DD23971A - - Google Patents

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Publication number
DD23971A
DD23971A DD23971DA DD23971A DD 23971 A DD23971 A DD 23971A DD 23971D A DD23971D A DD 23971DA DD 23971 A DD23971 A DD 23971A
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DD
German Democratic Republic
Application number
Publication of DD23971A publication Critical patent/DD23971A/xx

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DD23971D DD23971A (de)

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DD23971A true DD23971A (de)

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ID=232698

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DD (1) DD23971A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008062813A1 (de) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einer Heck-Propeller-Triebwerksanordnung
US8402740B2 (en) 2008-02-28 2013-03-26 Rolls-Royce Deutschland Ltd & Co Kg Aircraft propulsion unit in multi-fan design

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8402740B2 (en) 2008-02-28 2013-03-26 Rolls-Royce Deutschland Ltd & Co Kg Aircraft propulsion unit in multi-fan design
DE102008062813A1 (de) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einer Heck-Propeller-Triebwerksanordnung

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DD23971A (de)