EP1303683A1 - Turbocompresseur a geometrie variable avec virole en tole - Google Patents
Turbocompresseur a geometrie variable avec virole en toleInfo
- Publication number
- EP1303683A1 EP1303683A1 EP00953257A EP00953257A EP1303683A1 EP 1303683 A1 EP1303683 A1 EP 1303683A1 EP 00953257 A EP00953257 A EP 00953257A EP 00953257 A EP00953257 A EP 00953257A EP 1303683 A1 EP1303683 A1 EP 1303683A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- casing
- nozzle
- cartridge
- ring
- unison
- 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
Links
- 239000002184 metal Substances 0.000 title description 4
- 239000007789 gas Substances 0.000 claims abstract description 8
- 238000013459 approach Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
-
- 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
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
-
- 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 present invention relates generally to the field of turbochargers having variable inlet geometry of turbines.
- the present invention more particularly provides a structural arrangement for a support of variable inlet vanes independent of the turbine casing.
- turbochargers have significantly increased the overall efficiency and capabilities of the turbochargers
- complexity of the support and actuation structures for the blades has increased manufacturing costs and occasionally created maintenance problems.
- connection of the support structure of the blades to the turbine casing limits the flexibility of design and structure of the turbine casing.
- Turbine housings constitute a sensitive thermal load which can act on the performance of emission systems in automotive applications.
- integration of turbine casings into the exhaust manifold can produce a reduction in the number of parts and the complexity for a turbocharger installation for an automobile. It is therefore desirable to provide structural support arrangements for variable nozzles independent of the turbine casing to improve actuation systems to increase reliability and decrease manufacturing costs for the turbochargers that use them.
- a variable geometry turbocharger using the present invention includes a central housing having a central bore for carrying a bearing assembly supporting a shaft with a turbine wheel mounted at a first end and a compressor turbine mounted at a second end.
- a compressor housing incorporating the turbine is attached to the central housing and has an air inlet and a compressed air outlet.
- a cartridge comprising a base and an insert is fixed to the central casing opposite the compressor casing.
- the cartridge has a base and an insert.
- the base and the insertion piece mutually form an exhaust inlet nozzle and the nozzle has an exhaust outlet with an aerodynamic contour corresponding to the turbine wheel.
- a plurality of vanes having rotating posts extending from a first surface substantially parallel to the internal wall of the nozzle constitute the variable nozzle.
- the posts are received in circumferentially spaced openings in the base of the inner wall of the nozzle.
- the posts include actuating arms extending to engage in notches in a ring in unison engaged between the central casing and the base.
- the actuation of the ring in unison is carried out by a crank comprising an actuating arm engaging in a slot in the ring in unison.
- the crank is continuously movable from a first position to a second position, causing the movement of the actuating arm in the radial slot and imparting a force perpendicular to the radial slot to cause the movement of rotation of the ring to the unison.
- the rotational movement of the ring in unison causes the blades to rotate by the blade arms.
- a sheet metal exhaust casing is mounted on the cartridge on the central casing, providing an inlet for the exhaust gas into the nozzle.
- Figure 1 is an elevational view of an embodiment of a turbocharger using the present invention
- Figure 2a is a half elevation in side section around the center line showing the details of an exhaust casing, a central casing and a cartridge mounting with the turbine shaft wheel mounting , as supported by the bearing system
- Figure 2b is a half elevation in side section along a plane rotated relative to Figure 2a to show other details of the cartridge
- FIG. 3 is a representative view of the central casing and of the cartridge assembly, showing an embodiment according to the invention, with the exhaust casing partially removed
- FIG. 4 is a second view of the central casing and of the cartridge assembly with the cut-out insert to reveal the blades of the nozzle with variable geometry;
- FIG. 5 is a representative view from below of the arms of the blades with variable geometry, of the ring in partial unison and of the assembly of the blade crank shown.
- the embodiment of the invention shown in Figure 1 includes a compressor housing 10 which is connected to a back plate 12 using two or more clamps 14 secured by bolts 16.
- the back plate is fixed to a central casing 18 with several bolts 20 and an annular seal 22.
- the sheet metal exhaust casing 24 is connected to the central casing using bands 26 fixed by bolts 28. The gases from exhaust or other high-energy gases supplying the turbocharger enter the exhaust casing through the inlet 32.
- a cartridge generally designated by 34, is mounted on the central housing.
- a turbine wheel and shaft assembly 30 is carried by the bearing, the turbine wheel being suspended inside the cartridge.
- Multiple blades 36 are mounted on a cartridge base 38.
- the blades pivot on posts 40 extending from the blades into holes 42 in a surface 43 of the base which constitutes the internal wall of the inlet nozzle.
- Arms actuator 44 extend from the posts of the blades to engage. in notches 46 in the ring in unison 48.
- An actuating crank 50 ends at a first end by a lever arm 52 carrying a pin 54 to engage with the slot 56 in the ring in unison for the rotation of the ring.
- the crank extends from a boss 58 in the central casing passing through a sleeve 60 ending on an external arm 62 for engagement by an actuating device.
- An insert 64 is fixed to the central casing by bolts 66 received in holes 68.
- Support posts 70 hold the base, pressing the base against spacing pins 39 (better seen in FIG. 1) received in the central casing.
- An edge 71 which extends around the circumference of the insert is also engaged by the V-shaped band clamp.
- the insert comprises the external wall of the nozzle 72 in the immediate vicinity of the blades.
- the insert constitutes the exhaust gas outlet from the turbine 73 with an aerodynamic contour fixing the blades on the wheel of the turbine.
- the insert and the base with the fixed vanes and the actuating elements constitute the cartridge, which is separated from both the central casing and the exhaust casing and fixed between these two components.
- the use of the cartridge of the present invention makes it possible to simplify the exhaust casing compared to the designs of the prior art, facilitating improvements such as a sheet metal exhaust casing, as shown in the embodiments of the drawings.
- a bearing system comprising two bearings 74 and a spacer bearing 76 or, in other embodiments, a unitary bearing, - supports the mounting of the shaft wheel in the central bore of the central casing - 78.
- the shaft further extends through a ring d 'support 80 which engages with a support bearing 82 carried between the central casing and the rear plate of the compressor.
- a piston ring 84 closes the support ring with the shaft bore in the rear plate.
- the turbine of compressor 86 is fixed to the shaft wheel assembly.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
- Control Of Turbines (AREA)
- Non-Positive Displacement Air Blowers (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/FR2000/002068 WO2002006637A1 (fr) | 2000-07-19 | 2000-07-19 | Turbocompresseur a geometrie variable avec virole en tole |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1303683A1 true EP1303683A1 (fr) | 2003-04-23 |
EP1303683B1 EP1303683B1 (fr) | 2008-07-30 |
EP1303683B2 EP1303683B2 (fr) | 2012-09-19 |
Family
ID=8847164
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00953257A Expired - Lifetime EP1303683B2 (fr) | 2000-07-19 | 2000-07-19 | Turbocompresseur a geometrie variable avec virole en tole |
Country Status (13)
Country | Link |
---|---|
US (1) | US6951450B1 (fr) |
EP (1) | EP1303683B2 (fr) |
JP (1) | JP4846961B2 (fr) |
KR (1) | KR100669487B1 (fr) |
CN (1) | CN1304732C (fr) |
AT (1) | ATE403068T1 (fr) |
AU (1) | AU2000265774A1 (fr) |
BR (1) | BR0017293B1 (fr) |
CA (1) | CA2416331C (fr) |
DE (1) | DE60039723D1 (fr) |
HU (1) | HUP0301321A2 (fr) |
MX (1) | MXPA03000497A (fr) |
WO (1) | WO2002006637A1 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10436069B2 (en) | 2017-01-30 | 2019-10-08 | Garrett Transportation I Inc. | Sheet metal turbine housing with biaxial volute configuration |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
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ATE403068T1 (de) | 2000-07-19 | 2008-08-15 | Honeywell Int Inc | Turbokompressor mit verstellbaren leitschaufeln und schneckengehäuse/einlauf aus blech |
DE60226784D1 (de) * | 2002-09-05 | 2008-07-03 | Honeywell Int Inc | Turbolader mit verstellbaren leitschaufeln |
EP1925784B1 (fr) | 2002-09-05 | 2011-07-20 | Honeywell International Inc. | Turbocompresseur comprenant un dispositif doté d'une buse variable |
DE10325649B4 (de) * | 2003-06-06 | 2014-10-23 | Ihi Charging Systems International Gmbh | Abgasturbine für einen Abgasturbolader |
AU2003279321A1 (en) * | 2003-10-24 | 2005-05-19 | Honeywell International Inc. | Turbocharger with a thin-walled turbine housing having a floating flange attachment to the centre housing |
DE102004038748A1 (de) * | 2004-08-10 | 2006-02-23 | Daimlerchrysler Ag | Abgasturbolader für eine Brennkraftmaschine |
DE102004039477B4 (de) * | 2004-08-14 | 2015-01-08 | Ihi Charging Systems International Gmbh | Turbinengehäuse für einen Abgasturbolader |
DE102004057864A1 (de) * | 2004-11-30 | 2006-06-01 | Borgwarner Inc.(N.D.Ges.D.Staates Delaware), Auburn Hills | Abgasturbolader, Leitapparat für einen Abgasturbolader sowie Schaufelhebel für einen Leitapparat |
EP2035673B1 (fr) * | 2006-06-19 | 2014-06-11 | Turbo Energy Limited | Mécanisme à aubes de stator à calage variable pour turbocompresseurs |
US7559199B2 (en) * | 2006-09-22 | 2009-07-14 | Honeywell International Inc. | Variable-nozzle cartridge for a turbocharger |
JP2008215083A (ja) * | 2007-02-28 | 2008-09-18 | Mitsubishi Heavy Ind Ltd | 可変容量型排気ターボ過給機における可変ノズル機構部取付構造 |
US7712311B2 (en) | 2007-03-14 | 2010-05-11 | Gm Global Technology Operations, Inc. | Turbocharger assembly with catalyst coating |
JP2010523898A (ja) * | 2007-04-10 | 2010-07-15 | エリオット・カンパニー | 可変入口案内翼を有する遠心圧縮機 |
DE102008005405B4 (de) * | 2008-01-21 | 2021-03-04 | BMTS Technology GmbH & Co. KG | Turbine, insbesondere für einen Abgasturbolader, sowie Abgasturbolader |
DE102008052456A1 (de) * | 2008-10-21 | 2010-04-22 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Turbolader mit variabler Turbinengeometrie |
DE102008053170A1 (de) * | 2008-10-24 | 2010-04-29 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Ladeeinrichtung mit variabler Turbinen-/Verdichtergeometrie, insbesondere für einen Abgasturbolader eines Kraftfahrzeugs |
DE102008057504A1 (de) | 2008-11-15 | 2010-05-20 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Ladeeinrichtung |
JP4759062B2 (ja) * | 2009-01-15 | 2011-08-31 | トヨタ自動車株式会社 | ターボチャージャおよびターボチャージャの製造方法 |
DE102009005013B4 (de) * | 2009-01-17 | 2019-12-12 | Ihi Charging Systems International Gmbh | Verbindungsanordnung eines Turbinengehäuses mit einem Lagergehäuse und Abgasturbolader |
EP3168429B1 (fr) * | 2009-01-20 | 2018-03-07 | Williams International Co., L.L.C. | Cartouche de roue statorique de turbine destiné à être utilisé avec un noyau de turbocompresseur |
DE102009007663A1 (de) | 2009-02-05 | 2010-08-12 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Ladeeinrichtung |
DE102009015353A1 (de) | 2009-03-27 | 2010-09-30 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Ladeeinrichtung |
US8579579B2 (en) * | 2009-11-10 | 2013-11-12 | Honeywell International Inc. | Sealed shaft assembly for exhaust turbines |
US20110138805A1 (en) * | 2009-12-15 | 2011-06-16 | Honeywell International Inc. | Conjugate curve profiles for vane arms, main-arms, and unison rings |
DE102009058534A1 (de) * | 2009-12-16 | 2011-06-22 | Bosch Mahle Turbo Systems GmbH & Co. KG, 70376 | Abgasturbolader für eine Brennkraftmaschine |
US9091208B2 (en) | 2010-07-16 | 2015-07-28 | Honeywell International Inc. | Turbocharger bearing housing assembly |
US9097120B2 (en) * | 2010-08-26 | 2015-08-04 | Honeywell International Inc. | Turbine housing assembly |
US9021802B2 (en) | 2010-08-26 | 2015-05-05 | Honeywell International Inc. | Turbine housing assembly with wastegate |
US8764384B2 (en) * | 2010-12-16 | 2014-07-01 | Honeywell International Inc. | Joint for housing alignment |
US9352270B2 (en) | 2011-04-11 | 2016-05-31 | ADA-ES, Inc. | Fluidized bed and method and system for gas component capture |
DE102011075794A1 (de) | 2011-05-13 | 2012-11-15 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable Turbinen-/Verdichtergeometrie |
DE102011050506B4 (de) * | 2011-05-19 | 2013-04-18 | Benteler Automobiltechnik Gmbh | Abgasturbolader |
DE102011087244A1 (de) * | 2011-11-28 | 2013-05-29 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Variable Turbinengeometrie |
EP2861834B1 (fr) | 2012-06-19 | 2021-04-14 | Volvo Lastvagnar AB | Dispositif pour réguler un flux de gaz, système de post-traitement d'échappement et système de propulsion d'un véhicule |
WO2014047354A1 (fr) | 2012-09-20 | 2014-03-27 | ADA-ES, Inc. | Procédé et système de récupération de sites fonctionnels sur un sorbant contaminé par des sels thermostables |
US9702299B2 (en) * | 2012-12-26 | 2017-07-11 | Honeywell International Inc. | Turbine assembly |
KR20150102045A (ko) * | 2012-12-28 | 2015-09-04 | 보르그워너 인코퍼레이티드 | Vtg 터보차저를 위한 비대칭 액추에이터 피벗 샤프트 부싱 |
JP5807037B2 (ja) * | 2013-05-16 | 2015-11-10 | 株式会社豊田自動織機 | 可変ノズルターボチャージャ |
US9702266B2 (en) | 2014-06-30 | 2017-07-11 | Honeywell International Inc. | Turbocharger turbine housing |
US10472988B2 (en) | 2017-01-30 | 2019-11-12 | Garrett Transportation I Inc. | Sheet metal turbine housing and related turbocharger systems |
US10494955B2 (en) | 2017-01-30 | 2019-12-03 | Garrett Transportation I Inc. | Sheet metal turbine housing with containment dampers |
US10544703B2 (en) | 2017-01-30 | 2020-01-28 | Garrett Transportation I Inc. | Sheet metal turbine housing with cast core |
US10690144B2 (en) | 2017-06-27 | 2020-06-23 | Garrett Transportation I Inc. | Compressor housings and fabrication methods |
DE112018003592A5 (de) | 2017-07-14 | 2020-04-09 | Ihi Charging Systems International Gmbh | Verbindungsvorrichtung für einen abgasturbolader und abgasturbolader |
US10495100B2 (en) * | 2017-11-24 | 2019-12-03 | Garrett Transportation I Inc. | Inlet-adjustment mechanism for turbocharger compressor, having sealing means preventing recirculation and/or oil migration into the mechanism |
US20190178255A1 (en) * | 2017-12-12 | 2019-06-13 | Honeywell International Inc. | Vapor cycle compressor with variable inlet/outlet geometry |
US10883379B2 (en) * | 2018-05-11 | 2021-01-05 | Rolls-Royce Corporation | Variable diffuser having a respective penny for each vane |
US10648360B1 (en) * | 2018-09-25 | 2020-05-12 | Garrett Transportation I Inc. | Turbocharger turbine assembly |
US10927702B1 (en) | 2019-03-30 | 2021-02-23 | Savant Holdings LLC | Turbocharger or turbocharger component |
US11732729B2 (en) | 2021-01-26 | 2023-08-22 | Garrett Transportation I Inc | Sheet metal turbine housing |
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KR100662242B1 (ko) † | 2000-01-14 | 2006-12-28 | 허니웰 가렛트 쏘시에떼 아노님 | 결합된 공기역학적 표면을 가진 슬라이딩 블레이드와 열스크린 및 작동장치를 구비한 터보 과급기 |
ATE403068T1 (de) | 2000-07-19 | 2008-08-15 | Honeywell Int Inc | Turbokompressor mit verstellbaren leitschaufeln und schneckengehäuse/einlauf aus blech |
-
2000
- 2000-07-19 AT AT00953257T patent/ATE403068T1/de not_active IP Right Cessation
- 2000-07-19 AU AU2000265774A patent/AU2000265774A1/en not_active Abandoned
- 2000-07-19 HU HU0301321A patent/HUP0301321A2/hu unknown
- 2000-07-19 EP EP00953257A patent/EP1303683B2/fr not_active Expired - Lifetime
- 2000-07-19 JP JP2002512514A patent/JP4846961B2/ja not_active Expired - Fee Related
- 2000-07-19 MX MXPA03000497A patent/MXPA03000497A/es active IP Right Grant
- 2000-07-19 US US10/332,840 patent/US6951450B1/en not_active Expired - Lifetime
- 2000-07-19 KR KR1020037000794A patent/KR100669487B1/ko active IP Right Grant
- 2000-07-19 CA CA002416331A patent/CA2416331C/fr not_active Expired - Fee Related
- 2000-07-19 CN CNB008171238A patent/CN1304732C/zh not_active Expired - Lifetime
- 2000-07-19 WO PCT/FR2000/002068 patent/WO2002006637A1/fr active Search and Examination
- 2000-07-19 DE DE60039723T patent/DE60039723D1/de not_active Expired - Lifetime
- 2000-07-19 BR BRPI0017293-6A patent/BR0017293B1/pt not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
See references of WO0206637A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10436069B2 (en) | 2017-01-30 | 2019-10-08 | Garrett Transportation I Inc. | Sheet metal turbine housing with biaxial volute configuration |
Also Published As
Publication number | Publication date |
---|---|
AU2000265774A1 (en) | 2002-01-30 |
BR0017293B1 (pt) | 2008-11-18 |
ATE403068T1 (de) | 2008-08-15 |
DE60039723D1 (de) | 2008-09-11 |
CA2416331C (fr) | 2009-10-20 |
US6951450B1 (en) | 2005-10-04 |
MXPA03000497A (es) | 2004-09-10 |
BR0017293A (pt) | 2003-07-29 |
KR100669487B1 (ko) | 2007-01-16 |
WO2002006637A1 (fr) | 2002-01-24 |
JP2004505190A (ja) | 2004-02-19 |
EP1303683B1 (fr) | 2008-07-30 |
CA2416331A1 (fr) | 2002-01-24 |
EP1303683B2 (fr) | 2012-09-19 |
JP4846961B2 (ja) | 2011-12-28 |
HUP0301321A2 (en) | 2003-08-28 |
CN1433501A (zh) | 2003-07-30 |
KR20030020389A (ko) | 2003-03-08 |
CN1304732C (zh) | 2007-03-14 |
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