RU2013113929A - Герметичная изоляция соединения - Google Patents

Герметичная изоляция соединения Download PDF

Info

Publication number
RU2013113929A
RU2013113929A RU2013113929/06A RU2013113929A RU2013113929A RU 2013113929 A RU2013113929 A RU 2013113929A RU 2013113929/06 A RU2013113929/06 A RU 2013113929/06A RU 2013113929 A RU2013113929 A RU 2013113929A RU 2013113929 A RU2013113929 A RU 2013113929A
Authority
RU
Russia
Prior art keywords
turbine
blade
insulating element
tail
working blade
Prior art date
Application number
RU2013113929/06A
Other languages
English (en)
Russian (ru)
Inventor
Мэттью Роберт ПИЕРСЭЛЛ
Брайан Денвер ПОТТЕР
Original Assignee
Дженерал Электрик Компани
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 Дженерал Электрик Компани filed Critical Дженерал Электрик Компани
Publication of RU2013113929A publication Critical patent/RU2013113929A/ru

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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/10—Manufacture by removing material
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
RU2013113929/06A 2012-03-29 2013-03-28 Герметичная изоляция соединения RU2013113929A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/433,969 2012-03-29
US13/433,969 US9151169B2 (en) 2012-03-29 2012-03-29 Near-flow-path seal isolation dovetail

Publications (1)

Publication Number Publication Date
RU2013113929A true RU2013113929A (ru) 2014-10-10

Family

ID=48095547

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013113929/06A RU2013113929A (ru) 2012-03-29 2013-03-28 Герметичная изоляция соединения

Country Status (5)

Country Link
US (1) US9151169B2 (enExample)
EP (1) EP2644832B1 (enExample)
JP (1) JP6186150B2 (enExample)
CN (1) CN103362561B (enExample)
RU (1) RU2013113929A (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9328622B2 (en) * 2012-06-12 2016-05-03 General Electric Company Blade attachment assembly
CN104153824B (zh) * 2014-07-25 2016-05-04 江苏金通灵流体机械科技股份有限公司 透平多级气封结构
US10662793B2 (en) 2014-12-01 2020-05-26 General Electric Company Turbine wheel cover-plate mounted gas turbine interstage seal
US10337345B2 (en) 2015-02-20 2019-07-02 General Electric Company Bucket mounted multi-stage turbine interstage seal and method of assembly
US10683765B2 (en) * 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
IT202000004585A1 (it) * 2020-03-04 2021-09-04 Nuovo Pignone Tecnologie Srl Turbina e pala perfezionate per la protezione della radice dai gas caldi del percorso del flusso.
US11333026B2 (en) * 2020-05-26 2022-05-17 General Electric Company Vibration-damping system for turbomachine blade(s) on spacer adjacent blade stage

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL295165A (enExample) * 1962-07-11
US5318406A (en) * 1992-11-02 1994-06-07 General Electric Company Multipart gas turbine blade
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
US6652237B2 (en) 2001-10-15 2003-11-25 General Electric Company Bucket and wheel dovetail design for turbine rotors
US6884028B2 (en) * 2002-09-30 2005-04-26 General Electric Company Turbomachinery blade retention system
US6984112B2 (en) 2003-10-31 2006-01-10 General Electric Company Methods and apparatus for cooling gas turbine rotor blades
WO2006124619A2 (en) 2005-05-12 2006-11-23 General Electric Company BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (7FA+e, STAGE 2)
US7922455B2 (en) 2005-09-19 2011-04-12 General Electric Company Steam-cooled gas turbine bucker for reduced tip leakage loss
US7736131B1 (en) * 2008-07-21 2010-06-15 Florida Turbine Technologies, Inc. Turbine blade with carbon nanotube shell
US8137072B2 (en) 2008-10-31 2012-03-20 Solar Turbines Inc. Turbine blade including a seal pocket
US8714932B2 (en) * 2008-12-31 2014-05-06 General Electric Company Ceramic matrix composite blade having integral platform structures and methods of fabrication
US8221062B2 (en) * 2009-01-14 2012-07-17 General Electric Company Device and system for reducing secondary air flow in a gas turbine
US8696320B2 (en) * 2009-03-12 2014-04-15 General Electric Company Gas turbine having seal assembly with coverplate and seal
US8348603B2 (en) * 2009-04-02 2013-01-08 General Electric Company Gas turbine inner flowpath coverpiece
US20120045337A1 (en) 2010-08-20 2012-02-23 Michael James Fedor Turbine bucket assembly and methods for assembling same

Also Published As

Publication number Publication date
EP2644832A1 (en) 2013-10-02
CN103362561A (zh) 2013-10-23
EP2644832B1 (en) 2016-03-23
US20130259700A1 (en) 2013-10-03
US9151169B2 (en) 2015-10-06
JP2013204595A (ja) 2013-10-07
CN103362561B (zh) 2016-08-31
JP6186150B2 (ja) 2017-08-23

Similar Documents

Publication Publication Date Title
JP2015528540A5 (enExample)
WO2014105701A3 (en) Non-integral fan blade platform
BRPI0818386A2 (pt) Montagem de pá de turbina e tira de vedação
WO2014171990A3 (en) Turbine assembly and system for preventing leakage, corresponding methods of assembling and preventing air leakage
US9951625B2 (en) Turbine wheel for a turbine engine
RU2014123694A (ru) Крыльчатка для турбомашины
EP2620599A3 (en) Turbomachine with an angled abradable interstage seal and corresponding method of reducing a seal gap
EP4350125A3 (en) Non-contact seal assembly for a gas turbine engine
RU2012108735A (ru) Вибрационно-демпфирующая прокладка для лопасти вентилятора
WO2014108231A3 (de) Radnaben-motor und verfahren zum abdichten eines radnaben-motors
JP2013204595A5 (enExample)
CN103362561B (zh) 流路附近密封件隔离鸠尾榫
BR112014029523A8 (pt) Pá de ventilador para turborreator de avião, ventilador de turborreator de avião, e, turborreator de avião
BR112016028799A2 (pt) conjunto de disco do rotor, sistema de geração de potência e método de fabricação de um conjunto de disco do rotor
KR20110102908A (ko) 블레이드를 축 방향으로 지지하기 위한 시스템을 갖춘 터빈휠
CN104329123A (zh) 新型涡轮机动叶与轮盘固定结构
RU2014149236A (ru) Лопатка ротора турбины и осевой участок ротора для газовой турбины
BR112015028949A8 (pt) montagem de turbomáquina e método para montagem de turbomáquina
WO2015009821A3 (en) Improved disc brake rotor for heavy-duty vehicles
BR112017012593A2 (pt) conjunto de turbina de turbomáquina de aeronave
EP2208859A3 (en) Steam turbine and cooling method thereof
WO2015000862A3 (de) Rotor für einen nockenwellenversteller mit verbesserter geometrie
US20140127027A1 (en) Turbine rotor for a thermal electric power station
RU2013125740A (ru) Турбинный лопаточный узел для паровой турбины (варианты) и паровая турбина
KR102270498B1 (ko) 터보기계 로터 및 그 제조 방법

Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20180111