Kontrol Yüzeyleri Aktüatör ve Tahrik Mekanizması Geliştirme Çalışmaları

In order to see the system reactions of the piston pump to be used in the control surfaces hydraulic actuators, mathematical modeling will be done in the Amesim program and integrated into the general system architecture.

• Different drive mechanisms will be used to drive control surfaces in aircraft. Different freeplay amounts will occur due to the connection types of the mechanisms. There will be free play amounts that may be caused by the connection types used in the mechanisms. The amount of freeplay that may be caused by the connection types used in the mechanisms will be predicted by literature research and 2D or 3D modeling. Alternative designs will be made for designs with high amounts of freeplay.