KR860006618A - 배기 개스 터보급기의 터빈 - Google Patents

배기 개스 터보급기의 터빈 Download PDF

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Publication number
KR860006618A
KR860006618A KR1019860000994A KR860000994A KR860006618A KR 860006618 A KR860006618 A KR 860006618A KR 1019860000994 A KR1019860000994 A KR 1019860000994A KR 860000994 A KR860000994 A KR 860000994A KR 860006618 A KR860006618 A KR 860006618A
Authority
KR
South Korea
Prior art keywords
turbine
exhaust gas
guide ring
gas turbocharger
inner contour
Prior art date
Application number
KR1019860000994A
Other languages
English (en)
Other versions
KR940000336B1 (ko
Inventor
린지 울리히
Original Assignee
비비씨 브라운, 보베리 앤드 컴퍼니, 리미티드, 바덴
칼피도욱스,게르트뤽
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 비비씨 브라운, 보베리 앤드 컴퍼니, 리미티드, 바덴, 칼피도욱스,게르트뤽 filed Critical 비비씨 브라운, 보베리 앤드 컴퍼니, 리미티드, 바덴
Publication of KR860006618A publication Critical patent/KR860006618A/ko
Application granted granted Critical
Publication of KR940000336B1 publication Critical patent/KR940000336B1/ko

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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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • 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
    • F01D17/18—Final actuators arranged in stator parts varying effective number of nozzles or guide conduits, e.g. sequentially operable valves for steam turbines
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

내용 없음

Description

배기 개스 터보급기의 터빈
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 주안내링 및 보조 안내링과 아울러, 상류에 나비 밸브를 부착하고 있는 배기개스터보급기의 터빈의 축상 단면도.
제2도는 안내링과 회전날개의 내측 윤곽을 제1도와 다르게한 배개개스 터보급기의터빈의 축상단면도.
* 도면의 주요부분에 대한 부호의 설명
1…케이싱 1a…격벽
1b…보강대 2…주공급도관
3…보조공급도관 4…나비밸브
5…회전자 6…회전날개
7…주안내링 8…보조안내링
9…터빈고정 덮개링 9a…홈
10…볼트 11…내벽
12…볼트 13…링
14…맞춤못 A…직경
B…직경 C1…회전날개의 내측윤곽
C2…주안내링의 내측윤곽

Claims (4)

  1. 서로 개별적으로 공급 도관(2,3)을 갖춘 주안내링(7)과 보조 안내링(8)으로 구성하여 안내판들을 갖추도록 한 안내장치를 터빈의 회전 날개의 상류에 설치하는 한편, 보조 안내링(8)으로 향한 배기개스의 흐름은 나비밸브(4)로 제어할 수 있도록 한 것으로서, 보조 안내링(8)은 주 안내링(7)보다 작은 직경으로 설치하고 나비밸브(4)는 보조 안내링(8)의 상류에 설치하였음을 특징으로 하는 내연기관용 배기개스 터보급기의 터빈.
  2. 제1항의 것에 있어서, 주 안내링(7)의 내측윤곽(C2)이 회전날개(6)의 내측윤곽(C1)의 연장선상에 사실상 놓여있도록 하였음을 특징으로 하는 배기개스 터보급기의 터빈.
  3. 제2항의 것에 있어서, 주 안내링(7)의 하류측 가장 자리와 내측윤곽(C2)이 교차하는 지점에서의 직경(A)은 주 안내링(7)의 하류측 가장 자리와 내측윤곽(C1)이 교차하는 지점에서의 직경(B)의 85∼110%가 되도록 하였음을 특징으로 하는 배기개스 터보급기의 터빈.
  4. 제1항의 것에 있어서, 나비 밸브(4)는 개스유입케이싱내에 설치하였음을 특징으로하는 배기개스 터보급기의 터빈.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019860000994A 1985-02-20 1986-02-13 배기 개스 터보과급기의 터빈 KR940000336B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH771/85-3 1985-02-20
CH77185 1985-02-20

Publications (2)

Publication Number Publication Date
KR860006618A true KR860006618A (ko) 1986-09-13
KR940000336B1 KR940000336B1 (ko) 1994-01-17

Family

ID=4194797

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019860000994A KR940000336B1 (ko) 1985-02-20 1986-02-13 배기 개스 터보과급기의 터빈

Country Status (9)

Country Link
US (1) US4655038A (ko)
EP (1) EP0191380B1 (ko)
JP (1) JPS61192814A (ko)
KR (1) KR940000336B1 (ko)
CN (1) CN1004818B (ko)
DE (1) DE3666601D1 (ko)
DK (1) DK160953C (ko)
PL (1) PL149193B1 (ko)
SU (1) SU1480776A3 (ko)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3715729C1 (de) * 1987-05-12 1988-09-08 Krupp Mak Maschb Gmbh Turbinengehaeuse fuer einen Abgasturbolader einer Brennkraftmaschine
GB2252133A (en) * 1991-01-25 1992-07-29 Gec Aerospace Ltd Gas turbines
DE19618314A1 (de) * 1996-05-08 1997-11-13 Asea Brown Boveri Abgasturbine eines Abgasturboladers
DE19850732A1 (de) * 1998-11-04 2000-05-11 Asea Brown Boveri Axialturbine
WO2010085494A1 (en) 2009-01-20 2010-07-29 Williams International Co., L.L.C. Turbocharger with turbine nozzle cartridge
JP5222274B2 (ja) * 2009-02-18 2013-06-26 三菱重工業株式会社 軸流タービンを備えたターボ過給機
JP5192507B2 (ja) * 2010-03-19 2013-05-08 川崎重工業株式会社 ガスタービンエンジン
JP5342594B2 (ja) * 2011-03-31 2013-11-13 三菱重工業株式会社 ターボ過給機
DE102011080596A1 (de) * 2011-08-08 2013-02-14 Abb Turbo Systems Ag Anordnung für ein Leiten eines Abgases in einer axial angeströmten Abgasturbine
JP5260724B2 (ja) * 2011-12-28 2013-08-14 三菱重工業株式会社 ターボ過給機
DE102012211950A1 (de) 2012-07-09 2014-05-08 Abb Turbo Systems Ag Abgasturbine
EP2781695A1 (de) * 2013-03-22 2014-09-24 ABB Turbo Systems AG Leitvorrichtung einer Abgasturbine
JP5960105B2 (ja) * 2013-09-11 2016-08-02 三菱重工業株式会社 ターボ過給機、タービンノズル及び船舶
CN104110300B (zh) * 2014-08-06 2017-05-10 无锡康明斯涡轮增压技术有限公司 涡轮增压器
CN105065068B (zh) * 2015-08-13 2016-07-20 德阳东汽电站机械制造有限公司 一种用于汽轮机排汽缸的导流环
US11339710B2 (en) * 2018-05-09 2022-05-24 Feizal Alli Gaffoor Turbocharger

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR403153A (fr) * 1908-07-24 1909-10-27 App Rateau Soc D Expl Des Procédé et dispositifs de distribution combinée pour turbines à vapeurs mixtes
DE895293C (de) * 1950-11-05 1953-11-02 Licentia Gmbh Regelstufe von Axialturbinen fuer grosse Dampfdurchsatzmengen
FR1194802A (fr) * 1958-04-17 1959-11-12 Rateau Et Rene Anxionnaz Soc Perfectionnement aux turbines à gaz
US3270495A (en) * 1963-08-14 1966-09-06 Caterpillar Tractor Co Apparatus for controlling speed and vibration of engine turbochargers
FR1333843A (fr) * 1962-06-18 1963-08-02 Rateau Soc Dispositif d'injection du fluide moteur dans les turbines de grande puissance
DE2618194A1 (de) * 1975-04-28 1976-11-11 Garrett Corp Turbomaschine
FR2351249A1 (fr) * 1976-05-14 1977-12-09 Europ Turb Vapeur Perfectionnement a un dispositif d'admission du fluide moteur dans une turbine de grande puissance
DE2840201A1 (de) * 1978-09-15 1980-03-27 Maschf Augsburg Nuernberg Ag Vorrichtung zur veraenderung der zustroemquerschnittsflaeche der turbine eines abgasturboladers
US4406125A (en) * 1981-08-10 1983-09-27 Ford Motor Company Variable flow rate turbocharger
CH654625A5 (de) * 1981-11-30 1986-02-28 Bbc Brown Boveri & Cie Einlassgehaeuse einer dampfturbine.
JPS6010834B2 (ja) * 1982-01-09 1985-03-20 石川島播磨重工業株式会社 溶接装置の開先倣い装置
US4512714A (en) * 1982-02-16 1985-04-23 Deere & Company Variable flow turbine
DE3375419D1 (en) * 1982-04-29 1988-02-25 Bbc Brown Boveri & Cie Turbo charger with a sliding ring valve

Also Published As

Publication number Publication date
US4655038A (en) 1987-04-07
SU1480776A3 (ru) 1989-05-15
PL258019A1 (en) 1986-10-21
EP0191380B1 (de) 1989-10-25
KR940000336B1 (ko) 1994-01-17
CN86100943A (zh) 1986-08-20
DK76186A (da) 1986-08-21
DK160953C (da) 1991-11-04
EP0191380A1 (de) 1986-08-20
DE3666601D1 (en) 1989-11-30
JPS61192814A (ja) 1986-08-27
CN1004818B (zh) 1989-07-19
DK76186D0 (da) 1986-02-18
DK160953B (da) 1991-05-06
PL149193B1 (en) 1990-01-31

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