Mechanical closed transmission device for coaxial double-propeller helicopter main reduction test bed
The invention relates to the field of transmission, and particularly relates to a mechanical closed transmission device for a coaxial double-propeller helicopter main reduction test bed. The device comprises a coaxial double-propeller main reducer including an outer rotor shaft and an inner rotor sh...
Gespeichert in:
Hauptverfasser: | , , , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | The invention relates to the field of transmission, and particularly relates to a mechanical closed transmission device for a coaxial double-propeller helicopter main reduction test bed. The device comprises a coaxial double-propeller main reducer including an outer rotor shaft and an inner rotor shaft, a pair of coaxial double-propeller transmission assemblies which are symmetrical to each other,the outer rotor shaft and the inner rotor shaft. The coaxial double-propeller transmission assembly comprises an inner rotor upper gear box, an outer rotor upper gear box, a reversing gear box and ahigh-speed gear box. The device lays a foundation for overhaul and localization development of the main reducer of the type.
本发明涉及传动领域,是用于共轴双桨直升机主减试车台的机械封闭传动装置。该装置包括:包括外旋翼轴和内旋翼轴的共轴双桨主减、相互对称的一对共轴双桨传动组件、外旋翼轴、内旋翼轴;共轴双桨传动组件包括:内旋翼上置齿轮箱、外旋翼上置齿轮箱、换向齿轮箱和高速齿轮箱。本发明为该型主减的大修和国产化研制奠定基础。 |
---|