JP2003254083A5 - - Google Patents

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JP2003254083A5
JP2003254083A5 JP2002376196A JP2002376196A JP2003254083A5 JP 2003254083 A5 JP2003254083 A5 JP 2003254083A5 JP 2002376196 A JP2002376196 A JP 2002376196A JP 2002376196 A JP2002376196 A JP 2002376196A JP 2003254083 A5 JP2003254083 A5 JP 2003254083A5
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JP
Japan
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JP2002376196A
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JP2003254083A (ja
JP4204310B2 (ja
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Priority claimed from US10/087,681 external-priority patent/US6619030B1/en
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Publication of JP4204310B2 publication Critical patent/JP4204310B2/ja
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JP2002376196A 2002-03-01 2002-12-26 タービン間エンジンフレームによって支持された二重反転式低圧タービンロータを備える航空機用エンジン Expired - Fee Related JP4204310B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/087681 2002-03-01
US10/087,681 US6619030B1 (en) 2002-03-01 2002-03-01 Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors

Publications (3)

Publication Number Publication Date
JP2003254083A JP2003254083A (ja) 2003-09-10
JP2003254083A5 true JP2003254083A5 (ja) 2008-09-18
JP4204310B2 JP4204310B2 (ja) 2009-01-07

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JP2002376196A Expired - Fee Related JP4204310B2 (ja) 2002-03-01 2002-12-26 タービン間エンジンフレームによって支持された二重反転式低圧タービンロータを備える航空機用エンジン

Country Status (6)

Country Link
US (1) US6619030B1 (ja)
EP (1) EP1340902B1 (ja)
JP (1) JP4204310B2 (ja)
CA (1) CA2414992C (ja)
DE (1) DE60220636T2 (ja)
RU (1) RU2295046C2 (ja)

Families Citing this family (317)

* Cited by examiner, † Cited by third party
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