JP2002168196A5 - - Google Patents

Download PDF

Info

Publication number
JP2002168196A5
JP2002168196A5 JP2001343960A JP2001343960A JP2002168196A5 JP 2002168196 A5 JP2002168196 A5 JP 2002168196A5 JP 2001343960 A JP2001343960 A JP 2001343960A JP 2001343960 A JP2001343960 A JP 2001343960A JP 2002168196 A5 JP2002168196 A5 JP 2002168196A5
Authority
JP
Japan
Prior art keywords
shroud
flange
arcuate
bushing
vane
Prior art date
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.)
Withdrawn
Application number
JP2001343960A
Other languages
English (en)
Japanese (ja)
Other versions
JP2002168196A (ja
Filing date
Publication date
Application filed filed Critical
Publication of JP2002168196A publication Critical patent/JP2002168196A/ja
Publication of JP2002168196A5 publication Critical patent/JP2002168196A5/ja
Withdrawn legal-status Critical Current

Links

JP2001343960A 2000-11-09 2001-11-09 保持装置 Withdrawn JP2002168196A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US71065700A 2000-11-09 2000-11-09
US09/710657 2000-11-09

Publications (2)

Publication Number Publication Date
JP2002168196A JP2002168196A (ja) 2002-06-14
JP2002168196A5 true JP2002168196A5 (enExample) 2005-05-19

Family

ID=24854983

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001343960A Withdrawn JP2002168196A (ja) 2000-11-09 2001-11-09 保持装置

Country Status (2)

Country Link
EP (1) EP1205639A1 (enExample)
JP (1) JP2002168196A (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7125222B2 (en) * 2004-04-14 2006-10-24 General Electric Company Gas turbine engine variable vane assembly
US8038388B2 (en) 2007-03-05 2011-10-18 United Technologies Corporation Abradable component for a gas turbine engine
EP2405104A1 (de) * 2010-07-08 2012-01-11 Siemens Aktiengesellschaft Verdichter und zugehöriges Gasturbinenkraftwerk
EP2787177B1 (de) * 2013-04-02 2017-01-18 MTU Aero Engines AG Axiale Strömungsmaschine und Montageverfahren
WO2015031058A1 (en) * 2013-08-28 2015-03-05 United Technologies Corporation Variable vane bushing
FR3053383B1 (fr) * 2016-07-04 2019-08-02 Safran Aircraft Engines Clinquant de retention de douilles d'anneaux de commande d'aubes a calage variable et turboreacteur l'incorporant
DE102021129534A1 (de) * 2021-11-12 2023-05-17 MTU Aero Engines AG Leitschaufelanordnung einer Strömungsmaschine und Verfahren zur Montage einer Leitschaufelanordnung
US11739646B1 (en) * 2022-03-31 2023-08-29 General Electric Company Pre-sintered preform ball for ball-chute with hollow member therein for internal cooling of turbine component
US12228047B2 (en) 2022-03-31 2025-02-18 Ge Infrastructure Technology Llc Pre-sintered preform sealing device with hollow member therein for metering flow through passage of turbomachine component

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2524934B1 (fr) * 1982-04-08 1986-12-26 Snecma Dispositif de butee de securite pour pivot d'aubes de stator a calage variable
FR2723614B1 (fr) * 1994-08-10 1996-09-13 Snecma Dispositif d'assemblage d'un etage circulaire d'aubes pivotantes.
FR2775731B1 (fr) * 1998-03-05 2000-04-07 Snecma Etage circulaire d'aubes aux extremites interieures unies par un anneau de liaison
US6092984A (en) * 1998-12-18 2000-07-25 General Electric Company System life for continuously operating engines
US6086327A (en) * 1999-01-20 2000-07-11 Mack Plastics Corporation Bushing for a jet engine vane

Similar Documents

Publication Publication Date Title
JP6063738B2 (ja) タービンの回転セグメントを軸方向に保持するためのシステム
KR100669487B1 (ko) 가변 형상 터보차져
CA2625591C (en) Blade retention system for use in a gas turbine engine
JP2002202099A5 (enExample)
JP2002161702A5 (enExample)
CN102444437B (zh) 用于对齐涡轮机壳体的装置
JP3352690B2 (ja) プラットホームを有するロータブレードサポートおよびダンパの位置決め手段
JP2012021526A (ja) タービン回転ブレード及びロータホイール用のダブテールコネクタ
JP2009228664A (ja) ターボ型圧縮機のストラット構造
JP2013221513A (ja) タービンブレードのブレード取り付け領域をカバーするためのシステムおよび方法
CN107044346A (zh) 高负载事件期间的轴承外座圈固位
US6971852B2 (en) Method of and structure for enabling cooling of the engaging firtree features of a turbine disk and associated blades
US20150071768A1 (en) Variable pitch rectifier for a turbomachine compressor comprising two inner rings
EP1775428A3 (en) Fan stator
JP2002168196A5 (enExample)
JP5484942B2 (ja) 懸垂線状タービン・シール・システム
JP2006144784A5 (enExample)
US20070122270A1 (en) Turbomachine, especially a gas turbine
JP2002054459A5 (enExample)
CN107131005A (zh) 涡轮发动机护罩组件
JP2017101669A (ja) タービンディスク及びタービンディスクの製造方法
CN109416000A (zh) 涡轮发动机及组装方法
JP6118182B2 (ja) マルチピースロッキングブレードを備えるタービンロータ・ブレード組立体
CN106930975A (zh) 用于在涡扇发动机中使用的转子组件和组装的方法
JP2013253597A (ja) 止まり孔を備えるタービンロータ・ブレード組立体