HELICOPTER WITH A TRANSVERSE DUCT

The present invention relates to a helicopter having a tail unit (1) and a trailing axle line. A tail unit (1) includes a transverse duct (6) and a driving shaft (23) which is in a driving shaft fairing (14) for an aerodynamically and acoustically optimized reverse torque device (2) supported in a t...

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Bibliographic Details
Main Authors SASCHA SCHNEIDER, CHRISTIAN WEHLE, DIETER SCHIMKE
Format Patent
LanguageEnglish
Korean
Published 18.12.2013
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The present invention relates to a helicopter having a tail unit (1) and a trailing axle line. A tail unit (1) includes a transverse duct (6) and a driving shaft (23) which is in a driving shaft fairing (14) for an aerodynamically and acoustically optimized reverse torque device (2) supported in a transverse duct (6).
Bibliography:Application Number: KR20130065382