ES8402637A1 - Through-flow arrangement for the volute inlet of a radial turbine. - Google Patents
Through-flow arrangement for the volute inlet of a radial turbine.Info
- Publication number
- ES8402637A1 ES8402637A1 ES519793A ES519793A ES8402637A1 ES 8402637 A1 ES8402637 A1 ES 8402637A1 ES 519793 A ES519793 A ES 519793A ES 519793 A ES519793 A ES 519793A ES 8402637 A1 ES8402637 A1 ES 8402637A1
- Authority
- ES
- Spain
- Prior art keywords
- rotor
- volute casing
- flow path
- casing portion
- intake
- 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
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
- F01D9/026—Scrolls for radial machines or engines
-
- 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
- F01D17/146—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by throttling the volute inlet of radial machines or engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Valve Device For Special Equipments (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Paper (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. An exhaust gas turbine with a variable flow, in particular for driving turbochargers of internal combustion engines, comprising a rotor (28) which is rotatable about an axis and which has a multiplicity of rotor blades (34) which are arranged at peripheral spacings from each other, a turbine casing (13) in which the rotor is rotatable and which has an outlet (32) which is coaxial with respect to the rotor, a volute casing portion (16) and a curved intake portion (14) with an inlet (22) arranged at a spacing from the axis, a partitioning wall which forms an outer and an inner flow path (56, 54) in the intake portion (14) and in the volute casing portion (16), which is curved within the volute casing portion (16) in the same direction as said volute casing portion and which is so arranged in the volute casing portion (16) that there is formed a fixed guide surface tip (52) which lies substantially tangentially at the outer periphery of the rotor (22) and which keeps the outer and inner flow paths separate and the inner flow path (54), within the volute casing portion (16) to directly to the periphery of the rotor (28), is of a cross-sectional area which decreases as said flow path (54) increasingly approaches the rotor, and a valve-like member (36) with actuating means for varying the intake flow cross-section of one of the two flow paths in the intake portion (14), characterised in that the intake portion (14) which extends between its connection (18) to the exhaust gas manifold of the internal combustion engine and the connection to the volute casing portion (16) and the part of the partitioning wall (50) which is disposed in the intake portion (14) are curved in the same direction as the volute casing portion (16), that the partitioning wall (50) extends in the volute casing portion (16) in such a way that the end thereof itself forms the guide surface tip (52) which lies substantially tangentially at the periphery of the rotor (28) and the cross-sectional areas of the outer flow path (56) as well as those of the inner flow path (54), within the volute casing to directly to the periphery of the rotor (28), progressively decrease in the direction in which the flow path increasingly approaches the rotor (28), and that the valve-like member (36) is so associated with the inner flow path (54) that upon movement of the valve-like member (36) towards the position of closing off the inner flow path (54) both the average radius of curvature of the mass flow and the flow speed of the exhaust gases increase.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US34928382A | 1982-02-16 | 1982-02-16 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES519793A0 ES519793A0 (en) | 1984-02-01 |
| ES8402637A1 true ES8402637A1 (en) | 1984-02-01 |
Family
ID=23371688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES519793A Expired ES8402637A1 (en) | 1982-02-16 | 1983-02-15 | Through-flow arrangement for the volute inlet of a radial turbine. |
Country Status (10)
| Country | Link |
|---|---|
| EP (1) | EP0086466B1 (en) |
| JP (1) | JPS58150028A (en) |
| AT (1) | ATE27474T1 (en) |
| AU (1) | AU550503B2 (en) |
| BR (1) | BR8300621A (en) |
| CA (1) | CA1206419A (en) |
| DE (1) | DE3371804D1 (en) |
| ES (1) | ES8402637A1 (en) |
| MX (1) | MX156452A (en) |
| ZA (1) | ZA831015B (en) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59144101U (en) * | 1983-03-18 | 1984-09-26 | 株式会社小松製作所 | Variable vaneless housing switching device |
| JPS60128931A (en) * | 1983-12-16 | 1985-07-10 | Mazda Motor Corp | Exhaust turbine supercharger |
| DE29716357U1 (en) | 1997-09-11 | 1998-02-12 | Ohra Regalanlagen GmbH, 50169 Kerpen | Steel construction platform |
| DE102006060907A1 (en) | 2006-12-20 | 2008-06-26 | Mp-Engineering Gmbh | Turbocharger has controlling unit that has rotary rolling slider that is supported in turbine housing, which has cross opening that is based on longitudinal axis, and is excentricaly arranged for longitudinal axis |
| US7694518B2 (en) * | 2007-08-14 | 2010-04-13 | Deere & Company | Internal combustion engine system having a power turbine with a broad efficiency range |
| DE102008020406A1 (en) * | 2008-04-24 | 2009-10-29 | Daimler Ag | Exhaust gas turbocharger for an internal combustion engine of a motor vehicle and internal combustion engine |
| DE102009056632A1 (en) * | 2009-12-02 | 2011-06-09 | Continental Automotive Gmbh | turbocharger |
| KR101051016B1 (en) | 2010-12-14 | 2011-07-21 | 한국기계연구원 | Turbine having separated flow path |
| KR101924920B1 (en) | 2011-06-10 | 2018-12-04 | 보르그워너 인코퍼레이티드 | Double flow turbine housing turbocharger |
| CN103557069A (en) * | 2013-11-13 | 2014-02-05 | 中国北方发动机研究所(天津) | Switchable double-inlet asymmetric turbine volute |
| US10267318B2 (en) | 2014-03-21 | 2019-04-23 | Fluid Equipment Development Company, Llc | Method and system for tuning a turbine using a secondary injection valve |
| CN106460533B (en) * | 2014-05-19 | 2019-10-18 | 博格华纳公司 | For save fuel and via asymmetric double spiral case exhaust gas recycling optimization pulse power separation double volute turbocharger |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH239435A (en) * | 1942-05-23 | 1945-10-15 | Buechi Alfred | Free-floating turbine, especially for hot gases. |
| NL296316A (en) * | 1962-08-07 | |||
| CA1026234A (en) * | 1972-12-06 | 1978-02-14 | Cummins Engine Company | Turbine housing |
| US4027994A (en) * | 1975-08-08 | 1977-06-07 | Roto-Master, Inc. | Partially divided turbine housing for turbochargers and the like |
| US4177006A (en) * | 1977-09-29 | 1979-12-04 | The Garrett Corporation | Turbocharger control |
| JPS5849682B2 (en) * | 1977-10-05 | 1983-11-05 | 三菱重工業株式会社 | Turbine casing manufacturing method |
| DE2934041C2 (en) * | 1979-08-23 | 1983-08-11 | Günther Prof. Dr.-Ing. 5100 Aachen Dibelius | Controlled exhaust gas turbocharger turbine |
| DE3034271C2 (en) * | 1979-09-17 | 1982-11-11 | Ishikawajima-Harima Jukogyo K.K., Tokyo | Turbine housing for turbocharger |
| JPS591332B2 (en) * | 1979-09-17 | 1984-01-11 | 石川島播磨重工業株式会社 | Turbine compartment for turbocharger |
-
1982
- 1982-12-20 AU AU91658/82A patent/AU550503B2/en not_active Ceased
-
1983
- 1983-01-11 MX MX195888A patent/MX156452A/en unknown
- 1983-02-08 BR BR8300621A patent/BR8300621A/en not_active IP Right Cessation
- 1983-02-09 CA CA000421254A patent/CA1206419A/en not_active Expired
- 1983-02-11 DE DE8383101306T patent/DE3371804D1/en not_active Expired
- 1983-02-11 EP EP83101306A patent/EP0086466B1/en not_active Expired
- 1983-02-11 AT AT83101306T patent/ATE27474T1/en active
- 1983-02-14 JP JP58022676A patent/JPS58150028A/en active Pending
- 1983-02-15 ES ES519793A patent/ES8402637A1/en not_active Expired
- 1983-02-15 ZA ZA831015A patent/ZA831015B/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| ES519793A0 (en) | 1984-02-01 |
| EP0086466A1 (en) | 1983-08-24 |
| DE3371804D1 (en) | 1987-07-02 |
| AU9165882A (en) | 1983-08-25 |
| ZA831015B (en) | 1984-09-26 |
| JPS58150028A (en) | 1983-09-06 |
| BR8300621A (en) | 1983-11-08 |
| MX156452A (en) | 1988-08-23 |
| EP0086466B1 (en) | 1987-05-27 |
| CA1206419A (en) | 1986-06-24 |
| AU550503B2 (en) | 1986-03-20 |
| ATE27474T1 (en) | 1987-06-15 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FD1A | Patent lapsed |
Effective date: 20010301 |