JPS5727291B2 - - Google Patents

Info

Publication number
JPS5727291B2
JPS5727291B2 JP14256573A JP14256573A JPS5727291B2 JP S5727291 B2 JPS5727291 B2 JP S5727291B2 JP 14256573 A JP14256573 A JP 14256573A JP 14256573 A JP14256573 A JP 14256573A JP S5727291 B2 JPS5727291 B2 JP S5727291B2
Authority
JP
Japan
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.)
Expired
Application number
JP14256573A
Other languages
Japanese (ja)
Other versions
JPS4996113A (US07696358-20100413-C00002.png
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 filed Critical
Publication of JPS4996113A publication Critical patent/JPS4996113A/ja
Publication of JPS5727291B2 publication Critical patent/JPS5727291B2/ja
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20Mounting or supporting of plant; Accommodating heat expansion or creep
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49231I.C. [internal combustion] engine making
    • Y10T29/49234Rotary or radial engine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP14256573A 1972-12-26 1973-12-21 Expired JPS5727291B2 (US07696358-20100413-C00002.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00318179A US3842595A (en) 1972-12-26 1972-12-26 Modular gas turbine engine

Publications (2)

Publication Number Publication Date
JPS4996113A JPS4996113A (US07696358-20100413-C00002.png) 1974-09-11
JPS5727291B2 true JPS5727291B2 (US07696358-20100413-C00002.png) 1982-06-09

Family

ID=23237015

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14256573A Expired JPS5727291B2 (US07696358-20100413-C00002.png) 1972-12-26 1973-12-21

Country Status (8)

Country Link
US (1) US3842595A (US07696358-20100413-C00002.png)
JP (1) JPS5727291B2 (US07696358-20100413-C00002.png)
BE (1) BE809055A (US07696358-20100413-C00002.png)
CA (1) CA986730A (US07696358-20100413-C00002.png)
DE (1) DE2364430C2 (US07696358-20100413-C00002.png)
FR (1) FR2211591B1 (US07696358-20100413-C00002.png)
GB (1) GB1453304A (US07696358-20100413-C00002.png)
IT (1) IT1002234B (US07696358-20100413-C00002.png)

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JPS5060883A (US07696358-20100413-C00002.png) * 1973-10-01 1975-05-26
FR2288868A1 (fr) * 1973-12-03 1976-05-21 Snecma Canal d'ejection de turboreacteur et reacteur pourvu d'un tel canal
US4011718A (en) * 1975-08-01 1977-03-15 United Technologies Corporation Gas turbine construction
US4021138A (en) * 1975-11-03 1977-05-03 Westinghouse Electric Corporation Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
US4030288A (en) * 1975-11-10 1977-06-21 Caterpillar Tractor Co. Modular gas turbine engine assembly
US4083180A (en) * 1976-10-01 1978-04-11 Caterpillar Tractor Co. Gas turbine engine internal insulation
US4141212A (en) * 1977-06-20 1979-02-27 Avco Corporation Differentially geared regenerative reverse flow turbo shaft engine
IT1138763B (it) * 1981-05-04 1986-09-17 Nuovo Pignone Spa Perfezionamenti in una turbina a gas di potenza
FR2544387B1 (fr) * 1983-04-15 1985-06-14 Snecma Appareillage pour le transfert d'un module de turbine complet d'une machine d'equilibrage a un moteur et vice versa, et procede pour la mise en oeuvre dudit appareillage
US4573866A (en) * 1983-05-02 1986-03-04 United Technologies Corporation Sealed shroud for rotating body
DE3333436C1 (de) * 1983-09-16 1985-02-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Axial- und Umfangssicherung von statischen Gehaeusebauteilen fuer Stroemungsmaschinen
US4611464A (en) * 1984-05-02 1986-09-16 United Technologies Corporation Rotor assembly for a gas turbine engine and method of disassembly
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly
US4645424A (en) * 1984-07-23 1987-02-24 United Technologies Corporation Rotating seal for gas turbine engine
US4640092A (en) * 1986-03-03 1987-02-03 United Technologies Corporation Combustion chamber rear outer seal
US4744214A (en) * 1987-06-29 1988-05-17 United Technologies Corporation Engine modularity
US4785623A (en) * 1987-12-09 1988-11-22 United Technologies Corporation Combustor seal and support
FR2648182B1 (fr) * 1989-06-07 1991-08-30 Snecma Systeme de verrouillage provisoire de positionnement d'aubes a calage variable pendant le montage et turbomachine le comportant
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
US5224341A (en) * 1992-01-06 1993-07-06 United Technologies Corporation Separable fan strut for a gas turbofan powerplant
US5222360A (en) * 1991-10-30 1993-06-29 General Electric Company Apparatus for removably attaching a core frame to a vane frame with a stable mid ring
US5226788A (en) * 1991-12-23 1993-07-13 General Electric Company Turbine heat shield and bolt retainer assembly
US5211541A (en) * 1991-12-23 1993-05-18 General Electric Company Turbine support assembly including turbine heat shield and bolt retainer assembly
US5291732A (en) * 1993-02-08 1994-03-08 General Electric Company Combustor liner support assembly
US5333995A (en) * 1993-08-09 1994-08-02 General Electric Company Wear shim for a turbine engine
US5924288A (en) * 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
JP2877296B2 (ja) * 1995-09-11 1999-03-31 三菱重工業株式会社 ガスタービン燃焼器の取付、取外し装置
WO1997014529A1 (fr) * 1995-10-19 1997-04-24 Mitsubishi Jukogyo Kabushiki Kaisha Appareil a remplacer les bruleurs
US6691519B2 (en) * 2000-02-18 2004-02-17 Siemens Westinghouse Power Corporation Adaptable modular gas turbine power plant
DE10016082A1 (de) * 2000-03-31 2001-10-04 Alstom Power Nv Turbinengehäuse für eine axial durchströmte Gasturbine
US6428270B1 (en) * 2000-09-15 2002-08-06 General Electric Company Stage 3 bucket shank bypass holes and related method
US6464453B2 (en) * 2000-12-04 2002-10-15 General Electric Company Turbine interstage sealing ring
US6986201B2 (en) * 2002-12-04 2006-01-17 General Electric Company Methods for replacing combustor liners
US6904676B2 (en) * 2002-12-04 2005-06-14 General Electric Company Methods for replacing a portion of a combustor liner
US6893217B2 (en) * 2002-12-20 2005-05-17 General Electric Company Methods and apparatus for assembling gas turbine nozzles
DE10319015B4 (de) * 2003-04-27 2006-04-13 Mtu Aero Engines Gmbh Verfahren zur Wartung von Gasturbinen
US6899520B2 (en) * 2003-09-02 2005-05-31 General Electric Company Methods and apparatus to reduce seal rubbing within gas turbine engines
US6868675B1 (en) * 2004-01-09 2005-03-22 Honeywell International Inc. Apparatus and method for controlling combustor liner carbon formation
FR2913050B1 (fr) * 2007-02-28 2011-06-17 Snecma Turbine haute-pression d'une turbomachine
CN101946072B (zh) * 2008-02-28 2014-04-02 三菱重工业株式会社 燃气轮机及燃气轮机的机室开放方法
GB0920371D0 (en) * 2009-11-23 2010-01-06 Rolls Royce Plc Combustor system
US9410441B2 (en) * 2012-09-13 2016-08-09 Pratt & Whitney Canada Corp. Turboprop engine with compressor turbine shroud
US9771818B2 (en) 2012-12-29 2017-09-26 United Technologies Corporation Seals for a circumferential stop ring in a turbine exhaust case
US9624829B2 (en) 2013-03-05 2017-04-18 Industrial Turbine Company (Uk) Limited Cogen heat load matching through reheat and capacity match
US10036317B2 (en) 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
CN103511001B (zh) * 2013-07-11 2015-04-22 哈尔滨汽轮机厂有限责任公司 一种用于重型中低热值燃机的涡轮首级导叶
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
JP6271077B2 (ja) 2014-07-24 2018-01-31 シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft ガスタービンエンジン内で使用可能なステータベーンシステム
EP3088691B1 (en) * 2015-04-27 2019-06-19 Ansaldo Energia Switzerland AG Gas turbine disassembly method
US10823013B2 (en) * 2016-09-30 2020-11-03 General Electric Company Dual tierod assembly for a gas turbine engine and method of assembly thereof
US11111858B2 (en) 2017-01-27 2021-09-07 General Electric Company Cool core gas turbine engine
US10393381B2 (en) 2017-01-27 2019-08-27 General Electric Company Unitary flow path structure
US10371383B2 (en) 2017-01-27 2019-08-06 General Electric Company Unitary flow path structure
US10378770B2 (en) 2017-01-27 2019-08-13 General Electric Company Unitary flow path structure
US10816199B2 (en) 2017-01-27 2020-10-27 General Electric Company Combustor heat shield and attachment features
US10253643B2 (en) 2017-02-07 2019-04-09 General Electric Company Airfoil fluid curtain to mitigate or prevent flow path leakage
US10247019B2 (en) 2017-02-23 2019-04-02 General Electric Company Methods and features for positioning a flow path inner boundary within a flow path assembly
US10378373B2 (en) 2017-02-23 2019-08-13 General Electric Company Flow path assembly with airfoils inserted through flow path boundary
US10385776B2 (en) 2017-02-23 2019-08-20 General Electric Company Methods for assembling a unitary flow path structure
US10385709B2 (en) 2017-02-23 2019-08-20 General Electric Company Methods and features for positioning a flow path assembly within a gas turbine engine
US10370990B2 (en) 2017-02-23 2019-08-06 General Electric Company Flow path assembly with pin supported nozzle airfoils
US10253641B2 (en) 2017-02-23 2019-04-09 General Electric Company Methods and assemblies for attaching airfoils within a flow path
US10385731B2 (en) 2017-06-12 2019-08-20 General Electric Company CTE matching hanger support for CMC structures
US10961850B2 (en) * 2017-09-19 2021-03-30 General Electric Company Rotatable torque frame for gas turbine engine
US11402097B2 (en) 2018-01-03 2022-08-02 General Electric Company Combustor assembly for a turbine engine
US10598046B2 (en) 2018-07-11 2020-03-24 United Technologies Corporation Support straps and method of assembly for gas turbine engine
GB201817936D0 (en) * 2018-11-02 2018-12-19 Rolls Royce Plc Method of upgrading a modular gas turbine engine
CN109404049B (zh) * 2018-12-28 2024-04-09 中国船舶重工集团公司第七0三研究所 一种可快速拆装的氦气涡轮连接结构
GB201917397D0 (en) 2019-11-29 2020-01-15 Siemens Ag Method of assembling and disassembling a gas turbine engine module and an assembly therefor
US11268394B2 (en) 2020-03-13 2022-03-08 General Electric Company Nozzle assembly with alternating inserted vanes for a turbine engine
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067983A (en) * 1958-07-01 1962-12-11 Gen Motors Corp Turbine mounting construction
US3321179A (en) * 1965-09-13 1967-05-23 Caterpillar Tractor Co Gas turbine engines
US3365173A (en) * 1966-02-28 1968-01-23 Gen Electric Stator structure
DE1918858C3 (de) * 1969-04-14 1975-02-20 Konstantin Iwanowitsch Schdanow Gasturbinenanlage
US3602605A (en) * 1969-09-29 1971-08-31 Westinghouse Electric Corp Cooling system for a gas turbine

Also Published As

Publication number Publication date
GB1453304A (en) 1976-10-20
FR2211591A1 (US07696358-20100413-C00002.png) 1974-07-19
DE2364430A1 (de) 1974-06-27
BE809055A (fr) 1974-04-16
CA986730A (en) 1976-04-06
US3842595A (en) 1974-10-22
FR2211591B1 (US07696358-20100413-C00002.png) 1981-04-17
IT1002234B (it) 1976-05-20
DE2364430C2 (de) 1982-12-30
JPS4996113A (US07696358-20100413-C00002.png) 1974-09-11

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