JP2003278502A5 - - Google Patents

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Publication number
JP2003278502A5
JP2003278502A5 JP2002298169A JP2002298169A JP2003278502A5 JP 2003278502 A5 JP2003278502 A5 JP 2003278502A5 JP 2002298169 A JP2002298169 A JP 2002298169A JP 2002298169 A JP2002298169 A JP 2002298169A JP 2003278502 A5 JP2003278502 A5 JP 2003278502A5
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JP
Japan
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
JP2002298169A
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JP2003278502A (ja
JP4184031B2 (ja
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Publication date
Priority claimed from US09/976,564 external-priority patent/US6843928B2/en
Application filed filed Critical
Publication of JP2003278502A publication Critical patent/JP2003278502A/ja
Publication of JP2003278502A5 publication Critical patent/JP2003278502A5/ja
Application granted granted Critical
Publication of JP4184031B2 publication Critical patent/JP4184031B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2002298169A 2001-10-12 2002-10-11 翼形部基体から金属クラッドを除去するための方法 Expired - Fee Related JP4184031B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/976,564 US6843928B2 (en) 2001-10-12 2001-10-12 Method for removing metal cladding from airfoil substrate
US09/976564 2001-10-12

Publications (3)

Publication Number Publication Date
JP2003278502A JP2003278502A (ja) 2003-10-02
JP2003278502A5 true JP2003278502A5 (ja) 2005-11-04
JP4184031B2 JP4184031B2 (ja) 2008-11-19

Family

ID=25524230

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002298169A Expired - Fee Related JP4184031B2 (ja) 2001-10-12 2002-10-11 翼形部基体から金属クラッドを除去するための方法

Country Status (7)

Country Link
US (1) US6843928B2 (ja)
EP (1) EP1302562B1 (ja)
JP (1) JP4184031B2 (ja)
BR (1) BR0204152B1 (ja)
CA (1) CA2406430C (ja)
DE (1) DE60219116T2 (ja)
SG (1) SG107616A1 (ja)

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US9752441B2 (en) 2012-01-31 2017-09-05 United Technologies Corporation Gas turbine rotary blade with tip insert
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US20140064937A1 (en) * 2012-06-29 2014-03-06 General Electric Company Fan blade brush tip
US10385703B2 (en) * 2013-03-08 2019-08-20 United Technologies Corporation Fan blades with protective sheaths and galvanic shields
US20140259667A1 (en) * 2013-03-13 2014-09-18 James Witt System, kit and method for surface repair and reconditioning of industrial sized fan blades such as incorporated into a cooling tower
WO2014204573A1 (en) * 2013-06-17 2014-12-24 United Technologies Corporation Composite airfoil bonded to a metallic root
WO2015034612A1 (en) * 2013-09-09 2015-03-12 United Technologies Corporation Fan blades and manufacture methods
US10487843B2 (en) * 2013-09-09 2019-11-26 United Technologies Corporation Fan blades and manufacture methods
WO2015041841A1 (en) 2013-09-17 2015-03-26 United Technologies Corporation Aluminum airfoil with titanium coating
JP6278191B2 (ja) * 2014-04-07 2018-02-14 株式会社Ihi 複合材翼及び複合材翼の製造方法
FR3025127B1 (fr) * 2014-08-28 2017-03-17 Snecma Reparation d'un assemblage comprenant un corps principal et un renfort
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