JP2004076739A5 - - Google Patents

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Publication number
JP2004076739A5
JP2004076739A5 JP2003294855A JP2003294855A JP2004076739A5 JP 2004076739 A5 JP2004076739 A5 JP 2004076739A5 JP 2003294855 A JP2003294855 A JP 2003294855A JP 2003294855 A JP2003294855 A JP 2003294855A JP 2004076739 A5 JP2004076739 A5 JP 2004076739A5
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JP
Japan
Prior art keywords
low pressure
pressure turbine
turbine blade
blade row
row
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.)
Granted
Application number
JP2003294855A
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English (en)
Japanese (ja)
Other versions
JP4588306B2 (ja
JP2004076739A (ja
Filing date
Publication date
Priority claimed from US10/223,163 external-priority patent/US6711887B2/en
Application filed filed Critical
Publication of JP2004076739A publication Critical patent/JP2004076739A/ja
Publication of JP2004076739A5 publication Critical patent/JP2004076739A5/ja
Application granted granted Critical
Publication of JP4588306B2 publication Critical patent/JP4588306B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2003294855A 2002-08-19 2003-08-19 非交互嵌合二重反転式低圧タービンを備えた航空機用ガスタービンエンジン Expired - Fee Related JP4588306B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/223,163 US6711887B2 (en) 2002-08-19 2002-08-19 Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines

Publications (3)

Publication Number Publication Date
JP2004076739A JP2004076739A (ja) 2004-03-11
JP2004076739A5 true JP2004076739A5 (https=) 2006-09-28
JP4588306B2 JP4588306B2 (ja) 2010-12-01

Family

ID=31495293

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003294855A Expired - Fee Related JP4588306B2 (ja) 2002-08-19 2003-08-19 非交互嵌合二重反転式低圧タービンを備えた航空機用ガスタービンエンジン

Country Status (6)

Country Link
US (1) US6711887B2 (https=)
EP (1) EP1394385B1 (https=)
JP (1) JP4588306B2 (https=)
CN (1) CN1333165C (https=)
CA (1) CA2436664C (https=)
DE (1) DE60300804T2 (https=)

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US8744228B2 (en) * 2009-05-22 2014-06-03 Commscope, Inc. Of North Carolina Telecommunications patching system with cable management system and related cable management equipment
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US9506402B2 (en) 2011-07-29 2016-11-29 United Technologies Corporation Three spool engine bearing configuration
US10287976B2 (en) 2014-07-15 2019-05-14 United Technologies Corporation Split gear system for a gas turbine engine
US9932902B2 (en) 2014-07-15 2018-04-03 United Technologies Corporation Turbine section support for a gas turbine engine
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US11053797B2 (en) * 2017-01-23 2021-07-06 General Electric Company Rotor thrust balanced turbine engine
US10654577B2 (en) * 2017-02-22 2020-05-19 General Electric Company Rainbow flowpath low pressure turbine rotor assembly
US11085309B2 (en) 2017-09-22 2021-08-10 General Electric Company Outer drum rotor assembly
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
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