KR940005867A - 축류 터빈 - Google Patents

축류 터빈 Download PDF

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Publication number
KR940005867A
KR940005867A KR1019930012647A KR930012647A KR940005867A KR 940005867 A KR940005867 A KR 940005867A KR 1019930012647 A KR1019930012647 A KR 1019930012647A KR 930012647 A KR930012647 A KR 930012647A KR 940005867 A KR940005867 A KR 940005867A
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KR
South Korea
Prior art keywords
guide
vane
vanes
guide vane
guide vanes
Prior art date
Application number
KR1019930012647A
Other languages
English (en)
Inventor
엘베크야에르 페테르
슈라이베르 발테르
Original Assignee
한스 요트, 헤쩨르, 하아, 카이저
아세아 브라운 보베리 리미티드
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 한스 요트, 헤쩨르, 하아, 카이저, 아세아 브라운 보베리 리미티드 filed Critical 한스 요트, 헤쩨르, 하아, 카이저
Publication of KR940005867A publication Critical patent/KR940005867A/ko

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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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/142Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • 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
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

축류 터빈은 한 열이상이 굽은 안내 날개(7)와 한열이상의 회전 날개를 구비한다. 안내 날개 크기 전체에 걸친 상기 안내 날개(7)의 굽음은 익현에 대하여 직각에서 선택되며 원주 방향에서 각각의 인접한 안내 날개의 압력측을 향한다. 상기 안내 날개는 그 방사범위에서 점감된다. 안내 날개에서 경계층의 편향에 의해 발생하는2차 손실이 이러한 방식에 의해 감소된다

Description

축류 터빈
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 터빈의 부분 단면도, 제2도는 제1도에 도시된 유관(流管)의 외경상 실린더형 부분의 부분 전개도, 제3도는 굽은 안내 날개의 뼈대의 투시도, 제4도는 굽은 안내 날개의 윤곽도, 제5도는 축방향부의 유선을 도시한다. 제6도는 관의 높이에 걸친 개스 배기가스 날개 배출각을 비교하는 도포. 제7도는 터빈 압력비의 함수로서 손실의 감소를 도시한 도표.

Claims (4)

  1. 한 열이상의 굽은 안내 날개와 한 열이상의 회전 날개를 구비한 축류 터빈에 있어서, 안내 날개의 전체 크기에 걸친 안내 날개의 굽음이 익현에 대하여 직각에서 선택되고. 상기 안내 날개가 방사상 범위내에서 점점 가늘어진 (taper) 축류터 빈.
  2. 제1항에 있어서, 안내 날개의 굽음이 원주방향에서 각각의 인접한 안내 날개의 압력측을 향하여 굽은 축류터빈.
  3. 제1항에 있어서. 상기 점감 (taper) 이 외측반경으로부터 상기 안내 날개 크기의 절반까지는 익현대 날개사이의 거리의 비가 증가하는 형태의 안내 날개를 가지고. 상기 안내 날개 크기의 절반부에서 내측 반경까지는 익현대 날게 사이의 거리 비가 일정한 형태의 안내 날개를 갖는 방식으로 선택되는 축류 터빈
  4. 제1항에 있어서, 안내 날개 선단부 지역에 원추형으로 개구된 허브부를 갖는 축류 터빈의 안내 날개가 날개 크기 전체에 걸쳐서 뒤틀린 축류 터빈.
    ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.
KR1019930012647A 1992-08-29 1993-07-06 축류 터빈 KR940005867A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4228879A DE4228879A1 (de) 1992-08-29 1992-08-29 Axialdurchströmte Turbine
DEP4228879.7 1992-08-29

Publications (1)

Publication Number Publication Date
KR940005867A true KR940005867A (ko) 1994-03-22

Family

ID=6466787

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019930012647A KR940005867A (ko) 1992-08-29 1993-07-06 축류 터빈

Country Status (10)

Country Link
US (1) US5342170A (ko)
JP (1) JPH06173605A (ko)
KR (1) KR940005867A (ko)
CN (1) CN1086579A (ko)
CH (1) CH688867A5 (ko)
CZ (1) CZ285003B6 (ko)
DE (1) DE4228879A1 (ko)
GB (1) GB2270348B (ko)
PL (1) PL299621A1 (ko)
RU (1) RU2109961C1 (ko)

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9417406D0 (en) * 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
US5525038A (en) * 1994-11-04 1996-06-11 United Technologies Corporation Rotor airfoils to control tip leakage flows
US6375419B1 (en) * 1995-06-02 2002-04-23 United Technologies Corporation Flow directing element for a turbine engine
CN1100195C (zh) 1997-09-08 2003-01-29 西门子公司 用于叶片机械的叶片和汽轮机
EP0916812B1 (de) * 1997-11-17 2003-03-05 ALSTOM (Switzerland) Ltd Endstufe für axialdurchströmte Turbine
US6077036A (en) 1998-08-20 2000-06-20 General Electric Company Bowed nozzle vane with selective TBC
EP0990770B1 (de) * 1998-09-29 2003-06-25 ALSTOM (Switzerland) Ltd Hochbelastete Turbinenbeschaufelung
JP4086415B2 (ja) * 1999-06-03 2008-05-14 株式会社荏原製作所 タービン装置
DE19950228A1 (de) * 1999-10-19 2000-11-16 Voith Hydro Gmbh & Co Kg Hydraulische Strömungsmaschine
US6312219B1 (en) 1999-11-05 2001-11-06 General Electric Company Narrow waist vane
US6331100B1 (en) 1999-12-06 2001-12-18 General Electric Company Doubled bowed compressor airfoil
US6299412B1 (en) 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil
US6328533B1 (en) 1999-12-21 2001-12-11 General Electric Company Swept barrel airfoil
JP3785013B2 (ja) * 2000-01-12 2006-06-14 三菱重工業株式会社 タービン動翼
US6508630B2 (en) 2001-03-30 2003-01-21 General Electric Company Twisted stator vane
US6554569B2 (en) 2001-08-17 2003-04-29 General Electric Company Compressor outlet guide vane and diffuser assembly
US6682301B2 (en) 2001-10-05 2004-01-27 General Electric Company Reduced shock transonic airfoil
GB2384276A (en) * 2002-01-18 2003-07-23 Alstom Gas turbine low pressure stage
CN100353031C (zh) 2003-07-09 2007-12-05 西门子公司 透平叶片
US7547186B2 (en) 2004-09-28 2009-06-16 Honeywell International Inc. Nonlinearly stacked low noise turbofan stator
DE102004054752A1 (de) * 2004-11-12 2006-05-18 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe
US7195456B2 (en) * 2004-12-21 2007-03-27 United Technologies Corporation Turbine engine guide vane and arrays thereof
DE102005021058A1 (de) * 2005-05-06 2006-11-09 Mtu Aero Engines Gmbh Gasturbine, insbesondere Flugtriebwerk
CH698109B1 (de) 2005-07-01 2009-05-29 Alstom Technology Ltd Turbomaschinenschaufel.
JP2009531593A (ja) * 2006-03-31 2009-09-03 アルストム テクノロジー リミテッド 流体機械、特に蒸気タービンの案内ブレード
US7832981B2 (en) 2006-04-28 2010-11-16 Valeo, Inc. Stator vane having both chordwise and spanwise camber
US8087884B2 (en) * 2006-11-30 2012-01-03 General Electric Company Advanced booster stator vane
US7967571B2 (en) * 2006-11-30 2011-06-28 General Electric Company Advanced booster rotor blade
US8292574B2 (en) 2006-11-30 2012-10-23 General Electric Company Advanced booster system
US7758306B2 (en) * 2006-12-22 2010-07-20 General Electric Company Turbine assembly for a gas turbine engine and method of manufacturing the same
CA2695474A1 (en) 2007-04-24 2008-10-30 Alstom Technology Ltd. Fluid flow engine
US9009965B2 (en) * 2007-05-24 2015-04-21 General Electric Company Method to center locate cutter teeth on shrouded turbine blades
US8602729B2 (en) 2007-07-27 2013-12-10 Ansaldo Energia S.P.A. Steam turbine stage
WO2009118234A1 (de) * 2008-03-28 2009-10-01 Alstom Technology Ltd Schaufel für eine rotierende thermische maschine
DE102008060847B4 (de) * 2008-12-06 2020-03-19 MTU Aero Engines AG Strömungsmaschine
RU2405622C2 (ru) * 2009-03-23 2010-12-10 Владимир Андреевич Бушуев Лопаточный реактор для пиролиза углеводородов
DE102010009615B4 (de) 2010-02-27 2016-11-17 MTU Aero Engines AG Schaufelblatt mit gefädelten Profilschnitten
FR2967202B1 (fr) * 2010-11-10 2013-01-11 Snecma Procede d'optimisation du profil d'une aube en materiau composite pour roue mobile de turbomachine
US9181814B2 (en) * 2010-11-24 2015-11-10 United Technology Corporation Turbine engine compressor stator
CN102562654A (zh) * 2012-01-03 2012-07-11 大同北方天力增压技术有限公司 一种径流式压气机叶轮叶型设计方法
US20140072433A1 (en) * 2012-09-10 2014-03-13 General Electric Company Method of clocking a turbine by reshaping the turbine's downstream airfoils
US9869191B2 (en) 2012-10-09 2018-01-16 United Technologies Corporation Geared low fan pressure ratio fan exit guide vane stagger angle
US9435221B2 (en) 2013-08-09 2016-09-06 General Electric Company Turbomachine airfoil positioning
CN103696812A (zh) * 2013-12-23 2014-04-02 中国北车集团大连机车研究所有限公司 涡轮增压器用喷嘴环
US9470093B2 (en) 2015-03-18 2016-10-18 United Technologies Corporation Turbofan arrangement with blade channel variations
PL415835A1 (pl) * 2016-01-18 2017-07-31 General Electric Company Zespół łopatki sprężarki do gazowego silnika turbinowego i sposób kontrolowania strumienia przecieku przez uszczelnienia wokół zespołu łopatki sprężarki do gazowego silnika turbinowego
DE102017209660A1 (de) * 2017-06-08 2018-12-13 MTU Aero Engines AG Strömungsmaschine mit indirekt beeinflussbarer Hochdruckturbine
US20190106989A1 (en) * 2017-10-09 2019-04-11 United Technologies Corporation Gas turbine engine airfoil
CA3115079A1 (en) 2018-11-05 2020-05-14 Ihi Corporation Rotor blade of axial-flow fluid machine
CN110630335A (zh) * 2019-09-06 2019-12-31 北京市燃气集团有限责任公司 气体膨胀装置
CN114483204B (zh) * 2021-12-29 2023-07-14 东方电气集团东方汽轮机有限公司 一种适用于径轴向直立非垂直进气的静叶

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2110679A (en) * 1936-04-22 1938-03-08 Gen Electric Elastic fluid turbine
GB619690A (en) * 1946-07-03 1949-03-14 Robert William Corbitt Improvements in or relating to blades and guide-blades for turbines, rotary compressors and the like
GB712589A (en) * 1950-03-03 1954-07-28 Rolls Royce Improvements in or relating to guide vane assemblies in annular fluid ducts
US2795373A (en) * 1950-03-03 1957-06-11 Rolls Royce Guide vane assemblies in annular fluid ducts
GB1116580A (en) * 1965-11-17 1968-06-06 Bristol Siddeley Engines Ltd Stator blade assemblies for axial-flow turbine engines
US4131387A (en) * 1976-02-27 1978-12-26 General Electric Company Curved blade turbomachinery noise reduction
JPS5447907A (en) * 1977-09-26 1979-04-16 Hitachi Ltd Blading structure for axial-flow fluid machine
FR2505399A1 (fr) * 1981-05-05 1982-11-12 Alsthom Atlantique Aubage directeur pour veines divergentes de turbine a vapeur
GB2129882B (en) * 1982-11-10 1986-04-16 Rolls Royce Gas turbine stator vane
US4682935A (en) * 1983-12-12 1987-07-28 General Electric Company Bowed turbine blade
US4585395A (en) * 1983-12-12 1986-04-29 General Electric Company Gas turbine engine blade
GB2164098B (en) * 1984-09-07 1988-12-07 Rolls Royce Improvements in or relating to aerofoil section members for turbine engines
GB2177163B (en) * 1985-06-28 1988-12-07 Rolls Royce Improvements in or relating to aerofoil section members for gas turbine engines
US4741667A (en) * 1986-05-28 1988-05-03 United Technologies Corporation Stator vane
US4826400A (en) * 1986-12-29 1989-05-02 General Electric Company Curvilinear turbine airfoil
US5088892A (en) * 1990-02-07 1992-02-18 United Technologies Corporation Bowed airfoil for the compression section of a rotary machine
JPH03267506A (ja) * 1990-03-19 1991-11-28 Hitachi Ltd 軸流タービンの静翼
JPH0454203A (ja) * 1990-06-22 1992-02-21 Toshiba Corp タービン動翼およびタービン段落
JP2753382B2 (ja) * 1990-09-17 1998-05-20 株式会社日立製作所 軸流タービン静翼装置及び軸流タービン

Also Published As

Publication number Publication date
US5342170A (en) 1994-08-30
JPH06173605A (ja) 1994-06-21
GB2270348B (en) 1996-10-30
GB9314613D0 (en) 1993-08-25
CZ285003B6 (cs) 1999-04-14
DE4228879A1 (de) 1994-03-03
CH688867A5 (de) 1998-04-30
CN1086579A (zh) 1994-05-11
PL299621A1 (en) 1994-03-07
GB2270348A (en) 1994-03-09
CZ170593A3 (en) 1994-08-17
RU2109961C1 (ru) 1998-04-27

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