To keep things simple lets just say I need to demonstrate that the flap will return to its closed position in the event of a power failure. After reviewing some of the ideas posted and the inherent complexity of the mechanical systems I am considering a hybrid hydraulic alternative. My thoughts...
what is a CB? .. the landing gear solution would be ideal, but I am trying to keep the system as simple as possible and i think it would add too much weight.
I know hydraulics are definite solution,but i wanted to come up with electric alternative. rb1957.. the flap would definitely need to be positioned by the mechanism. As far as the system jamming i think its going to be a possibility regardless of the system design.
I know the aerodynamic forces will be constantly changing, i was going to add a spring to keep constant pressure and act as the closing force in a stalled condition. From what I am gathering, a ball-screw can be pretty easily back-driven but at what cost to the holding power? What i am looking...
I am working on a project regarding general aviation aircraft. I need to deploy a device, very similar to flaps, on the airplane. For safety reasons the Flaps must be able to return to their original position if any system failure were to occur. In other words the actuators holding power must be...
