EP1128025A2 - Strömungsmaschine radialer Bauart - Google Patents
Strömungsmaschine radialer Bauart Download PDFInfo
- Publication number
- EP1128025A2 EP1128025A2 EP01100423A EP01100423A EP1128025A2 EP 1128025 A2 EP1128025 A2 EP 1128025A2 EP 01100423 A EP01100423 A EP 01100423A EP 01100423 A EP01100423 A EP 01100423A EP 1128025 A2 EP1128025 A2 EP 1128025A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- guide vanes
- sliding ring
- ring
- guide blade
- impeller
- 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- Withdrawn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
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
- F01D17/165—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 invention relates to a fluid flow machine of the radial type according to the Generic term of patent claim 1.
- the invention is therefore based on the object of applying both requirements at the same time meet without the structural effort goes beyond the scope.
- the torsion of the guide vanes results in the recesses during axial movement the slot ring both to a change in the exit angle after the Leitapparat, as well as a change in the free flow cross-section. This results in an optimal adaptation of the turbomachine unsteady states, for example at the entrance to an exhaust gas turbine of an ATL.
- Fig. 1 shows a longitudinal section through a turbomachine, shown here Example of an exhaust gas turbine from an ATL.
- the exhaust gas turbine consists essentially of a spiral housing 1 for supplying the exhaust gas, an adjustable diffuser 2, an impeller 3 and a housing 4.
- the adjustable diffuser 2 consists of guide vanes 5 with a Twist. The twist is clearly shown in Fig. 3.
- the guide vanes (5) are rotatable on the one hand with pins 6, but axially fixed in one Sliding ring 7 mounted, on the other hand in a slot ring 8, which is fixed to the housing 4th connected is.
- the sliding ring 7 is concentric with a running axis 9 of the impeller 3 arranged and can, as indicated by the arrow, together with the guide vanes 5 be moved axially.
- the guide device 2 makes one without excessive construction effort optimal adaptation to a transient amount of exhaust gas and exhaust gas enthalpy Internal combustion engine possible.
- Fig. 3 shows the slot ring 8 in a view from the output side of the exhaust gas turbine
- the torsion of the guide vanes 5 can be seen 1 slide ring 7 shown in Fig. 1 move in the axial direction, they twist because of their twist around their pins 6, since they can be seen in FIG. 2 Recesses 10 are performed with play.
- the outflow angle and the free flow cross section vary at the same time. The construction effort is kept within reasonable limits.
- the adjustable guide apparatus shown using the example of an exhaust gas turbine can of course be used also apply to compressors to extract the kinetic energy from there Impeller gas flow emerging to be converted into static pressure energy with as little loss as possible.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
- Fig. 1
- einen Längsschnitt durch eine Abgasturbine eines ATL mit Leitapparat und Laufrad
- Fig. 2
- eine Ansicht des Laufrades mit Schlitzring von der Austrittsseite der Abgasturbine her gesehen
- Fig. 3
- eine Ansicht des Schieberinges mit Leitschaufeln
Claims (1)
- Strömungsmaschine radialer Bauart mit Spiralgehäuse, einem verstellbaren Leitapparat bestehend aus Leitschaufeln und Verstellmechanismus und einem Laufrad mit Gehäuse, dadurch gekennzeichnet, daß die Leitschaufeln (5) mit Verwindung ausgeführt sind, daß die Leitschaufeln (5) einerseits mittels Zapfen (6) drehbar, aber axial fixiert in einem Schiebering (7) gelagert sind, wobei der Schiebering (7) konzentrisch zur Laufachse (9) eines Laufrades (3) angeordnet und zu dieser axial verschiebbar ist, und daß die Leitschaufeln (5) andererseits in Aussparungen (10) eines Schlitzrings (8) derart geführt sind, so daß sie bei axialer Verschiebung des Schieberinges (7) wegen ihrer Verwindung eine Drehbewegung um die Zapfen (6) ausführen.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10009099 | 2000-02-25 | ||
DE2000109099 DE10009099A1 (de) | 2000-02-25 | 2000-02-25 | Strömungsmaschine radialer Bauart |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1128025A2 true EP1128025A2 (de) | 2001-08-29 |
EP1128025A3 EP1128025A3 (de) | 2003-01-02 |
Family
ID=7632524
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01100423A Withdrawn EP1128025A3 (de) | 2000-02-25 | 2001-01-08 | Strömungsmaschine radialer Bauart |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1128025A3 (de) |
DE (1) | DE10009099A1 (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004035994A1 (en) * | 2002-09-18 | 2004-04-29 | Honeywell International Inc. | Variable nozzle device for a turbocharger and method for operating the same |
WO2004074643A1 (en) * | 2003-02-19 | 2004-09-02 | Honeywell International Inc. | Nozzle device for a turbocharger and associated control method |
EP1571298A1 (de) * | 2004-03-02 | 2005-09-07 | Siemens Aktiengesellschaft | Schaufel für eine Strömungsmaschine und Strömungsmaschine |
GB2467382A (en) * | 2009-02-03 | 2010-08-04 | Cummins Turbo Tech Ltd | Variable geometry turbine |
US20140248138A1 (en) * | 2008-07-25 | 2014-09-04 | Cummins Turbo Technologies Limited | Variable geometry turbine |
WO2017005470A1 (de) * | 2015-07-08 | 2017-01-12 | Continental Automotive Gmbh | Abgasturbolader mit verstellbarer turbinengeometrie |
WO2019239076A1 (fr) * | 2018-06-14 | 2019-12-19 | Liebherr-Aerospace Toulouse Sas | Système de conditionnement d'air d'une cabine d'aeronef comprenant une turbomachine equipée d'un distributeur de turbine radiale |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5666498A (en) * | 1979-11-05 | 1981-06-04 | Hitachi Ltd | Vaned diffuser |
DE4218229C1 (en) * | 1992-06-03 | 1993-03-04 | Man B & W Diesel Ag, 8900 Augsburg, De | Turbocharger with radial flow through impeller - has blade retaining recesses, into which blades are insertable after axial shift of adjuster |
US5214920A (en) * | 1990-11-27 | 1993-06-01 | Leavesley Malcolm G | Turbocharger apparatus |
US5452986A (en) * | 1994-01-12 | 1995-09-26 | Dresser-Rand Company | Vaned diffuser |
WO1999053180A1 (de) * | 1998-04-15 | 1999-10-21 | Daimlerchrysler Ag | Abgasturboladerturbine |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4232400C1 (de) * | 1992-03-14 | 1993-08-19 | Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De |
-
2000
- 2000-02-25 DE DE2000109099 patent/DE10009099A1/de not_active Withdrawn
-
2001
- 2001-01-08 EP EP01100423A patent/EP1128025A3/de not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5666498A (en) * | 1979-11-05 | 1981-06-04 | Hitachi Ltd | Vaned diffuser |
US5214920A (en) * | 1990-11-27 | 1993-06-01 | Leavesley Malcolm G | Turbocharger apparatus |
DE4218229C1 (en) * | 1992-06-03 | 1993-03-04 | Man B & W Diesel Ag, 8900 Augsburg, De | Turbocharger with radial flow through impeller - has blade retaining recesses, into which blades are insertable after axial shift of adjuster |
US5452986A (en) * | 1994-01-12 | 1995-09-26 | Dresser-Rand Company | Vaned diffuser |
WO1999053180A1 (de) * | 1998-04-15 | 1999-10-21 | Daimlerchrysler Ag | Abgasturboladerturbine |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 005, no. 131 (M-084), 21. August 1981 (1981-08-21) & JP 56 066498 A (HITACHI LTD), 4. Juni 1981 (1981-06-04) * |
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004035994A1 (en) * | 2002-09-18 | 2004-04-29 | Honeywell International Inc. | Variable nozzle device for a turbocharger and method for operating the same |
US7497654B2 (en) | 2002-09-18 | 2009-03-03 | Honeywell International Inc. | Variable nozzle device for a turbocharger and method for operating the same |
WO2004074643A1 (en) * | 2003-02-19 | 2004-09-02 | Honeywell International Inc. | Nozzle device for a turbocharger and associated control method |
US7458764B2 (en) * | 2003-02-19 | 2008-12-02 | Honeywell International, Inc. | Nozzle device for a turbocharger and associated control method |
EP1571298A1 (de) * | 2004-03-02 | 2005-09-07 | Siemens Aktiengesellschaft | Schaufel für eine Strömungsmaschine und Strömungsmaschine |
WO2005085601A1 (de) * | 2004-03-02 | 2005-09-15 | Siemens Aktiengesellschaft | Axial durchströmbare, stationäre gasturbine |
US9404383B2 (en) * | 2008-07-25 | 2016-08-02 | Cummins Turbo Technologies Limited | Variable geometry turbine |
US20140248138A1 (en) * | 2008-07-25 | 2014-09-04 | Cummins Turbo Technologies Limited | Variable geometry turbine |
GB2467382B (en) * | 2009-02-03 | 2015-02-18 | Cummins Turbo Tech Ltd | Variable geometry turbine |
GB2467382A (en) * | 2009-02-03 | 2010-08-04 | Cummins Turbo Tech Ltd | Variable geometry turbine |
WO2017005470A1 (de) * | 2015-07-08 | 2017-01-12 | Continental Automotive Gmbh | Abgasturbolader mit verstellbarer turbinengeometrie |
CN107683364A (zh) * | 2015-07-08 | 2018-02-09 | 大陆汽车有限公司 | 具有可调整涡轮机几何构型的排气涡轮增压器 |
CN107683364B (zh) * | 2015-07-08 | 2020-03-06 | 大陆汽车有限公司 | 具有可调整涡轮机几何构型的排气涡轮增压器 |
US10774732B2 (en) | 2015-07-08 | 2020-09-15 | Vitesco Technologies GmbH | Exhaust-gas turbocharger with adjustable turbine geometry |
WO2019239076A1 (fr) * | 2018-06-14 | 2019-12-19 | Liebherr-Aerospace Toulouse Sas | Système de conditionnement d'air d'une cabine d'aeronef comprenant une turbomachine equipée d'un distributeur de turbine radiale |
FR3082563A1 (fr) * | 2018-06-14 | 2019-12-20 | Liebherr-Aerospace Toulouse Sas | Distributeur d'une turbine radiale de turbomachine, turbomachine comprenant un tel distributeur et systeme de conditionnement d'air comprenant une telle turbomachine |
US11434780B2 (en) | 2018-06-14 | 2022-09-06 | Liebherr-Aerospace Toulouse Sas | Air-conditioning system for an aircraft cabin, comprising a turbomachine provided with a radial turbine distributor |
Also Published As
Publication number | Publication date |
---|---|
EP1128025A3 (de) | 2003-01-02 |
DE10009099A1 (de) | 2001-08-30 |
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