EP1552112A2 - Turbolader mit einem einsatz mit doppeltem spiel für die leitschaufeln - Google Patents
Turbolader mit einem einsatz mit doppeltem spiel für die leitschaufelnInfo
- Publication number
- EP1552112A2 EP1552112A2 EP03767927A EP03767927A EP1552112A2 EP 1552112 A2 EP1552112 A2 EP 1552112A2 EP 03767927 A EP03767927 A EP 03767927A EP 03767927 A EP03767927 A EP 03767927A EP 1552112 A2 EP1552112 A2 EP 1552112A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- fins
- annular
- insert
- clearance
- notch
- 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- Withdrawn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
- 230000002093 peripheral effect Effects 0.000 claims abstract description 4
- 125000006850 spacer group Chemical group 0.000 claims abstract description 3
- 239000007789 gas Substances 0.000 claims description 6
- 238000007373 indentation Methods 0.000 abstract 2
- 230000000903 blocking effect Effects 0.000 description 2
- 230000010339 dilation Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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
- F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
-
- 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
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
Definitions
- the insert 30 is a flat annular piece, of the same dimensions as the wing-holding ring.
- the fin ring is kept spaced from the insert by means of several spacers 34 of selected height so that the top of the fins makes a predetermined functional play with it.
- FIG. 5 shows a turbocharger without insert.
- the fin ring 22 is fixed to a wall 28 of the passage which communicates the volute chamber 14 with the turbine wheel 16.
- the fins 24 make a nominal functional clearance e with the other face 46 or U-shaped face which delimits said passage.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0212723 | 2002-10-14 | ||
| FR0212723A FR2845731B1 (fr) | 2002-10-14 | 2002-10-14 | Turbocompresseur a insert double jeu pour vehicule automobile |
| PCT/FR2003/050087 WO2004036010A2 (fr) | 2002-10-14 | 2003-10-14 | Turbocompresseur a insert double jeu pour les aubes de guidage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1552112A2 true EP1552112A2 (de) | 2005-07-13 |
Family
ID=32039688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP03767927A Withdrawn EP1552112A2 (de) | 2002-10-14 | 2003-10-14 | Turbolader mit einem einsatz mit doppeltem spiel für die leitschaufeln |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP1552112A2 (de) |
| FR (1) | FR2845731B1 (de) |
| WO (1) | WO2004036010A2 (de) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0407978D0 (en) * | 2004-04-08 | 2004-05-12 | Holset Engineering Co | Variable geometry turbine |
| WO2007093406A1 (de) * | 2006-02-16 | 2007-08-23 | Borgwarner Inc. | Schaufellagerringanordnung eines turboladers mit variabler turbinengeometrie |
| US8056336B2 (en) * | 2008-05-05 | 2011-11-15 | Honeywell International Inc. | Turbocharger with variable nozzle having vane sealing surfaces |
| DE102008039093A1 (de) * | 2008-08-21 | 2010-02-25 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Abgasturbolader für ein Kraftfahrzeug |
| US9932888B2 (en) * | 2016-03-24 | 2018-04-03 | Borgwarner Inc. | Variable geometry turbocharger |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB880903A (en) * | 1957-04-15 | 1961-10-25 | Dowty Rotol Ltd | Improvements in or relating to turbines |
| US3495921A (en) * | 1967-12-11 | 1970-02-17 | Judson S Swearingen | Variable nozzle turbine |
| US4502836A (en) * | 1982-07-02 | 1985-03-05 | Swearingen Judson S | Method for nozzle clamping force control |
| DE3516738A1 (de) * | 1985-05-09 | 1986-11-13 | Mtu Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen | Stroemungsmaschine |
| US4679984A (en) * | 1985-12-11 | 1987-07-14 | The Garrett Corporation | Actuation system for variable nozzle turbine |
| US4741666A (en) * | 1985-12-23 | 1988-05-03 | Ishikawajima-Harima Jukogyo Kabushiki Kaisha | Variable displacement turbocharger |
| US4880351A (en) * | 1986-05-30 | 1989-11-14 | Honda Giken Kogyo Kabushiki Kaisha | Variable capacity turbine |
| JPS63183207A (ja) * | 1987-01-23 | 1988-07-28 | Honda Motor Co Ltd | 可変容量式タ−ビン |
| DE19752534C1 (de) * | 1997-11-27 | 1998-10-08 | Daimler Benz Ag | Radialdurchströmte Abgasturboladerturbine |
| DE19838928C1 (de) * | 1998-08-27 | 1999-04-22 | Daimler Chrysler Ag | Variabel einstellbares Leitschaufelgitter |
-
2002
- 2002-10-14 FR FR0212723A patent/FR2845731B1/fr not_active Expired - Fee Related
-
2003
- 2003-10-14 EP EP03767927A patent/EP1552112A2/de not_active Withdrawn
- 2003-10-14 WO PCT/FR2003/050087 patent/WO2004036010A2/fr not_active Ceased
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2004036010A3 * |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2845731A1 (fr) | 2004-04-16 |
| FR2845731B1 (fr) | 2005-01-28 |
| WO2004036010A3 (fr) | 2004-06-10 |
| WO2004036010A2 (fr) | 2004-04-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2718847C (fr) | Carter pour roue a aubes mobiles de turbomachine | |
| EP2307735B1 (de) | Turbomaschinenverdichter | |
| FR2814205A1 (fr) | Turbomachine a veine d'ecoulement ameliore | |
| FR2823794A1 (fr) | Aube rapportee et refroidie pour turbine | |
| CA2463186C (fr) | Dispositif de commande d'aubes a calage variable dans une turbomachine | |
| EP3201438B1 (de) | Laufschaufel einer turbomaschine mit einem flansch, der an einer sperrkerbe in der rotorscheibe anliegt | |
| EP1524406B1 (de) | Anordnung einer Turbomaschinenenlaufschaufel | |
| EP0424197A1 (de) | Drosselklappe | |
| FR2882570A1 (fr) | Dipositif de commande d'aubes a calage variable dans une turbomachine | |
| EP3084141B1 (de) | Turbinenmotorverdichter, insbesondere eines flugzeug-turbomotors oder mantelstrom-triebwerks | |
| WO2004036010A2 (fr) | Turbocompresseur a insert double jeu pour les aubes de guidage | |
| FR3067387A1 (fr) | Ecope d'alimentation en air pour l'alimentation d'un systeme de refroidissement et de controle des jeux d'une turbine | |
| FR3087855A1 (fr) | Un turbocompresseur centrifuge ayant un trajet de flux de gaz comportant une chambre de detente | |
| FR2888876A1 (fr) | Dispositif d'amortissement des vibrations d'un rotor dans une turbomachine | |
| EP1491721A1 (de) | Verdichterschaufel eines Strahltriebwerkes | |
| FR3077371A1 (fr) | Dispositif de ventilation et module de refroidissement comportant un tel dispositif de ventilation | |
| FR2863659A1 (fr) | Dispositif d'obturation d'un conduit d'une ligne d'echappement | |
| FR2650360A1 (fr) | Vanne a papillon | |
| WO2025158119A1 (fr) | Ensemble d'étanchéité amélioré pour turbine de turbomachine | |
| FR2881190A1 (fr) | Dispositif d'actionnement pour redresseurs a calage variable, et moteur d'aeronef equipe d'un tel dispositif | |
| FR3156861A1 (fr) | Traitement de carter non axisymétrique à ouverture piloté avec plenum | |
| EP4028654A1 (de) | Kühlmodul für ein motorfahrzeug, das eine strömungsmaschine umfasst | |
| WO2005075862A1 (fr) | Dispositif d 'obturation d'un conduit d'une ligne d'echappement | |
| FR2654154A1 (fr) | Robinet a papillon pour dispositif d'alimentation en carburant de moteur a combustion interne. | |
| WO2001034958A1 (fr) | Corps papillon possedant un papillon muni d'un lamage |
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 |
|
| 17P | Request for examination filed |
Effective date: 20050412 |
|
| AK | Designated contracting states |
Kind code of ref document: A2 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 |
|
| RBV | Designated contracting states (corrected) |
Designated state(s): BE DE ES GB IT |
|
| 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: 20101005 |