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
16.01.2018
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
Europäisches Patentamt | 2016
|Engineering Index Backfile | 1930
|Engineering Index Backfile | 1937
PERFORMANCE OF VEHICLE TRAFFIC HORNS
SAE Technical Papers | 1987