EP1439283A1 - Agencement de montage d'aubes a calage variable - Google Patents
Agencement de montage d'aubes a calage variable Download PDFInfo
- Publication number
- EP1439283A1 EP1439283A1 EP04100115A EP04100115A EP1439283A1 EP 1439283 A1 EP1439283 A1 EP 1439283A1 EP 04100115 A EP04100115 A EP 04100115A EP 04100115 A EP04100115 A EP 04100115A EP 1439283 A1 EP1439283 A1 EP 1439283A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pivots
- levers
- mounting arrangement
- casing
- removable
- 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.)
- Withdrawn
Links
- 230000000717 retained effect Effects 0.000 claims description 2
- 230000000295 complement effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification 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
-
- 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
Definitions
- the subject of this invention is a arrangement for mounting variable-pitch vanes.
- Variable pitch vanes are called blades attached to the stator of a turbomachine and which have the ability to rotate to modify characteristics that they impose on the flow of gas and thus adjust the machine to its different regimes.
- blades include, at their end external, pivots passing through the casing while being there retained by bearings allowing rotation, and the arrangement still includes levers engaged on portions outside the pivot housing.
- levers are joined to a ring of common control going around the casing and whose rotation rotates the levers, pivots and vanes themselves.
- the portions of the pivots have a square section and the lever heads have a square housing.
- the commitment of the square section in the square housing of the lever allows to rotate the pivots and these blades in rotation.
- a nut is screwed onto a threaded end of the pivots to hold the heads of the levers in place securely circumstance.
- the pivots can tilt in the crankcase passages, possibly causing damage as a result of friction of elements of the mobile assembly on the housing or on the rotor. And even when the bearings are in better condition, gas leaks sometimes important are noted. This is why we have sought an improved arrangement in which these disadvantages would be reduced.
- the characteristic essential of the new assembly is that it is possible adjust the clearance between the housing and the heads levers and, by reducing this play, lessen the gas leaks and better oppose tipping pivots thanks to the additional support provided by the head of the lever.
- blade pivots are divided into two connected parts by means of axial position adjustment allowing to vary their length; one of the parties, who is removable, pivots and which carries the end threaded in which the retaining nut is engaged, has a stop for the lever; and the levers are tightened between the stops and the nuts. So the modification of the adjustment between the two parts of the pivot is equivalent to a change in distance between the casing and the removable portion of the pivots, and therefore between the housing and the lever.
- a convenient means of connection between the two end parts of the pivots is a thread.
- FIG. 1 The outer portion of a blade 1 appears in Figure 1, as well as its pivot 2 extending to through a passage 3 of a casing 4 out of it.
- a pair of bearings 5 and 6 supports pivot 2 at ends of passage 3, and bearings 5 and 6 include, in addition to an annular socket 7 assigned to the centering of pivot 2 in passage 3, a portion flat 8 arranged around the ends of passage 3 and limiting the travel of the assembly without allow direct contact between dawn 1 and the internal end of the passage 3 or between the casing 4 and a head 9 of a control lever 10.
- This lever 10 extends out of the casing 4 and its head 9 comprises a housing 11 in which is engaged the end of the pivot.
- the housing 11 includes a square section 12, or more generally polygonal, over part of its height, and pivot 2 has a section complementary to this place, which allows it to rotate by tilting lever 10. This is achieved by a ring 13 not shown in detail but which is concentric to the stator 4.
- the lever 10 carries a pin 14 at its end opposite to the head 9 and which penetrates in the ring 13. By turning the latter, the pin 14 is moved and the lever 10 turns.
- the square section 12 extends only at the bottom of the housing 11, and above all the end of pivot 2 is divided into two portions one of which 15 is integral with the main portion of the pivot 2 (the one located in passage 3) but has a smaller radius, while the other portion 16 is removable and covers the previous one, to which it is connected in an adjustable manner by thread 17.
- the removable portion 16 carries the threaded end 18 usual blade pivots and retaining nut 19 engaged around this end.
- the portion removable 16 includes a stop 20 in the form of outer flange at its lower end, and the housing 11 has a stepped shape 21 abutting against the flange 20.
- the screwing of the nut 19 makes it possible to tighten the head 9 between him and the stop 20 and therefore maintain the head 9 at a determined height and invariable on the removable portion 16.
- the removable portion 16 has been adjusted, thanks to thread 17, at a height relative to the other portion 15 chosen so that the clearance between the bottom of the head 9 and the part plate 8 of the outer bearing 5 is very reduced. So, an involuntary tilting of pivot 2 when the bearings 5 and 6 are worn immediately produces a contact between the head 9 and the portion 8, limiting this failover.
- the square section 12 extends under the removable portion 16 and the stop 20.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Bolts, Nuts, And Washers (AREA)
- Clamps And Clips (AREA)
- Hinges (AREA)
Abstract
Description
Claims (3)
- Agencement de montage d'aubes (1) à calage variable, comprenant des pivots (2) des aubes traversant un carter (4), des leviers (10) de commande engagés sur des portions extérieures au carter des pivots, et des écrous (19) vissés sur des extrémités filetées (18) des portions extérieures, des têtes (11) des leviers (10) étant retenues entre les écrous et le carter, caractérisé en ce que les portions extérieures sont divisées en deux parties (15, 16) reliées par un moyen d'ajustement de position (17) permettant de faire varier la longueur des portions extérieures, une desdites parties (16), qui est amovible des pivots, porte l'extrémité filetée, et comporte une butée (20) du levier, les leviers (10) étant serrés entre les butées et les écrous.
- Agencement de montage d'aubes à calage variable selon la revendication 1, caractérisé en ce que le moyen d'ajustement de position consiste en un filetage.
- Agencement de montage d'aubes à calage variable selon l'une quelconque des revendications 1 ou 2, caractérisé en ce que les leviers comprennent des encoches (22) d'introduction des parties amovibles (16) dans une direction latérale à des logements (11) des leviers par lesquels ceux-ci sont engagés sur les portions extérieures des pivots, les encoches comprenant des régions élargies (23) recevant les butées (20).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0300476A FR2850131B1 (fr) | 2003-01-17 | 2003-01-17 | Agencement de montage d'aubes a calage variable |
| FR0300476 | 2003-01-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1439283A1 true EP1439283A1 (fr) | 2004-07-21 |
Family
ID=32524964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP04100115A Withdrawn EP1439283A1 (fr) | 2003-01-17 | 2004-01-15 | Agencement de montage d'aubes a calage variable |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20040146398A1 (fr) |
| EP (1) | EP1439283A1 (fr) |
| JP (1) | JP2004225693A (fr) |
| CA (1) | CA2455016A1 (fr) |
| FR (1) | FR2850131B1 (fr) |
| RU (1) | RU2004101422A (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP4130441A1 (fr) * | 2021-08-05 | 2023-02-08 | MTU Aero Engines AG | Dispositif de liaison d'une aube à calage variable d'une turbine à gaz et turbine à gaz |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8414248B2 (en) | 2008-12-30 | 2013-04-09 | Rolls-Royce Corporation | Variable geometry vane |
| US10030533B2 (en) * | 2012-09-21 | 2018-07-24 | United Technologies Corporation | Flanged bushing for variable vane |
| US10208618B2 (en) * | 2013-02-04 | 2019-02-19 | United Technologies Corporation | Vane arm having a claw |
| DE102013211629A1 (de) * | 2013-06-20 | 2015-01-08 | MTU Aero Engines AG | Leitschaufelanordnung und Verfahren zum Montieren einer Leitschaufel |
| DE102016224523A1 (de) * | 2016-12-08 | 2018-06-14 | MTU Aero Engines AG | Leitschaufelverstellung mit seitlich montiertem Verstellhebel |
| GB201711582D0 (en) * | 2017-07-19 | 2017-08-30 | Rolls Royce Plc | Unison ring assembly |
| CN120007380A (zh) * | 2023-11-15 | 2025-05-16 | 中国航发商用航空发动机有限责任公司 | 用于调节发动机叶片角度的摇臂组件以及发动机叶片组件 |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2113194A1 (de) * | 1971-03-18 | 1972-09-28 | Daimler Benz Ag | Lagerung von Verstellschaufeln |
| US3990810A (en) * | 1975-12-23 | 1976-11-09 | Westinghouse Electric Corporation | Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine |
| US4139329A (en) * | 1977-05-16 | 1979-02-13 | Westinghouse Canada Limited | Vane tip motion transfer device |
| US4307994A (en) * | 1979-10-15 | 1981-12-29 | General Motors Corporation | Variable vane position adjuster |
| FR2583820A1 (fr) * | 1985-06-20 | 1986-12-26 | Snecma | Dispositif de variation de section de passage d'un distributeur de turbine |
| EP0545656A1 (fr) * | 1991-12-02 | 1993-06-09 | General Electric Company | Montage d'aubage statorique à calage variable pour compresseur axial de turbine à gaz |
| FR2699595A1 (fr) * | 1992-12-23 | 1994-06-24 | Snecma | Dispositif de guidage en rotation d'un anneau de commande d'aubes pivotantes. |
-
2003
- 2003-01-17 FR FR0300476A patent/FR2850131B1/fr not_active Expired - Fee Related
-
2004
- 2004-01-12 CA CA002455016A patent/CA2455016A1/fr not_active Abandoned
- 2004-01-14 JP JP2004006209A patent/JP2004225693A/ja active Pending
- 2004-01-14 US US10/756,780 patent/US20040146398A1/en not_active Abandoned
- 2004-01-15 EP EP04100115A patent/EP1439283A1/fr not_active Withdrawn
- 2004-01-16 RU RU2004101422/06A patent/RU2004101422A/ru not_active Application Discontinuation
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2113194A1 (de) * | 1971-03-18 | 1972-09-28 | Daimler Benz Ag | Lagerung von Verstellschaufeln |
| US3990810A (en) * | 1975-12-23 | 1976-11-09 | Westinghouse Electric Corporation | Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine |
| US4139329A (en) * | 1977-05-16 | 1979-02-13 | Westinghouse Canada Limited | Vane tip motion transfer device |
| US4307994A (en) * | 1979-10-15 | 1981-12-29 | General Motors Corporation | Variable vane position adjuster |
| FR2583820A1 (fr) * | 1985-06-20 | 1986-12-26 | Snecma | Dispositif de variation de section de passage d'un distributeur de turbine |
| EP0545656A1 (fr) * | 1991-12-02 | 1993-06-09 | General Electric Company | Montage d'aubage statorique à calage variable pour compresseur axial de turbine à gaz |
| FR2699595A1 (fr) * | 1992-12-23 | 1994-06-24 | Snecma | Dispositif de guidage en rotation d'un anneau de commande d'aubes pivotantes. |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP4130441A1 (fr) * | 2021-08-05 | 2023-02-08 | MTU Aero Engines AG | Dispositif de liaison d'une aube à calage variable d'une turbine à gaz et turbine à gaz |
Also Published As
| Publication number | Publication date |
|---|---|
| CA2455016A1 (fr) | 2004-07-17 |
| FR2850131A1 (fr) | 2004-07-23 |
| FR2850131B1 (fr) | 2005-02-25 |
| JP2004225693A (ja) | 2004-08-12 |
| US20040146398A1 (en) | 2004-07-29 |
| RU2004101422A (ru) | 2005-07-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2577593C (fr) | Dispositif de reglage du centrage d'un anneau de synchronisation de commande d'aubes pivotantes de turbomachine | |
| EP0810944B1 (fr) | Axe de blocage rapide destine a etre utilise sur un cycle | |
| FR3111161A1 (fr) | Systeme de verrouillage d'aubes de soufflante a calage variable | |
| EP0115724B1 (fr) | Dispositif de bridage notamment pour la fixation de pièces sur une machine-outil | |
| FR3115817A1 (fr) | Bride de verrouillage d'aubes de soufflante à calage variable | |
| FR2699595A1 (fr) | Dispositif de guidage en rotation d'un anneau de commande d'aubes pivotantes. | |
| CA2503050C (fr) | Dispositif d'assemblage de brides annulaires, en particulier dans une turbomachine | |
| EP1696134A2 (fr) | Dispositif de réglage du centrage d'un anneau de synchronisation de commande d'aubes pivotantes de turbomachine | |
| CA2583850C (fr) | Aube de stator a calage variable de turbomachine | |
| EP2053203B1 (fr) | Perfectionnement à un anneau de commande de calage des aubes fixes d'une turbomachine. | |
| FR2491024A1 (fr) | Dispositif reglable de support pour un ensemble colonne et arbre de direction pouvant basculer | |
| EP1439283A1 (fr) | Agencement de montage d'aubes a calage variable | |
| CA2530133A1 (fr) | Dispositif de liaison, de longueur ajustable, entre deux pieces | |
| CA2470089C (fr) | Dispositif de guidage d'une aube a angle de calage variable | |
| FR3069013B1 (fr) | Dispositif de calage reglable d'une aube pivotante pour un redresseur de flux | |
| FR3009335A1 (fr) | Dispositif de guidage d'aubes de redresseur a angle de calage variable de turbomachine | |
| CA1038231A (fr) | Pompes centrifuges | |
| EP1577495A1 (fr) | Palier à roulement de turbomachine à encombrement réduit | |
| FR2882570A1 (fr) | Dipositif de commande d'aubes a calage variable dans une turbomachine | |
| FR2882577A1 (fr) | Dispositif de reglage du centrage d'un anneau de synchronisation de commande d'aubes pivotantes de turbomachine | |
| FR2742800A1 (fr) | Agencement d'extremites internes d'un etage d'aubes a calage variable | |
| FR2877059A1 (fr) | Biellette de commande destinee a l'entrainement d'une aube a calage variable | |
| EP3770472B1 (fr) | Vanne papillon perfectionnée pour le transport de fluide sous haute pression ou sous extrême pression | |
| FR3083286A1 (fr) | Vanne pourvue d'un organe de stabilisation solidaire du volet et ligne d'echappement equipee d'une telle vanne | |
| FR2743846A1 (fr) | Douille de retenue d'aube pivotante et agencement correspondant |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
| AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
| 17P | Request for examination filed |
Effective date: 20050107 |
|
| AKX | Designation fees paid |
Designated state(s): DE ES FR GB IT SE |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: SNECMA |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
| 18D | Application deemed to be withdrawn |
Effective date: 20060308 |