DE3371804D1 - 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
DE3371804D1
DE3371804D1 DE8383101306T DE3371804T DE3371804D1 DE 3371804 D1 DE3371804 D1 DE 3371804D1 DE 8383101306 T DE8383101306 T DE 8383101306T DE 3371804 T DE3371804 T DE 3371804T DE 3371804 D1 DE3371804 D1 DE 3371804D1
Authority
DE
Germany
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
Application number
DE8383101306T
Other languages
German (de)
Inventor
Merle Lavern Kaesser
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deere and Co
Original Assignee
Deere and Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Deere and Co filed Critical Deere and Co
Application granted granted Critical
Publication of DE3371804D1 publication Critical patent/DE3371804D1/en
Expired legal-status Critical Current

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

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.
DE8383101306T 1982-02-16 1983-02-11 Through-flow arrangement for the volute inlet of a radial turbine Expired DE3371804D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US34928382A 1982-02-16 1982-02-16

Publications (1)

Publication Number Publication Date
DE3371804D1 true DE3371804D1 (en) 1987-07-02

Family

ID=23371688

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8383101306T Expired DE3371804D1 (en) 1982-02-16 1983-02-11 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 (11)

* Cited by examiner, † Cited by third party
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
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
US9932843B2 (en) 2011-06-10 2018-04-03 Borgwarner Inc. 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
WO2015179386A1 (en) * 2014-05-19 2015-11-26 Borgwarner Inc. Dual volute turbocharger to optimize pulse energy separation for fuel economy and egr utilization via asymmetric dual volutes

Family Cites Families (9)

* Cited by examiner, † Cited by third party
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
JPS591332B2 (en) * 1979-09-17 1984-01-11 石川島播磨重工業株式会社 Turbine compartment for turbocharger
DE3034271C2 (en) * 1979-09-17 1982-11-11 Ishikawajima-Harima Jukogyo K.K., Tokyo Turbine housing for turbocharger

Also Published As

Publication number Publication date
AU550503B2 (en) 1986-03-20
ATE27474T1 (en) 1987-06-15
EP0086466B1 (en) 1987-05-27
ES519793A0 (en) 1984-02-01
MX156452A (en) 1988-08-23
JPS58150028A (en) 1983-09-06
ZA831015B (en) 1984-09-26
AU9165882A (en) 1983-08-25
BR8300621A (en) 1983-11-08
EP0086466A1 (en) 1983-08-24
CA1206419A (en) 1986-06-24
ES8402637A1 (en) 1984-02-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee