A counter-rotating propeller system (14) comprises a cyclic pitch system (60) connected to a first plurality of propeller blades (18) and a variable pitch system (100) connected to a second plurality of propeller blades (20). The first plurality of propeller blades (18) and the second plurality of propeller blades (20) are configured to rotate about a common axis (A).
Cyclic pitch actuation system for counter-rotating propellers
Zyklisches Neigungsbetätigungssystem für gegenläufige Propeller
Système d'actionnement de pas cyclique pour hélices contrarotatives
19.08.2015
Patent
Elektronische Ressource
Englisch
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|Engineering Index Backfile | 1940
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