JP2011099437A5 - - Google Patents

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Publication number
JP2011099437A5
JP2011099437A5 JP2010245232A JP2010245232A JP2011099437A5 JP 2011099437 A5 JP2011099437 A5 JP 2011099437A5 JP 2010245232 A JP2010245232 A JP 2010245232A JP 2010245232 A JP2010245232 A JP 2010245232A JP 2011099437 A5 JP2011099437 A5 JP 2011099437A5
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JP
Japan
Prior art keywords
turbine blade
coating
protective coating
resistant
oxidation
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
JP2010245232A
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English (en)
Japanese (ja)
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JP5693149B2 (ja
JP2011099437A (ja
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Publication of JP2011099437A publication Critical patent/JP2011099437A/ja
Publication of JP2011099437A5 publication Critical patent/JP2011099437A5/ja
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Publication of JP5693149B2 publication Critical patent/JP5693149B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010245232A 2009-11-02 2010-11-01 耐摩耗性及び耐酸化性のタービン翼 Expired - Fee Related JP5693149B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009051661 2009-11-02
DE102009051661.1 2009-11-02

Publications (3)

Publication Number Publication Date
JP2011099437A JP2011099437A (ja) 2011-05-19
JP2011099437A5 true JP2011099437A5 (enExample) 2013-12-12
JP5693149B2 JP5693149B2 (ja) 2015-04-01

Family

ID=43402110

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010245232A Expired - Fee Related JP5693149B2 (ja) 2009-11-02 2010-11-01 耐摩耗性及び耐酸化性のタービン翼

Country Status (5)

Country Link
US (1) US8740572B2 (enExample)
EP (1) EP2316988B1 (enExample)
JP (1) JP5693149B2 (enExample)
CA (1) CA2719273C (enExample)
DE (1) DE102010049398A1 (enExample)

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DE102014202457A1 (de) 2014-02-11 2015-08-13 Siemens Aktiengesellschaft Verbesserte Verschleißbeständigkeit eines Hochtemperaturbauteils durch Kobaltbeschichtung
US9358663B2 (en) 2014-04-16 2016-06-07 General Electric Company System and methods of removing a multi-layer coating from a substrate
US20160237832A1 (en) * 2015-02-12 2016-08-18 United Technologies Corporation Abrasive blade tip with improved wear at high interaction rate
DE102015208781A1 (de) 2015-05-12 2016-11-17 MTU Aero Engines AG Kombination von Schaufelspitzenpanzerung und Erosionsschutzschicht sowie Verfahren zur Herstellung derselben
DE102015208783A1 (de) 2015-05-12 2016-11-17 MTU Aero Engines AG Abdeckverfahren zur Herstellung einer Kombination von Schaufelspitzenpanzerung und Erosionsschutzschicht
US10415579B2 (en) 2016-09-28 2019-09-17 General Electric Company Ceramic coating compositions for compressor blade and methods for forming the same
EP3301260A1 (en) * 2016-09-30 2018-04-04 Siemens Aktiengesellschaft Turbine blade with increase tip lifetime and a method for manufacturing said turbine blade
RU2645631C1 (ru) * 2016-12-07 2018-02-26 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" (КНИТУ-КАИ) Способ нанесения покрытия на образец (варианты) и устройство для его осуществления (варианты)
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US10533429B2 (en) * 2017-02-27 2020-01-14 Rolls-Royce Corporation Tip structure for a turbine blade with pressure side and suction side rails
EP3546703A1 (de) * 2018-03-29 2019-10-02 Siemens Aktiengesellschaft Turbinenlaufschaufel für eine gasturbine
EP3546702A1 (de) 2018-03-29 2019-10-02 Siemens Aktiengesellschaft Turbinenlaufschaufel für eine gasturbine
US11346232B2 (en) * 2018-04-23 2022-05-31 Rolls-Royce Corporation Turbine blade with abradable tip
US10933469B2 (en) 2018-09-10 2021-03-02 Honeywell International Inc. Method of forming an abrasive nickel-based alloy on a turbine blade tip
US20200157953A1 (en) * 2018-11-20 2020-05-21 General Electric Company Composite fan blade with abrasive tip
CN109249120B (zh) * 2018-11-23 2020-10-23 佛山市固高自动化技术有限公司 一种风机叶轮加工的多工位全自动焊接方法
CN109628921A (zh) * 2018-12-31 2019-04-16 中北大学 基于激光熔覆和脉冲电子束制备CoCrAlY涂层的方法
CN110747377B (zh) * 2019-11-15 2020-11-10 清华大学 一种高铬镍基高温合金及其制备方法与应用
CN110899695A (zh) * 2019-12-09 2020-03-24 浙江翰德圣智能再制造技术有限公司 一种激光增材制造微弧火花MCrAlY电极的方法
DE102020206202A1 (de) 2020-05-18 2021-11-18 MTU Aero Engines AG Schaufel für eine Strömungsmaschine mit Schaufelspitzenpanzerung und Erosionsschutzschicht und Verfahren zur Herstellung Derselben
DE202020107410U1 (de) 2020-12-18 2022-03-21 Liebherr-Aerospace Lindenberg Gmbh Metallisches Bauteil
US11486263B1 (en) 2021-06-28 2022-11-01 General Electric Company System for addressing turbine blade tip rail wear in rubbing and cooling
EP4245963B1 (en) * 2022-03-16 2025-09-10 Rolls-Royce Deutschland Ltd & Co KG Gas turbine engine and method for manufacturing a rotor blade
CN117102703B (zh) * 2022-05-16 2025-12-05 强一半导体(苏州)股份有限公司 一种复合陶瓷通孔的激光加工方法
DE102023100617A1 (de) * 2023-01-12 2024-07-18 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung eingetragener Verein Verfahren zum Beschichten und Zerspanen von Bauteilen
DE102023111281A1 (de) * 2023-05-02 2024-11-07 MTU Aero Engines AG Verfahren zum Bearbeiten eines Rotors eines Flugtriebwerks, welcher Schaufeln aufweist, die zumindest im Bereich ihrer Schaufelspitzen mit einer Beschichtung versehen sind, und Schneidwerkzeug

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US5794338A (en) * 1997-04-04 1998-08-18 General Electric Company Method for repairing a turbine engine member damaged tip
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