JP2015098848A5 - - Google Patents

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Publication number
JP2015098848A5
JP2015098848A5 JP2013239794A JP2013239794A JP2015098848A5 JP 2015098848 A5 JP2015098848 A5 JP 2015098848A5 JP 2013239794 A JP2013239794 A JP 2013239794A JP 2013239794 A JP2013239794 A JP 2013239794A JP 2015098848 A5 JP2015098848 A5 JP 2015098848A5
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JP
Japan
Prior art keywords
blade
stop plate
axial
rotor disk
axial groove
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.)
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Application number
JP2013239794A
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English (en)
Japanese (ja)
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JP5999845B2 (ja
JP2015098848A (ja
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Priority claimed from JP2013239794A external-priority patent/JP5999845B2/ja
Priority to JP2013239794A priority Critical patent/JP5999845B2/ja
Priority to EP14864540.1A priority patent/EP3023590A4/en
Priority to PCT/JP2014/069897 priority patent/WO2015075970A1/ja
Priority to CN201480046021.5A priority patent/CN105473824A/zh
Priority to KR1020167003952A priority patent/KR20160030314A/ko
Publication of JP2015098848A publication Critical patent/JP2015098848A/ja
Publication of JP2015098848A5 publication Critical patent/JP2015098848A5/ja
Publication of JP5999845B2 publication Critical patent/JP5999845B2/ja
Application granted granted Critical
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Anticipated expiration legal-status Critical

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JP2013239794A 2013-11-20 2013-11-20 タービンロータ組立体およびタービンロータ組立体における翼止板並びに翼止板の組付け方法 Active JP5999845B2 (ja)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2013239794A JP5999845B2 (ja) 2013-11-20 2013-11-20 タービンロータ組立体およびタービンロータ組立体における翼止板並びに翼止板の組付け方法
KR1020167003952A KR20160030314A (ko) 2013-11-20 2014-07-29 터빈 로터 조립체 및 터빈 로터 조립체에 있어서의 블레이드 정지판 그리고 블레이드 정지판의 설치 방법
PCT/JP2014/069897 WO2015075970A1 (ja) 2013-11-20 2014-07-29 タービンロータ組立体およびタービンロータ組立体における翼止板並びに翼止板の組付け方法
CN201480046021.5A CN105473824A (zh) 2013-11-20 2014-07-29 涡轮机转子组装体和涡轮机转子组装体的叶片止动板以及叶片止动板的组装方法
EP14864540.1A EP3023590A4 (en) 2013-11-20 2014-07-29 TURBINE ROTOR ASSEMBLY, TURBO ROTOR PLATE FOR TURBINE ROTOR ASSEMBLY AND METHOD FOR MOUNTING A PLATE OF PLATE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013239794A JP5999845B2 (ja) 2013-11-20 2013-11-20 タービンロータ組立体およびタービンロータ組立体における翼止板並びに翼止板の組付け方法

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2016166603A Division JP2016205402A (ja) 2016-08-29 2016-08-29 翼止板

Publications (3)

Publication Number Publication Date
JP2015098848A JP2015098848A (ja) 2015-05-28
JP2015098848A5 true JP2015098848A5 (ko) 2016-02-04
JP5999845B2 JP5999845B2 (ja) 2016-09-28

Family

ID=53179249

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013239794A Active JP5999845B2 (ja) 2013-11-20 2013-11-20 タービンロータ組立体およびタービンロータ組立体における翼止板並びに翼止板の組付け方法

Country Status (5)

Country Link
EP (1) EP3023590A4 (ko)
JP (1) JP5999845B2 (ko)
KR (1) KR20160030314A (ko)
CN (1) CN105473824A (ko)
WO (1) WO2015075970A1 (ko)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6499777B2 (ja) 2016-01-13 2019-04-10 三菱日立パワーシステムズ株式会社 翼引き抜き装置及び方法
FR3057908B1 (fr) * 2016-10-21 2019-11-22 Safran Aircraft Engines Ensemble rotatif d'une turbomachine muni d'un systeme de maintien axial d'une aube
CN113710414A (zh) 2019-03-29 2021-11-26 平田机工株式会社 测定装置
SG11202110089XA (en) 2019-03-29 2021-10-28 Hirata Spinning Attachment device
JP7145320B2 (ja) 2019-03-29 2022-09-30 平田機工株式会社 製造システム
CN110259521A (zh) * 2019-07-31 2019-09-20 中国科学院工程热物理研究所 一种用于叶轮机械的叶片保持器
CN114076000B (zh) * 2020-08-17 2024-05-07 中国航发商用航空发动机有限责任公司 叶片轴向限位装置、叶盘结构以及燃气轮机
CN112096653B (zh) * 2020-11-18 2021-01-19 中国航发上海商用航空发动机制造有限责任公司 叶片缘板、叶片环、叶轮盘以及燃气涡轮发动机
CN113478180B (zh) * 2021-07-15 2022-11-25 重庆江增船舶重工有限公司 一种增压器锁紧片的加工方法及其翻边工具

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2801074A (en) * 1952-10-01 1957-07-30 United Aircraft Corp Blade retaining means
US3045329A (en) * 1959-07-30 1962-07-24 Gen Electric Method for assembling tongue-and-groove members with locking keys
JPH0414702U (ko) * 1990-05-24 1992-02-06
JPH0514501U (ja) 1991-08-01 1993-02-26 三菱重工業株式会社 流体機械の動翼
JPH0618601U (ja) * 1992-08-10 1994-03-11 石川島播磨重工業株式会社 タービン動翼のダンパー
JPH10317907A (ja) * 1997-05-22 1998-12-02 Hitachi Ltd 圧縮機翼固定構造
DE19757188A1 (de) * 1997-12-22 1999-06-24 Asea Brown Boveri Einrichtung zur Befestigung der Laufschaufeln einstufiger Axialturbinen
US6190131B1 (en) * 1999-08-31 2001-02-20 General Electric Co. Non-integral balanced coverplate and coverplate centering slot for a turbine
JP4315801B2 (ja) 2001-07-03 2009-08-19 アーベーベー・ターボ・ジステムス・アクチエンゲゼルシヤフト 軸流ターボ機械の動翼のための固定システム
US8425194B2 (en) * 2007-07-19 2013-04-23 General Electric Company Clamped plate seal
FR2921409B1 (fr) * 2007-09-25 2009-12-18 Snecma Clinquant pour aube de turbomachine.

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