JP2003138902A5 - - Google Patents

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Publication number
JP2003138902A5
JP2003138902A5 JP2002291753A JP2002291753A JP2003138902A5 JP 2003138902 A5 JP2003138902 A5 JP 2003138902A5 JP 2002291753 A JP2002291753 A JP 2002291753A JP 2002291753 A JP2002291753 A JP 2002291753A JP 2003138902 A5 JP2003138902 A5 JP 2003138902A5
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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.)
Granted
Application number
JP2002291753A
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Japanese (ja)
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JP2003138902A (ja
JP4307814B2 (ja
Filing date
Publication date
Priority claimed from US09/972,443 external-priority patent/US6682301B2/en
Application filed filed Critical
Publication of JP2003138902A publication Critical patent/JP2003138902A/ja
Publication of JP2003138902A5 publication Critical patent/JP2003138902A5/ja
Application granted granted Critical
Publication of JP4307814B2 publication Critical patent/JP4307814B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2002291753A 2001-10-05 2002-10-04 衝撃波が減少された遷音速翼形部 Expired - Fee Related JP4307814B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/972443 2001-10-05
US09/972,443 US6682301B2 (en) 2001-10-05 2001-10-05 Reduced shock transonic airfoil

Publications (3)

Publication Number Publication Date
JP2003138902A JP2003138902A (ja) 2003-05-14
JP2003138902A5 true JP2003138902A5 (enExample) 2005-11-04
JP4307814B2 JP4307814B2 (ja) 2009-08-05

Family

ID=25519663

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002291753A Expired - Fee Related JP4307814B2 (ja) 2001-10-05 2002-10-04 衝撃波が減少された遷音速翼形部

Country Status (3)

Country Link
US (2) US6682301B2 (enExample)
EP (1) EP1300547B1 (enExample)
JP (1) JP4307814B2 (enExample)

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US11454120B2 (en) * 2018-12-07 2022-09-27 General Electric Company Turbine airfoil profile
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