AU9165882A - Variable flow turbine - Google Patents

Variable flow turbine

Info

Publication number
AU9165882A
AU9165882A AU91658/82A AU9165882A AU9165882A AU 9165882 A AU9165882 A AU 9165882A AU 91658/82 A AU91658/82 A AU 91658/82A AU 9165882 A AU9165882 A AU 9165882A AU 9165882 A AU9165882 A AU 9165882A
Authority
AU
Australia
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.)
Granted
Application number
AU91658/82A
Other versions
AU550503B2 (en
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
Publication of AU9165882A publication Critical patent/AU9165882A/en
Application granted granted Critical
Publication of AU550503B2 publication Critical patent/AU550503B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026Scrolls for radial machines or engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/146Final 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Paper (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.
AU91658/82A 1982-02-16 1982-12-20 Variable flow turbine Ceased AU550503B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US34928382A 1982-02-16 1982-02-16
US349283 1982-02-16

Publications (2)

Publication Number Publication Date
AU9165882A true AU9165882A (en) 1983-08-25
AU550503B2 AU550503B2 (en) 1986-03-20

Family

ID=23371688

Family Applications (1)

Application Number Title Priority Date Filing Date
AU91658/82A Ceased AU550503B2 (en) 1982-02-16 1982-12-20 Variable flow 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) ES519793A0 (en)
MX (1) MX156452A (en)
ZA (1) ZA831015B (en)

Families Citing this family (12)

* 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
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
DE112012001912T5 (en) 2011-06-10 2014-01-30 Borgwarner Inc. Turbocharger with double-flow turbine housing
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)

* 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
ES8402637A1 (en) 1984-02-01
ATE27474T1 (en) 1987-06-15
CA1206419A (en) 1986-06-24
ES519793A0 (en) 1984-02-01
EP0086466B1 (en) 1987-05-27
ZA831015B (en) 1984-09-26
BR8300621A (en) 1983-11-08
MX156452A (en) 1988-08-23
EP0086466A1 (en) 1983-08-24
JPS58150028A (en) 1983-09-06
DE3371804D1 (en) 1987-07-02

Similar Documents

Publication Publication Date Title
EP0605184B1 (en) Turbocharger having reduced noise emissions
US4512714A (en) Variable flow turbine
US5146752A (en) Exhaust gas turbocharger on an internal-combustion engine
US3994620A (en) Variable exducer turbine control
US4565068A (en) Turbocharger
KR20030076984A (en) Bladeless turbocharger
AU550503B2 (en) Variable flow turbine
US8919119B2 (en) Sliding vane geometry turbines
JPS6138125A (en) Supercharger of exhaust gas turbine for internal combustion engine
ES8407336A1 (en) A variable inlet area turbine.
JPS5812479B2 (en) Yobisenkaitabochayasouchi
WO2015119828A1 (en) Heat shield for mixed flow turbine wheel turbochargers
GB1426554A (en) Turbo superchargers for internal combustion engines
FR2577999B1 (en) DISTRIBUTOR BLADE MUFFLER, MOUNTED ON THE SUCTION SIDE OF THE COMPRESSOR OF A TURBO-COMPRESSOR DRIVEN BY EXHAUST GASES
SE8603412L (en) DEVICE FOR DIRECTIONAL CHANGE OF A THROUGH INPUT TO A COMPRESSOR BY A EXHAUST TURCH CHARGER TO A COMBUSTION ENGINE INCOMING AIR FLOW
WO1999023374A3 (en) Jet engine having radial turbine blades and flow-directing turbine manifolds
US4655038A (en) Exhaust gas turbo-charger turbine
US3059415A (en) Turbocharger for internal combustion engines
SE8603410D0 (en) DEVICE FOR INCREASING THE SPEED OF A EXHAUST ROLLER
US4781528A (en) Variable capacity radial flow turbine
RU2750512C2 (en) System and method for reducing turbocharger compressor noise
JPS63306232A (en) Fluidic type variable displacement turbocharger
ES281744U (en) Scroll for a radial turbine.
JPS611829A (en) Tubo-supercharger
US4381172A (en) Centripetal flow gas turbine