | Palier d'extremite interne d'aube pivotante |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0780544A1 EP0780544A1 (fr) | 1997-06-25 |
| EP0780544B1 true EP0780544B1 (fr) | 1999-03-10 |
Family
ID=9485705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP96402807A Expired - Lifetime EP0780544B1 (fr) | 1995-12-20 | 1996-12-19 | Palier d'extrémité interne d'aube pivotante |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5796199A (fr) |
| EP (1) | EP0780544B1 (fr) |
| DE (1) | DE69601695T2 (fr) |
| FR (1) | FR2742799B1 (fr) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2775731B1 (fr) * | 1998-03-05 | 2000-04-07 | Snecma | Etage circulaire d'aubes aux extremites interieures unies par un anneau de liaison |
| FR2874977A1 (fr) * | 2004-09-07 | 2006-03-10 | Snecma Moteurs Sa | Douille de support pivotant pour pivot d'aube a calage variable de turbomachine |
| US7360990B2 (en) * | 2004-10-13 | 2008-04-22 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| US7278819B2 (en) * | 2005-07-05 | 2007-10-09 | General Electric Company | Variable stator vane lever arm assembly and method of assembling same |
| FR2889242B1 (fr) * | 2005-07-27 | 2007-11-02 | Snecma | Douille pour pivot d'aube a angle de calage variable pour turbomachine |
| US9353643B2 (en) * | 2007-04-10 | 2016-05-31 | United Technologies Corporation | Variable stator vane assembly for a turbine engine |
| US7854586B2 (en) * | 2007-05-31 | 2010-12-21 | United Technologies Corporation | Inlet guide vane inner air seal surge retaining mechanism |
| FR2920469A1 (fr) * | 2007-08-30 | 2009-03-06 | Snecma Sa | Aube a calage variable de turbomachine |
| DE102008021683A1 (de) * | 2008-04-30 | 2009-11-05 | Rolls-Royce Deutschland Ltd & Co Kg | Rotierende Einheit für einen Axialkompressor |
| EP2295732A1 (fr) * | 2009-09-14 | 2011-03-16 | Alstom Technology Ltd | Turbine axiale et procédé de décharge d'un écoulement d'une turbine axiale |
| DE102011077626A1 (de) * | 2011-06-16 | 2012-12-20 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Wastegate-Ventilvorrichtung |
| US9932988B2 (en) * | 2013-02-15 | 2018-04-03 | United Technologies Corporation | Bushing arranged between a body and a shaft, and connected to the shaft |
| EP2952693B1 (fr) | 2014-06-06 | 2021-04-28 | Raytheon Technologies Corporation | Carter avec fonctionnalité de rétention d'aube |
| EP3009604B1 (fr) * | 2014-09-19 | 2018-08-08 | United Technologies Corporation | Système d'aubes fixes-variables fixées radialement |
| RU2612666C1 (ru) * | 2015-12-09 | 2017-03-13 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" | Регулируемый направляющий аппарат осевого компрессора турбомашины |
| DE102016207212A1 (de) * | 2016-04-28 | 2017-11-02 | MTU Aero Engines AG | Leitschaufelkranz für eine Strömungsmaschine |
| DE102016215807A1 (de) * | 2016-08-23 | 2018-03-01 | MTU Aero Engines AG | Innenring für einen Leitschaufelkranz einer Strömungsmaschine |
| DE102017109952A1 (de) * | 2017-05-09 | 2018-11-15 | Rolls-Royce Deutschland Ltd & Co Kg | Rotorvorrichtung einer Strömungsmaschine |
| DE102018210601A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Segmentring zur montage in einer strömungsmaschine |
| US10808568B2 (en) * | 2018-09-12 | 2020-10-20 | Raytheon Technologies Corporation | Airfoil assembly for a gas turbine engine |
| US11816936B2 (en) | 2018-12-03 | 2023-11-14 | Bendix Commercial Vehicle Systems, Llc | System and method for detecting driver tampering of vehicle information systems |
| FR3123885B1 (fr) * | 2021-06-15 | 2023-06-16 | Safran Aircraft Engines | Redresseur non carene de turbomachine equipe d’aubes de stator fixees a des pivots et turbomachine correspondante |
| FR3132123B1 (fr) * | 2022-01-21 | 2023-12-08 | Safran Aircraft Engines | Aube de redresseur de flux secondaire de turbomachine, turbomachine munie de celle-ci |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4363600A (en) * | 1981-04-06 | 1982-12-14 | General Motors Corporation | Variable vane mounting |
| FR2524934B1 (fr) * | 1982-04-08 | 1986-12-26 | Snecma | Dispositif de butee de securite pour pivot d'aubes de stator a calage variable |
| FR2556410B1 (fr) * | 1983-12-07 | 1986-09-12 | Snecma | Dispositif de centrage de l'anneau interieur d'un stator a ailettes a calage variable |
| FR2599785B1 (fr) * | 1986-06-04 | 1990-10-12 | Snecma | Aubage directeur d'entree d'air a calage variable pour turboreacteur |
| GB2210935B (en) * | 1987-10-10 | 1992-05-27 | Rolls Royce Plc | Variable stator vane assembly |
| US4990056A (en) * | 1989-11-16 | 1991-02-05 | General Motors Corporation | Stator vane stage in axial flow compressor |
| CA2082709A1 (fr) * | 1991-12-02 | 1993-06-03 | Srinivasan Venkatasubbu | Aubage de stator a incidence variable pour compresseur a ecoulement axial de turbomachine |
| FR2691507B1 (fr) * | 1992-05-20 | 1994-07-08 | Snecma | Structure d'etancheite pour une aube pivotante de turbomachine. |
| FR2696208B1 (fr) * | 1992-09-30 | 1994-11-10 | Snecma | Aube à calage variable. |
| DE4237031C1 (de) * | 1992-11-03 | 1994-02-10 | Mtu Muenchen Gmbh | Verstellbare Leitschaufel |
| FR2699595B1 (fr) * | 1992-12-23 | 1995-01-20 | Snecma | Dispositif de guidage en rotation d'un anneau de commande d'aubes pivotantes. |
| US5517817A (en) * | 1993-10-28 | 1996-05-21 | General Electric Company | Variable area turbine nozzle for turbine engines |
| US5593275A (en) * | 1995-08-01 | 1997-01-14 | General Electric Company | Variable stator vane mounting and vane actuation system for an axial flow compressor of a gas turbine engine |
-
1995
- 1995-12-20 FR FR9515120A patent/FR2742799B1/fr not_active Expired - Fee Related
-
1996
- 1996-12-04 US US08/759,927 patent/US5796199A/en not_active Expired - Lifetime
- 1996-12-19 DE DE69601695T patent/DE69601695T2/de not_active Expired - Lifetime
- 1996-12-19 EP EP96402807A patent/EP0780544B1/fr not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| DE69601695T2 (de) | 2000-06-29 |
| US5796199A (en) | 1998-08-18 |
| FR2742799A1 (fr) | 1997-06-27 |
| DE69601695D1 (de) | 1999-04-15 |
| EP0780544A1 (fr) | 1997-06-25 |
| FR2742799B1 (fr) | 1998-01-16 |
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