TW552348B - Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine - Google Patents

Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine Download PDF

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Publication number
TW552348B
TW552348B TW091121604A TW91121604A TW552348B TW 552348 B TW552348 B TW 552348B TW 091121604 A TW091121604 A TW 091121604A TW 91121604 A TW91121604 A TW 91121604A TW 552348 B TW552348 B TW 552348B
Authority
TW
Taiwan
Prior art keywords
flange
extension
scope
ratio
axis
Prior art date
Application number
TW091121604A
Other languages
English (en)
Chinese (zh)
Inventor
Massimo Pinzauti
Carlo Bacciottini
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Application granted granted Critical
Publication of TW552348B publication Critical patent/TW552348B/zh

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
TW091121604A 2001-09-20 2002-09-20 Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine TW552348B (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
TW552348B true TW552348B (en) 2003-09-11

Family

ID=11448401

Family Applications (1)

Application Number Title Priority Date Filing Date
TW091121604A TW552348B (en) 2001-09-20 2002-09-20 Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine

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
US10221761B2 (en) 2013-04-18 2019-03-05 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

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US1977911A (en) * 1933-10-04 1934-10-23 Universal Pipe And Radiator Co Pipe joint
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
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
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
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
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
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
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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

Also Published As

Publication number Publication date
EP1296021B1 (en) 2006-12-27
US20030057702A1 (en) 2003-03-27
DE60217038T2 (de) 2007-07-12
JP2003176701A (ja) 2003-06-27
EP1296021A3 (en) 2004-12-15
RU2300670C2 (ru) 2007-06-10
ITMI20011961A1 (it) 2003-03-20
CA2404187A1 (en) 2003-03-20
CA2404187C (en) 2009-01-13
EP1296021A2 (en) 2003-03-26
KR20030025849A (ko) 2003-03-29
KR100673407B1 (ko) 2007-01-23
DE60217038D1 (de) 2007-02-08
ITMI20011961A0 (it) 2001-09-20
JP4169556B2 (ja) 2008-10-22
US6672630B2 (en) 2004-01-06

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GD4A Issue of patent certificate for granted invention patent
MM4A Annulment or lapse of patent due to non-payment of fees