In a material determining step, the material constituting an actuator and the material constituting a link are determined such that at least one of the materials contains fiber reinforced plastic. In a computing step, a computation model that defines the relationship between a control surface, the actuator, and the link is used to compute the change in gain margin with the change in a rigidity ratio, which is the ratio of the rigidity of the link to the rigidity of the actuator. The rigidities of the actuator and the link are determined in a rigidity determining step based on a result of the above-described computation, the shapes of the actuator and the link are determined in a shape determining step, and the actuator and the link are formed in a formation step, and are assembled in an assembly step.
Actuator-link assembly manufacturing method, actuator-link assembly designing method, and actuator-link assembly
Verfahren zur Herstellung einer Aktuatorverbindungsanordnung, Verfahren zum Entwurf einer Aktuatorverbindungsanordnung und Aktuatorverbindungsanordnung
Procédé de fabrication d'ensemble de lien d'actionneur, procédé de conception d'ensemble de lien d'actionneur et ensemble de lien d'actionneur
2018-01-24
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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