A rotorcraft rotor comprises a blade having a pitch axis, a primary pitch horn for the blade, and a secondary horn opposite the primary pitch horn with respect to the pitch axis.
Un rotor de giravion comprend une pale qui a un axe de tangage, un bras de commande primaire de la pale et un bras de commande secondaire opposé au bras de commande primaire par rapport à laxe de tangage.
ROTORCRAFT ROTOR INCLUDING PRIMARY PITCH HORNS AND SECONDARY HORNS
ROTOR DE GIRAVION COMPRENANT DES BRAS DE COMMANDE DE PAS PRIMAIRES ET DES BRAS DE COMMANDE SECONDAIRES
2018-01-16
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rotorcraft rotor including primary pitch horns and secondary horns
Europäisches Patentamt | 2018
|Rotorcraft rotor including primary pitch horns and secondary horns
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|Engineering Index Backfile | 1930
|PERFORMANCE OF VEHICLE TRAFFIC HORNS
SAE Technical Papers | 1987
Engineering Index Backfile | 1937