JP2014231797A5 - - Google Patents

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Publication number
JP2014231797A5
JP2014231797A5 JP2013113415A JP2013113415A JP2014231797A5 JP 2014231797 A5 JP2014231797 A5 JP 2014231797A5 JP 2013113415 A JP2013113415 A JP 2013113415A JP 2013113415 A JP2013113415 A JP 2013113415A JP 2014231797 A5 JP2014231797 A5 JP 2014231797A5
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JP
Japan
Prior art keywords
gas turbine
degrees
partition wall
turbine
longitudinal direction
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.)
Granted
Application number
JP2013113415A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014231797A (ja
JP6184173B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority to JP2013113415A priority Critical patent/JP6184173B2/ja
Priority claimed from JP2013113415A external-priority patent/JP6184173B2/ja
Priority to CN201410228340.XA priority patent/CN104213943B/zh
Priority to US14/289,188 priority patent/US9822659B2/en
Priority to EP14170172.2A priority patent/EP2813671A1/en
Publication of JP2014231797A publication Critical patent/JP2014231797A/ja
Publication of JP2014231797A5 publication Critical patent/JP2014231797A5/ja
Application granted granted Critical
Publication of JP6184173B2 publication Critical patent/JP6184173B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013113415A 2013-05-29 2013-05-29 ガスタービン Active JP6184173B2 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2013113415A JP6184173B2 (ja) 2013-05-29 2013-05-29 ガスタービン
CN201410228340.XA CN104213943B (zh) 2013-05-29 2014-05-27 燃气轮机
US14/289,188 US9822659B2 (en) 2013-05-29 2014-05-28 Gas turbine with honeycomb seal
EP14170172.2A EP2813671A1 (en) 2013-05-29 2014-05-28 Gas turbine with honeycomb seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013113415A JP6184173B2 (ja) 2013-05-29 2013-05-29 ガスタービン

Publications (3)

Publication Number Publication Date
JP2014231797A JP2014231797A (ja) 2014-12-11
JP2014231797A5 true JP2014231797A5 (enExample) 2016-07-14
JP6184173B2 JP6184173B2 (ja) 2017-08-23

Family

ID=50897373

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013113415A Active JP6184173B2 (ja) 2013-05-29 2013-05-29 ガスタービン

Country Status (4)

Country Link
US (1) US9822659B2 (enExample)
EP (1) EP2813671A1 (enExample)
JP (1) JP6184173B2 (enExample)
CN (1) CN104213943B (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10371163B2 (en) * 2016-02-02 2019-08-06 General Electric Company Load absorption systems and methods
US10718352B2 (en) 2016-07-26 2020-07-21 Rolls-Royce Corporation Multi-cellular abradable liner
US10472980B2 (en) * 2017-02-14 2019-11-12 General Electric Company Gas turbine seals
US10369630B2 (en) * 2017-02-24 2019-08-06 General Electric Company Polyhedral-sealed article and method for forming polyhedral-sealed article
WO2019013665A1 (en) * 2017-07-14 2019-01-17 Siemens Aktiengesellschaft HIGHLY ELONGATED FIN TIP SEAL ARRANGEMENT
JP6986426B2 (ja) * 2017-11-29 2021-12-22 三菱重工業株式会社 タービン
WO2019177599A1 (en) * 2018-03-14 2019-09-19 Siemens Energy, Inc. Canted honeycomb abradable structure for a gas turbine
IT201900014724A1 (it) 2019-08-13 2021-02-13 Ge Avio Srl Elementi di trattenimento delle pale per turbomacchine.
IT201900014736A1 (it) 2019-08-13 2021-02-13 Ge Avio Srl Elementi di tenuta integrali per pale trattenute in un rotore a tamburo esterno anulare girevole in una turbomacchina.
IT201900014739A1 (it) 2019-08-13 2021-02-13 Ge Avio Srl Elementi di trattenimento delle pale per turbomacchine.
WO2022091798A1 (ja) * 2020-10-30 2022-05-05 三菱重工業株式会社 ハニカムシール、及び回転機械
FR3122668B1 (fr) * 2021-05-04 2023-05-26 Safran Aircraft Engines Procédé de montage d’un élément abradable comprenant une structure alvéolaire dans une gorge annulaire d’un organe de turbomachine
US11674405B2 (en) 2021-08-30 2023-06-13 General Electric Company Abradable insert with lattice structure
CN119754880A (zh) * 2024-12-19 2025-04-04 哈尔滨工业大学 一种用于削弱小尺寸叶轮机械叶顶泄露流的机匣处理结构

Family Cites Families (25)

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Publication number Priority date Publication date Assignee Title
GB793886A (en) * 1955-01-24 1958-04-23 Solar Aircraft Co Improvements in or relating to sealing means between relatively movable parts
US3365172A (en) * 1966-11-02 1968-01-23 Gen Electric Air cooled shroud seal
JPS4623525Y1 (enExample) 1967-07-17 1971-08-13
US3649033A (en) 1969-12-24 1972-03-14 Nippon Denso Co Honeycomb rotor-sealing device and method of manufacture
FR2552159B1 (fr) * 1983-09-21 1987-07-10 Snecma Dispositif de liaison et d'etancheite de secteurs d'aubes de stator de turbine
US4884820A (en) * 1987-05-19 1989-12-05 Union Carbide Corporation Wear resistant, abrasive laser-engraved ceramic or metallic carbide surfaces for rotary labyrinth seal members
US4832999A (en) * 1987-10-27 1989-05-23 Avco Lycoming/Textron Honeycomb structure assemblies
US5520508A (en) * 1994-12-05 1996-05-28 United Technologies Corporation Compressor endwall treatment
DE19828065A1 (de) * 1998-06-24 1999-12-30 Bmw Rolls Royce Gmbh Wabenstruktur-Dichtung insbesondere für eine Gasturbine
US6120242A (en) * 1998-11-13 2000-09-19 General Electric Company Blade containing turbine shroud
JP2001123803A (ja) * 1999-10-21 2001-05-08 Toshiba Corp シール装置並びに同装置を備えた蒸気タービン及び発電プラント
DE10038452B4 (de) * 2000-08-07 2011-05-26 Alstom Technology Ltd. Abdichtung einer thermischen Turbomaschine
US6652226B2 (en) 2001-02-09 2003-11-25 General Electric Co. Methods and apparatus for reducing seal teeth wear
FR2846034B1 (fr) * 2002-10-22 2006-06-23 Snecma Moteurs Carter, compresseur, turbine et turbomoteur a combustion comprenant un tel carter
JP4370894B2 (ja) 2003-12-04 2009-11-25 株式会社Ｉｈｉ 密封装置
DE102005002270A1 (de) * 2005-01-18 2006-07-20 Mtu Aero Engines Gmbh Triebwerk
US7686581B2 (en) * 2006-06-07 2010-03-30 General Electric Company Serpentine cooling circuit and method for cooling tip shroud
US9009965B2 (en) * 2007-05-24 2015-04-21 General Electric Company Method to center locate cutter teeth on shrouded turbine blades
JP5173887B2 (ja) 2009-02-25 2013-04-03 三菱重工業株式会社 シール材
JP2011226559A (ja) * 2010-04-20 2011-11-10 Mitsubishi Heavy Ind Ltd 被切削性ハニカムシール材及びガスタービン
CN201943757U (zh) 2010-12-14 2011-08-24 北京蓝爱迪电力技术有限公司 一种两维倾斜蜂窝汽封
CN201884072U (zh) * 2010-12-14 2011-06-29 北京蓝爱迪电力技术有限公司 一种轴向倾斜蜂窝汽封
CN201943758U (zh) * 2010-12-14 2011-08-24 北京蓝爱迪电力技术有限公司 一种切向倾斜蜂窝汽封
US8790088B2 (en) * 2011-04-20 2014-07-29 General Electric Company Compressor having blade tip features
JP2013019507A (ja) 2011-07-13 2013-01-31 Mitsubishi Heavy Ind Ltd シール材

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