KR100673407B1 - 가스 터빈 내의 축류 압축기와 고압 로터 디스크 유닛 사이의 연결을 위한 개선된 플랜지 - Google Patents

가스 터빈 내의 축류 압축기와 고압 로터 디스크 유닛 사이의 연결을 위한 개선된 플랜지 Download PDF

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KR100673407B1
KR100673407B1 KR1020020057040A KR20020057040A KR100673407B1 KR 100673407 B1 KR100673407 B1 KR 100673407B1 KR 1020020057040 A KR1020020057040 A KR 1020020057040A KR 20020057040 A KR20020057040 A KR 20020057040A KR 100673407 B1 KR100673407 B1 KR 100673407B1
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South Korea
Prior art keywords
rotor disk
disk unit
connection
axial compressor
flange
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Expired - Fee Related
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KR1020020057040A
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English (en)
Korean (ko)
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KR20030025849A (ko
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핀자우티마시모
바시오티니카를로
Original Assignee
누보 피그노네 홀딩 에스피에이
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Publication of KR20030025849A publication Critical patent/KR20030025849A/ko
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    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • 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
    • F01D25/243—Flange connections; Bolting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/076—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end by clamping together two faces perpendicular to the axis of rotation, e.g. with bolted flanges

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR1020020057040A 2001-09-20 2002-09-18 가스 터빈 내의 축류 압축기와 고압 로터 디스크 유닛 사이의 연결을 위한 개선된 플랜지 Expired - Fee Related KR100673407B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT2001MI001961A ITMI20011961A1 (it) 2001-09-20 2001-09-20 Flangia migliorata di accoppiamento tra compressore assiale e gruppo di dischi rotorici di alta pressione in una turbina a gas
ITMI2001A001961 2001-09-20

Publications (2)

Publication Number Publication Date
KR20030025849A KR20030025849A (ko) 2003-03-29
KR100673407B1 true KR100673407B1 (ko) 2007-01-23

Family

ID=11448401

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020020057040A Expired - Fee Related KR100673407B1 (ko) 2001-09-20 2002-09-18 가스 터빈 내의 축류 압축기와 고압 로터 디스크 유닛 사이의 연결을 위한 개선된 플랜지

Country Status (9)

Country Link
US (1) US6672630B2 (enExample)
EP (1) EP1296021B1 (enExample)
JP (1) JP4169556B2 (enExample)
KR (1) KR100673407B1 (enExample)
CA (1) CA2404187C (enExample)
DE (1) DE60217038T2 (enExample)
IT (1) ITMI20011961A1 (enExample)
RU (1) RU2300670C2 (enExample)
TW (1) TW552348B (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITMI20011961A1 (it) * 2001-09-20 2003-03-20 Nuovo Pignone Spa Flangia migliorata di accoppiamento tra compressore assiale e gruppo di dischi rotorici di alta pressione in una turbina a gas
RU2324056C2 (ru) * 2006-04-10 2008-05-10 Открытое Акционерное Общество "Теплоэнергосервис-ЭК" (ОАО "Теплоэнергосервис-ЭК") Ротор турбомашины
RU2352788C1 (ru) * 2007-07-25 2009-04-20 Открытое акционерное общество "Авиадвигатель" Высокотемпературная газовая турбина
US8459943B2 (en) * 2010-03-10 2013-06-11 United Technologies Corporation Gas turbine engine rotor sections held together by tie shaft, and with blade rim undercut
US9200520B2 (en) 2012-06-22 2015-12-01 General Electric Company Gas turbine conical flange bolted joint
US20140064976A1 (en) * 2012-08-14 2014-03-06 Kevin L. Corcoran Rotor keyhole fillet for a gas turbine engine
US9279325B2 (en) * 2012-11-08 2016-03-08 General Electric Company Turbomachine wheel assembly having slotted flanges
EP3693543A1 (en) 2013-04-18 2020-08-12 United Technologies Corporation Turbine minidisk bumper for gas turbine engine
CN104074551B (zh) * 2014-06-19 2015-09-23 中国北方发动机研究所(天津) 一种涡轮叶轮分体式结构
CN105402157B (zh) * 2015-12-25 2018-06-05 中国航空工业集团公司沈阳发动机设计研究所 一种整体式盘轴结构
US10343765B2 (en) * 2016-06-02 2019-07-09 United Technologies Corporation Toroidal spinner aft flange
CN107654768A (zh) * 2017-11-02 2018-02-02 张家港市三林金泰新能源有限公司 新型能源内燃机法兰

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2804323A (en) * 1954-08-19 1957-08-27 Rolls Royce Axial-flow compressors and turbines
US3688371A (en) * 1970-04-30 1972-09-05 Gen Electric The method of manufacturing compositely formed rotors
US4167097A (en) * 1977-09-09 1979-09-11 International Harvester Company Gas turbine engines with improved compressor-combustor interfaces
US4184797A (en) * 1977-10-17 1980-01-22 General Electric Company Liquid-cooled turbine rotor
US5054996A (en) * 1990-07-27 1991-10-08 General Electric Company Thermal linear actuator for rotor air flow control in a gas turbine
US5218816A (en) * 1992-01-28 1993-06-15 General Electric Company Seal exit flow discourager
EP1296021A2 (en) * 2001-09-20 2003-03-26 Nuovo Pignone Holding S.P.A. Flange connection between compressor shaft and turbine rotor disc

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1977911A (en) * 1933-10-04 1934-10-23 Universal Pipe And Radiator Co Pipe joint
US4074914A (en) * 1975-07-28 1978-02-21 United Technologies Corporation High pressure lightweight flanges
US4183562A (en) * 1977-04-01 1980-01-15 Regan Offshore International, Inc. Marine riser conduit section coupling means
US4310286A (en) * 1979-05-17 1982-01-12 United Technologies Corporation Rotor assembly having a multistage disk
DE3738929A1 (de) * 1987-11-17 1989-05-24 Leybold Ag Geblaese mit laufrad und leitelement
RU2098670C1 (ru) * 1995-06-26 1997-12-10 Акционерное общество "Авиадвигатель" Устройство для регулирования положения поворотных направляющих лопаток компрессора или турбины газотурбинного двигателя
DE19605971C2 (de) * 1996-02-17 1998-09-17 Mtu Muenchen Gmbh Lageranordnung für Drehkörper
US5702131A (en) * 1996-03-01 1997-12-30 Wagner Spray Tech Corporation Outlet fitting for a portable turbine
RU2109176C1 (ru) * 1996-07-01 1998-04-20 Акционерное общество открытого типа "Уральский завод гражданской авиации" Способ ремонта направляющего аппарата компрессора газотурбинного двигателя
EP0840016B1 (de) * 1996-10-29 2003-02-05 Siemens Aktiengesellschaft Turbomaschine, insbesondere Verdichter in Topfbauweise
US5833435A (en) * 1996-12-24 1998-11-10 United Technologies Corporation Inlet nose cone assembly and method for repairing the assembly
US5746574A (en) * 1997-05-27 1998-05-05 General Electric Company Low profile fluid joint
US5967566A (en) * 1998-01-06 1999-10-19 Schlicht; Gunter Light-weight, slip-on pipe flange
US6077035A (en) * 1998-03-27 2000-06-20 Pratt & Whitney Canada Corp. Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine
DE19828817C2 (de) * 1998-06-27 2000-07-13 Mtu Muenchen Gmbh Rotor für eine Turbomaschine
US6546732B1 (en) * 2001-04-27 2003-04-15 General Electric Company Methods and apparatus for cooling gas turbine engine combustors

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2804323A (en) * 1954-08-19 1957-08-27 Rolls Royce Axial-flow compressors and turbines
US3688371A (en) * 1970-04-30 1972-09-05 Gen Electric The method of manufacturing compositely formed rotors
US4167097A (en) * 1977-09-09 1979-09-11 International Harvester Company Gas turbine engines with improved compressor-combustor interfaces
US4184797A (en) * 1977-10-17 1980-01-22 General Electric Company Liquid-cooled turbine rotor
US5054996A (en) * 1990-07-27 1991-10-08 General Electric Company Thermal linear actuator for rotor air flow control in a gas turbine
US5218816A (en) * 1992-01-28 1993-06-15 General Electric Company Seal exit flow discourager
EP1296021A2 (en) * 2001-09-20 2003-03-26 Nuovo Pignone Holding S.P.A. Flange connection between compressor shaft and turbine rotor disc
JP2003176701A (ja) * 2001-09-20 2003-06-27 Nuovo Pignone Holding Spa ガスタービンの軸流圧縮機と高圧側ロータディスク装置との間を接続するための改良フランジ
US6672630B2 (en) * 2001-09-20 2004-01-06 Nuovo Pignone Holding S.P.A. Flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine

Also Published As

Publication number Publication date
ITMI20011961A0 (it) 2001-09-20
DE60217038T2 (de) 2007-07-12
DE60217038D1 (de) 2007-02-08
CA2404187C (en) 2009-01-13
TW552348B (en) 2003-09-11
ITMI20011961A1 (it) 2003-03-20
CA2404187A1 (en) 2003-03-20
US6672630B2 (en) 2004-01-06
EP1296021A2 (en) 2003-03-26
RU2300670C2 (ru) 2007-06-10
EP1296021A3 (en) 2004-12-15
JP4169556B2 (ja) 2008-10-22
JP2003176701A (ja) 2003-06-27
US20030057702A1 (en) 2003-03-27
EP1296021B1 (en) 2006-12-27
KR20030025849A (ko) 2003-03-29

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