JP2006052732A5 - - Google Patents

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Publication number
JP2006052732A5
JP2006052732A5 JP2005229006A JP2005229006A JP2006052732A5 JP 2006052732 A5 JP2006052732 A5 JP 2006052732A5 JP 2005229006 A JP2005229006 A JP 2005229006A JP 2005229006 A JP2005229006 A JP 2005229006A JP 2006052732 A5 JP2006052732 A5 JP 2006052732A5
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JP
Japan
Prior art keywords
blade
group
blades
pockets
filling
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.)
Pending
Application number
JP2005229006A
Other languages
English (en)
Japanese (ja)
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JP2006052732A (ja
Filing date
Publication date
Priority claimed from US10/913,407 external-priority patent/US7147437B2/en
Application filed filed Critical
Publication of JP2006052732A publication Critical patent/JP2006052732A/ja
Publication of JP2006052732A5 publication Critical patent/JP2006052732A5/ja
Pending legal-status Critical Current

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JP2005229006A 2004-08-09 2005-08-08 混合同調ハイブリッドブレードおよびそれに関連する方法 Pending JP2006052732A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/913,407 US7147437B2 (en) 2004-08-09 2004-08-09 Mixed tuned hybrid blade related method

Publications (2)

Publication Number Publication Date
JP2006052732A JP2006052732A (ja) 2006-02-23
JP2006052732A5 true JP2006052732A5 (https=) 2008-09-18

Family

ID=34941842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2005229006A Pending JP2006052732A (ja) 2004-08-09 2005-08-08 混合同調ハイブリッドブレードおよびそれに関連する方法

Country Status (6)

Country Link
US (1) US7147437B2 (https=)
EP (1) EP1626161B1 (https=)
JP (1) JP2006052732A (https=)
KR (1) KR20060050297A (https=)
CN (1) CN1734062B (https=)
DE (1) DE602005006483D1 (https=)

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US7429165B2 (en) * 2006-06-14 2008-09-30 General Electric Company Hybrid blade for a steam turbine
EP1985803A1 (de) * 2007-04-23 2008-10-29 Siemens Aktiengesellschaft Verfahren zum Herstellen von beschichteten Turbinenlaufschaufeln
US7887299B2 (en) * 2007-06-07 2011-02-15 Honeywell International Inc. Rotary body for turbo machinery with mistuned blades
GB2450936B (en) * 2007-07-13 2010-01-20 Rolls Royce Plc Bladed rotor balancing
GB2450937B (en) * 2007-07-13 2009-06-03 Rolls Royce Plc Component with tuned frequency response
US8100641B2 (en) * 2008-09-09 2012-01-24 General Electric Company Steam turbine having stage with buckets of different materials
US8043063B2 (en) * 2009-03-26 2011-10-25 Pratt & Whitney Canada Corp. Intentionally mistuned integrally bladed rotor
US8419370B2 (en) * 2009-06-25 2013-04-16 Rolls-Royce Corporation Retaining and sealing ring assembly
US8469670B2 (en) * 2009-08-27 2013-06-25 Rolls-Royce Corporation Fan assembly
US8435006B2 (en) * 2009-09-30 2013-05-07 Rolls-Royce Corporation Fan
FR2956875B1 (fr) * 2010-02-26 2012-09-21 Snecma Aube allegee pour turbomachine, carter comportant une pluralite d'une telle aube et turbomachine comportant au moins un tel carter
US8726725B2 (en) 2011-03-08 2014-05-20 Schlumberger Technology Corporation Apparatus, system and method for determining at least one downhole parameter of a wellsite
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US9097125B2 (en) * 2012-08-17 2015-08-04 Mapna Group Intentionally frequency mistuned turbine blades
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US10641281B2 (en) 2016-08-08 2020-05-05 United Technologies Corporation Mistuned laminate airfoil
US10837287B2 (en) * 2017-01-20 2020-11-17 Pratt & Whitney Canada Corp. Mistuned bladed rotor and associated manufacturing method
JP6745235B2 (ja) * 2017-03-10 2020-08-26 三菱日立パワーシステムズ株式会社 ロータ及びこのロータを備える回転機械
US10954804B2 (en) * 2017-07-05 2021-03-23 Raytheon Technologies Corporation Rotary machines including a hybrid rotor with hollow and solid rotor blade sets
WO2019087281A1 (ja) * 2017-10-31 2019-05-09 三菱重工エンジン＆ターボチャージャ株式会社 タービン動翼、ターボチャージャ及びタービン動翼の製造方法
US10731471B2 (en) * 2018-12-28 2020-08-04 General Electric Company Hybrid rotor blades for turbine engines
JP7219829B2 (ja) * 2019-06-28 2023-02-08 シーメンス エナジー グローバル ゲゼルシャフト ミット ベシュレンクテル ハフツング ウント コンパニー コマンディートゲゼルシャフト モーダル周波数応答の調整を行うタービン翼形部
US11220913B2 (en) * 2019-10-23 2022-01-11 Rolls-Royce Corporation Gas turbine engine blades with airfoil plugs for selected tuning
US11255199B2 (en) 2020-05-20 2022-02-22 Rolls-Royce Corporation Airfoil with shaped mass reduction pocket
US11767765B2 (en) * 2021-09-28 2023-09-26 General Electric Company Glass viscous damper
US11746659B2 (en) 2021-12-23 2023-09-05 Rolls-Royce North American Technologies Inc. Fan blade with internal shear-thickening fluid damping
US11560801B1 (en) 2021-12-23 2023-01-24 Rolls-Royce North American Technologies Inc. Fan blade with internal magnetorheological fluid damping
US12043368B2 (en) * 2022-03-23 2024-07-23 General Electric Company Rotating airfoil assembly

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US5947688A (en) * 1997-12-22 1999-09-07 General Electric Company Frequency tuned hybrid blade
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