JP2003286857A5 - - Google Patents

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Publication number
JP2003286857A5
JP2003286857A5 JP2003055273A JP2003055273A JP2003286857A5 JP 2003286857 A5 JP2003286857 A5 JP 2003286857A5 JP 2003055273 A JP2003055273 A JP 2003055273A JP 2003055273 A JP2003055273 A JP 2003055273A JP 2003286857 A5 JP2003286857 A5 JP 2003286857A5
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JP
Japan
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JP2003055273A
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JP2003286857A (ja
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Priority claimed from US10/087,428 external-priority patent/US6732502B2/en
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Publication of JP2003286857A publication Critical patent/JP2003286857A/ja
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JP2003055273A 2002-03-01 2003-03-03 高い全圧力比の圧縮機を備えた二重反転式航空機用ガスタービンエンジン Pending JP2003286857A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/087,428 US6732502B2 (en) 2002-03-01 2002-03-01 Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor
US10/087428 2002-03-01

Publications (2)

Publication Number Publication Date
JP2003286857A JP2003286857A (ja) 2003-10-10
JP2003286857A5 true JP2003286857A5 (ja) 2006-05-11

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JP2003055273A Pending JP2003286857A (ja) 2002-03-01 2003-03-03 高い全圧力比の圧縮機を備えた二重反転式航空機用ガスタービンエンジン

Country Status (7)

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US (1) US6732502B2 (ja)
EP (1) EP1340903B1 (ja)
JP (1) JP2003286857A (ja)
CN (1) CN1453466A (ja)
CA (1) CA2419367C (ja)
DE (1) DE60336870D1 (ja)
RU (1) RU2302545C2 (ja)

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